$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ NEAR $ $ Near Earth Asteroid Rendevous DPTRAJ-ODP CRUISE LOCKFILE, VERSION 1.1 $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ This file contains the text used to create near_lock_eros_V1.1.nio, $ the master DPTRAJ-ODP GIN file for NEAR radio science. $ $ Throughout this file, it is assumed EROS will take the place of Pluto $ as the object with ID code #9. $ $ Jon Giorgini $ $ -- CHANGE HISTORY -- $ $ June 1998 Version 1.0 $ Sept 1998 Version 1.1 Update station covariance (APNAM4, APNAM5) $ Add Eros Set III covariance $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ IDPXIT = 0, $ LABL(1) = 'EROS LOCKFILE V1.1 - OCTOBER 1998', LABL(2) = 'NEAR NAV/RADIO SCIENCE', LABL(3) = ' ', SCNAME = 'NEAR', SCID = 93, REF50 = .FALSE., $ Reference epoch: .FALSE. => 2000, .TRUE. => 1950 $ $ J2000 is an inertial coordinate system defined here by the planetary $ ephemeris and has a standard epoch of January 1.5, 2000, JD 2451545.0 $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Astrodynamic constants from planetary & satellite ephemerides: $ $ The following astrodynamic constants are nominally obtained from the $ planetary and satellite ephemerides, unless explicitly specified in $ the GIN inputs. $ $ For these constants, the program GINUPDATE does the following: $ $ i) If the GIN inputs contain the values, it uses these. $ $ Otherwise: $ ii) If a satellite ephemeris is used, it gets the values from there. $ $ Otherwise: $ iii) It will read the values from the planet ephemeris, if used. $ $ In summary, all parameters are obtained from the assigned ephemerides; $ however, these values may be overwritten by GIN inputs. Two exceptions $ are AU and C: they cannot be overwritten by GIN inputs. $ $ $ Constants nominally obtained from the satellite ephemeris: $ $ GM of planet and satellites: GM, SATGM $ J2 & J3 of the planet: OBAJ(2), OBAJ(3) $ Planet pole right ascension, declination & rates & time: PLCOF $ $ The names on the satellite ephemeris file for Mars are: $ GM4, RADIUS, J402, J404, ZACPL4, ZDEPL4, DACPL4, $ DDEPL4, POLTIM, 401GM, 402GM, 400GM $ $ $ Constants nominally obtained from the planetary ephemeris: $ AU, BETREL, C, GAMREL, GM $ $ Note: Here GM(3) = GM0300 is calculated from GM0301 and EMRAT on the $ file by using GM0300 = EMRAT x GM301. $ $ Parameters gotten directly from the planetary ephemeris file: $ $ The values in DE403 are: $ $ AU = 0.1495978706910000D+09, $ Astronomical Unit. $ C = 0.2997924580000000D+06, $ Speed of light. $ EMRAT = 0.8130058500000000D+02, $ Earth-Moon GM ratio. $ NTSEC = 0.2062648062470964D+06, $ Arc seconds per radian. $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ BEGIN DPTRAJ $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Astrodynamic Constants: $ $ 1) Davies, M. E., et al., "Report of the IAU/IAG/COSPAR Working Group $ on Cartographic Coordinates and Rotational Elements of the Planets $ and Satellites: 1994," Celestial Mechanics and Dynamical Astronomy, $ Vol. 63, 1996, pp. 127-148. $ $ 2) "The Introduction of the Improved IAU System of Astronomical $ Constants, Time Scales and Reference Frame into the Astronomical $ Almanac," Supplement to the Astronomical Almanac, Prepared $ Jointly by the Nautical Almanac Office, U.S. Observatory and $ H.M. Nautical Almanac Office, Royal Greenwich Observatory, 1983. $ $ 3) "Planetary Constants and Models," Mars Observer Project Document $ 642-321, JPL Document D-3444, November 1990. $ $ 4) Standish, E. M., et al., "JPL Planetary and Lunar Ephemerides, $ DE403/LE403", JPL IOM 314.10-127, May 22, 1995. $ $ Planetary radii (km): $ $ These are geometric equatorial radii of the planets. Note that there $ are also 'dynamic' radii used in the oblateness models specified by $ the variable 'ORB' which is independent of the geometric radii, 'RADI'. $ 'RADI' values are taken from Davies, except for Mars which is from the $ USGS model, as referenced by the Mars Project Planetary Constants Document. $ (Radii of planets 5, 6, 7, 8, correspond to a 1 bar surface). $ RADI( 1) = 0.243970D4, RADI( 2) = 0.605180D4, RADI( 3) = 0.637814D4, RADI( 4) = 0.339340D4, $ Mars - USGS model (See ref. 3). RADI( 5) = 0.714920D5, RADI( 6) = 0.602680D5, RADI( 7) = 0.255590D5, RADI( 8) = 0.247640D5, $ RADI( 9) = 0.119500D4, $ Pluto (NOT USED) RADI( 9) = 14.5D0 , $ EROS RADI(10) = 0.696000D6, RADI(11) = 0.173740D4, $ $ Planetary flatness: $ $ These values are calculated from data taken from Davies, except for $ Mars, which is from the USGS model, as referenced by the Mars Project $ Planetary Constants Document. $ $ The flatness factor is the geometric ellipticity of the body, equal $ to the ratio of the difference between the equatorial and polar $ radii to the equatorial radius. $ FLAT(1) = 11*0.0D0, $ Spherical model used for zero values. $ FLAT(3) = 0.003353642D0, $ Earth FLAT(4) = 0.005208300D0, $ Mars - USGS model (See ref. 3). FLAT(5) = 0.064874391D0, $ Jupiter FLAT(6) = 0.097962434D0, $ Saturn FLAT(7) = 0.022927344D0, $ Uranus FLAT(8) = 0.017081246D0, $ Neptune $ $ Gravitational constants -- from ephemeris DE403: $ $ GM( 1) =.2203208048641792D+05, $ GM( 2) =.3248585988264597D+06, $ GM( 3) =.3986004356081032D+06, $ Updated later (gravity model) $ GM( 4) =.4282831425806710D+05, $ Updated later (gravity model) $ GM( 5) =.1267127678577960D+09, $ GM( 6) =.3794062606113727D+08, $ GM( 7) =.5794549007071872D+07, $ GM( 8) =.6836534063879259D+07, $ GM( 9) =.9816008877070042D+03, $ Pluto (not used) GM( 9) = .0009D0, $ EROS $ GM(10) =.1327124400179870D+12, $ GM(11) =.4902799107879768D+04, $ Updated in the gravity field model. $ $ BETREL = 1.0D0, $ Beta relativity parameter. $ GAMREL = 1.0D0, $ Gamma relativity parameter. LREL = 0.0D0, $ Relativity parameter. $ LOVENO(1,0,1) = 132*0.0D0, $ Zero out and initialize love numbers. $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Oblateness model for Earth: $ $ Normalized Zonal, Sectorial & Tesseral harmonic coefficients. $ $ 1) B. D. Tapley, et al., "The JGM-3 Gravity Model," Annales Geophysicae, $ Supplement 1, C192, 1994. $ $ 2) R. S. Nerem, et al., "Gravity Model Development for TOPEX/Poseidon: $ Joint Gravity Models 1 and 2," Journal of Geophysical Research, $ paper number 94JC01376, 1994. $ $ 3) L. A. Cangahuala, et al., "TOPEX/Poseidon Precision Orbit Determination: $ Quick-Look Operations with SLR & GPS Data," Paper AAS 95-368 presented $ at AAS/AIAA Astrodynamics Specialist Conference, Halifax, Nova Scotia, $ Canada, 14-17 August 1995. $ $ An Earth GM value of 398600.4415 km3/s2 is used with the JGM-3 field. $ This value exceeds the DE403 value by 0.005892 km3/s2. $ $ The reference epoch for the J2, C21, S21 values was 01-JAN-1986. $ The following rates on J2, C21, S21 were applied: $ $ J2 rate = -1.16275535D-11 per year $ C21 rate = -1.3D-11 per year $ S21 rate = 1.1D-11 per year $ $ The values for J2, C21, S21 are for an epoch of 06-NOV-1996. $ OBF(1,2) = 'EARTH',8,0,8, $ 8 x 8 field. OBD(2) = 9.24649D5, $ Distance to end oblateness calculations(km). OBR(2) = 6378.1363D0, $ Gravitational equatorial mean radius (km). OBNORM(2) = .TRUE., $ Normalized harmonics. $ GM( 3) = 3.986004415D+5, $ Earth GM value in km3/s2. $ $ Zero out and initialize the harmonic coefficient array: $ OBXJ(1,1) = 15*0.0D0, OBXC(1,1,1) = 64*0.0D0, OBXS(1,1,1) = 64*0.0D0, $ $ The truncated (8x8) JGM-3 geopotential: $ OBXJ(1,1) = .000000000000D+00, OBXJ(2,1) = .484165249330D-03, OBXJ(3,1) = -.957170590888D-06, OBXJ(4,1) = -.539777068357D-06, OBXJ(5,1) = -.686589879865D-07, OBXJ(6,1) = .149671561786D-06, OBXJ(7,1) = -.907229416432D-07, OBXJ(8,1) = -.491180031747D-07, $ OBXC(1,1,1) = .000000000000D+00, OBXS(1,1,1) = .000000000000D+00, OBXC(2,1,1) = -.327998640000D-09, OBXS(2,1,1) = .131459710000D-08, OBXC(2,2,1) = .243926074866D-05, OBXS(2,2,1) = -.140026639759D-05, OBXC(3,1,1) = .203013720555D-05, OBXS(3,1,1) = .248130798256D-06, OBXC(3,2,1) = .904706341273D-06, OBXS(3,2,1) = -.618922846478D-06, OBXC(3,3,1) = .721144939823D-06, OBXS(3,3,1) = .141420398474D-05, OBXC(4,1,1) = -.536243554299D-06, OBXS(4,1,1) = -.473772370616D-06, OBXC(4,2,1) = .350670156459D-06, OBXS(4,2,1) = .662571345943D-06, OBXC(4,3,1) = .990868905774D-06, OBXS(4,3,1) = -.200987354847D-06, OBXC(4,4,1) = -.188481367425D-06, OBXS(4,4,1) = .308848036904D-06, OBXC(5,1,1) = -.627273696977D-07, OBXS(5,1,1) = -.941946321344D-07, OBXC(5,2,1) = .652459102764D-06, OBXS(5,2,1) = -.323334352444D-06, OBXC(5,3,1) = -.451837048088D-06, OBXS(5,3,1) = -.214954193464D-06, OBXC(5,4,1) = -.295123393022D-06, OBXS(5,4,1) = .497414272309D-07, OBXC(5,5,1) = .174831577700D-06, OBXS(5,5,1) = -.669392937249D-06, OBXC(6,1,1) = -.761035804073D-07, OBXS(6,1,1) = .268998189326D-07, OBXC(6,2,1) = .483274721249D-07, OBXS(6,2,1) = -.373815919444D-06, OBXC(6,3,1) = .570209657580D-07, OBXS(6,3,1) = .888947380083D-08, OBXC(6,4,1) = -.862280326198D-07, OBXS(6,4,1) = -.471405112321D-06, OBXC(6,5,1) = -.267112271720D-06, OBXS(6,5,1) = -.536410164664D-06, OBXC(6,6,1) = .950165183386D-08, OBXS(6,6,1) = -.237261478895D-06, OBXC(7,1,1) = .280286522037D-06, OBXS(7,1,1) = .947773178133D-07, OBXC(7,2,1) = .329760227424D-06, OBXS(7,2,1) = .931936968310D-07, OBXC(7,3,1) = .250501526750D-06, OBXS(7,3,1) = -.217320108453D-06, OBXC(7,4,1) = -.275540963074D-06, OBXS(7,4,1) = -.124141512485D-06, OBXC(7,5,1) = .164400381464D-08, OBXS(7,5,1) = .180753352335D-07, OBXC(7,6,1) = -.358842633079D-06, OBXS(7,6,1) = .151778084434D-06, OBXC(7,7,1) = .137951705641D-08, OBXS(7,7,1) = .241285940808D-07, OBXC(8,1,1) = .233337516872D-07, OBXS(8,1,1) = .584992749394D-07, OBXC(8,2,1) = .800706639316D-07, OBXS(8,2,1) = .655185590975D-07, OBXC(8,3,1) = -.192517643314D-07, OBXS(8,3,1) = -.862858365342D-07, OBXC(8,4,1) = -.244358064393D-06, OBXS(8,4,1) = .698570748504D-07, OBXC(8,5,1) = -.254984100103D-07, OBXS(8,5,1) = .890902974946D-07, OBXC(8,6,1) = -.658593538644D-07, OBXS(8,6,1) = .308920641580D-06, OBXC(8,7,1) = .672627018487D-07, OBXS(8,7,1) = .748131967687D-07, OBXC(8,8,1) = -.123970613955D-06, OBXS(8,8,1) = .120441006688D-06, $ $ Love number for Earth: $ $ 1) Global Earth Physics - A Handbook of Physical Constants, $ AGU Reference Shelf 1, American Geophysical Union, 1995. $ $ See the section by Charles F. Yoder (JPL): $ "Astrometric and Geodetic Properties of Earth and the Solar System" $ $ 2) Merit Standard from D. N. Yuan, June 5, 1992. $ LOVENO(2,0,3) = 0.2990D0, LOVENO(2,1,3) = 0.3000D0, LOVENO(2,2,3) = 0.3020D0, LOVENO(3,0,3) = 0.0930D0, LOVENO(3,1,3) = 0.0930D0, LOVENO(3,2,3) = 0.0930D0, LOVENO(3,3,3) = 0.0940D0, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Oblateness model for the Moon: $ $ Normalized Zonal, Sectorial & Tesseral harmonic coefficients. $ $ LUN60D: 60th degree and order lunar gravity field based upon Lunar $ Orbiters I through V and Apollo 15 and 16 subsatellites. $ $ The reference for this gravity field is: $ $ 1) A. S. Konopliv, W. L. Sjogren, R. N. Wimberly, R. A. Cook, and $ V. Alwar, "A High Resolution Lunar Gravity Field and Predicted $ Orbit Behavior," paper AAS 93-622 presented at AAS/AIAA Astrodynamics $ Specialist Conference, Victoria, B.C., Canada, August 16-19, 1993. $ $ A lunar GM value of 4902.797814 km3/s2 is used with the LUN60D field. $ This value is less than the DE403 value by 0.001294 km3/s2. $ $ The harmonic coefficients below are normalized and use an equatorial $ radius for the Moon of 1738.0 km. $ OBF(1,3) = 'MOON',8,0,8, $ 8 x 8 field. OBD(3) = 6.6183D4, $ Distance to end oblateness calculations (km). OBR(3) = 1738.0D0, $ Gravitational equatorial mean radius (km). OBNORM(3) = .TRUE., $ Normalized harmonics. $ GM(11) = 4902.797814D0, $ Moon GM value in km3/s2. $ $ Zero out and initialize the harmonic coefficient array: $ OBXJ(1,2) = 15*0.0D0, OBXC(1,1,2) = 64*0.0D0, OBXS(1,1,2) = 64*0.0D0, $ $ The truncated (8x8) LUN60D potential: $ OBXJ(1,2) = .000000000000D+00, OBXJ(2,2) = .911441850621D-04, OBXJ(3,2) = .311902819637D-05, OBXJ(4,2) = -.307835221987D-05, OBXJ(5,2) = .769368830934D-06, OBXJ(6,2) = -.420247761012D-05, OBXJ(7,2) = -.555725061234D-05, OBXJ(8,2) = -.258213200841D-05, $ OBXC(1,1,2) = .000000000000D+00, OBXS(1,1,2) = .000000000000D+00, OBXC(2,1,2) = -.251087450783D-06, OBXS(2,1,2) = .189247705893D-06, OBXC(2,2,2) = .346584314967D-04, OBXS(2,2,2) = -.105183661563D-06, OBXC(3,1,2) = .264955051975D-04, OBXS(3,1,2) = .543526879871D-05, OBXC(3,2,2) = .143205732800D-04, OBXS(3,2,2) = .481901453019D-05, OBXC(3,3,2) = .123281980475D-04, OBXS(3,3,2) = -.151614566810D-05, OBXC(4,1,2) = -.601000708063D-05, OBXS(4,1,2) = .144154958330D-05, OBXC(4,2,2) = -.756048899234D-05, OBXS(4,2,2) = -.660908653420D-05, OBXC(4,3,2) = -.157205412560D-05, OBXS(4,3,2) = -.134147521823D-04, OBXC(4,4,2) = -.606603204952D-05, OBXS(4,4,2) = .356365436446D-05, OBXC(5,1,2) = -.993581295251D-06, OBXS(5,1,2) = -.409939311978D-05, OBXC(5,2,2) = .430063826944D-05, OBXS(5,2,2) = .121711990315D-05, OBXC(5,3,2) = .902472365556D-06, OBXS(5,3,2) = .850307049372D-05, OBXC(5,4,2) = .276860468026D-05, OBXS(5,4,2) = .552557057068D-07, OBXC(5,5,2) = .322944662780D-05, OBXS(5,5,2) = -.222204702132D-05, OBXC(6,1,2) = .196677219382D-05, OBXS(6,1,2) = -.317395782132D-05, OBXC(6,2,2) = -.416720046585D-05, OBXS(6,2,2) = -.211311689024D-05, OBXC(6,3,2) = -.316953232988D-05, OBXS(6,3,2) = -.376535765877D-05, OBXC(6,4,2) = -.180602664212D-06, OBXS(6,4,2) = -.358296927763D-05, OBXC(6,5,2) = .145132004062D-05, OBXS(6,5,2) = -.103266424334D-04, OBXC(6,6,2) = -.482864333845D-05, OBXS(6,6,2) = .644590137048D-05, OBXC(7,1,2) = .728684437826D-05, OBXS(7,1,2) = -.158503139890D-06, OBXC(7,2,2) = -.100389024426D-05, OBXS(7,2,2) = .285458316571D-05, OBXC(7,3,2) = .287132227683D-06, OBXS(7,3,2) = .217926631287D-05, OBXC(7,4,2) = -.112896199507D-05, OBXS(7,4,2) = .118350939045D-05, OBXC(7,5,2) = .460145803221D-06, OBXS(7,5,2) = .438750435056D-07, OBXC(7,6,2) = -.121628912845D-05, OBXS(7,6,2) = .976728544757D-06, OBXC(7,7,2) = -.164471397816D-05, OBXS(7,7,2) = -.607247211380D-06, OBXC(8,1,2) = .283644952155D-06, OBXS(8,1,2) = .130269495198D-05, OBXC(8,2,2) = .359236596796D-05, OBXS(8,2,2) = .192706617599D-05, OBXC(8,3,2) = -.157578446767D-05, OBXS(8,3,2) = .410590400224D-06, OBXC(8,4,2) = .397422040228D-05, OBXS(8,4,2) = -.614403578567D-06, OBXC(8,5,2) = -.112498071178D-05, OBXS(8,5,2) = .228062269000D-05, OBXC(8,6,2) = -.243673445826D-05, OBXS(8,6,2) = -.370214046613D-06, OBXC(8,7,2) = -.116915198183D-05, OBXS(8,7,2) = .352222836341D-05, OBXC(8,8,2) = -.259980412308D-05, OBXS(8,8,2) = .974066807776D-06, $ $ Love number for the Moon: $ $ 1) Global Earth Physics - A Handbook of Physical Constants, $ AGU Reference Shelf 1, American Geophysical Union, 1995. $ $ See the section by Charles F. Yoder (JPL): $ "Astrometric and Geodetic Properties of Earth and the Solar System" $ $ 2) Ferrari, A. J., et al., "Geophysical Parameters of the Earth-Moon $ System," Journal of Geophysical Research, Vol. 85, pp. 3939-3951. $ LOVENO(2,0,11) = 0.0302D0, $ +/- 0.0012 LOVENO(2,1,11) = 0.0302D0, $ From Ferrari: 0.022 +/- 0.013 LOVENO(2,2,11) = 0.0302D0, $ $ Earth-Moon indirect oblateness: $ IOBF = 1, $ 1 => On, 0 => Off $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Oblateness model for Mars: $ $ Normalized Zonal, Sectorial & Tesseral harmonic coefficients. $ $ The following is the "header" information which was on the original $ gravity coefficient file obtained from Alex Konopliv: $ $ JPL Gravity field MARS50C $ From Viking 1,2 and Mariner 9 data $ $ Alex Konopliv $ Jet Propulsion Laboratory $ ask@krait.jpl.nasa.gov $ (818) 354-6105 $ $ 1) Alexander S. Konopliv, William L. Sjogren, "The JPL Mars Gravity $ Field, Mars50c, Based Upon Viking and Mariner 9 Doppler Tracking $ Data", JPL Publication 95-5, February 1995. $ $ 2) Davies, M. E., et al., "Report of the IAU/IAG/COSPAR Working Group $ on Cartographic Coordinates and Rotational Elements of the Planets $ and Satellites: 1991," Celestial Mechanics and Dynamical Astronomy, $ Vol. 53, 1992, pp. 377-397. $ $ The following paragraphs from the above reference describe some of $ the parameters used in the gravity field generation. $ $ The International Astronomical Union (IAU) 1991 (Davies et al., $ 1992) rotational constants specified the orientation of Mars and, $ hence, the gravity field. The JPL DE200 planetary ephemeris $ (Standish, 1990) was used for calculation of the planetary point $ mass perturbations. The MAR027 Phobos and Deimos satellite ephemeris $ covered the Viking data time span for the calculation of the point $ mass accelerations of Phobos and Deimos on the spacecraft, but no $ forces on Mariner 9 were included due to Phobos and Deimos. MAR027 $ is a fit of the observations of Phobos and Deimos to the Sinclair/Morley $ theory. $ $ For the Doppler observables, averaged seasonal troposphere $ calibrations as given by Chao (1972) were applied. Any observations $ below 10-degrees elevation were deleted because of unmodeled troposphere $ effects. Daily UT1 and polar motion values from the JPL Space91 $ solution (Gross, 1992) were included and DSN station locations are $ in the International Earth Rotation Service (IERS) reference frame $ as given by Folkner (1991) with the AMO-2 plate motion model and $ solid-Earth tides corrections added. Ideally, future solutions will $ include the frame tie rotational offset between the IERS and planetary $ ephemeris frames, solve for the Mars ephemeris, or use an ephemeris $ such as DE400 in the radio frame. $ $ Planetary constants related to the gravity field: $ $ The following are the ODP Mars rotational parameters namelist inputs $ which are consistent with the Mars50c gravity field. They are from the $ 1991 IAU/IAG/COSPAR working group report on coordinates and rotational $ elements. $ $ Size of gravity field to activate in trajectory calculations: $ OBF(1,1) = 'MARS',8,0,8, $ Truncated to an 8 x 8 field. $ $ Distance within which oblateness calculations begin (km): $ OBD(1) = 5.77232D5, $ $ Gravitational equatorial mean radius (km): $ OBR(1) = 3394.2D0, $ $ Mars GM associated with gravity field (km3/s2): $ Note: This value may overwrite, or be overwritten by, the values on $ the planetary or satellite ephemeris files. $ GM( 4) = 42828.370371D0, $ $ Are the spherical harmonics normalized or unnormalized: $ OBNORM(1) =.TRUE., $ Normalized harmonics $ $ Zero out and initialize the harmonic coefficient array: $ OBAJ(1) = 50*0.0D0, OBAC(1,1) = 2500*0.0D0, OBAS(1,1) = 2500*0.0D0, $ $ Zonal harmonics (normalized): $ OBAJ(1) = .000000000000D+00, OBAJ(2) = .875919760273D-03, OBAJ(3) = .119340679166D-04, OBAJ(4) = -.515052493229D-05, OBAJ(5) = .182402897065D-05, OBAJ(6) = -.145665966143D-05, OBAJ(7) = -.840128810448D-06, OBAJ(8) = -.498316049196D-06, $ $ Sectorial & Tesseral harmonic coefficients (normalized): $ $ OBAC & OBAS are stored on the GIN file as OBACS. $ OBAC(1,1) = .000000000000D+00, OBAS(1,1) = .000000000000D+00, OBAC(2,1) = .132033468405D-07, OBAS(2,1) = .675285290457D-09, OBAC(2,2) = -.843122022711D-04, OBAS(2,2) = .496785329690D-04, OBAC(3,1) = .386567700057D-05, OBAS(3,1) = .252774247650D-04, OBAC(3,2) = -.159257903505D-04, OBAS(3,2) = .846687289437D-05, OBAC(3,3) = .354141266874D-04, OBAS(3,3) = .251996626619D-04, OBAC(4,1) = .423920765688D-05, OBAS(4,1) = .374755584188D-05, OBAC(4,2) = -.111646822443D-05, OBAS(4,2) = -.896339096830D-05, OBAC(4,3) = .651418723273D-05, OBAS(4,3) = -.272352421181D-06, OBAC(4,4) = .113002982991D-06, OBAS(4,4) = -.128953895406D-04, OBAC(5,1) = .483319737757D-06, OBAS(5,1) = .209711155235D-05, OBAC(5,2) = -.424950879878D-05, OBAS(5,2) = -.122480912838D-05, OBAC(5,3) = .330314698123D-05, OBAS(5,3) = .254191256762D-06, OBAC(5,4) = -.468758582735D-05, OBAS(5,4) = -.332592263843D-05, OBAC(5,5) = -.442180487607D-05, OBAS(5,5) = .383605422433D-05, OBAC(6,1) = .189292146731D-05, OBAS(6,1) = -.162575855711D-05, OBAC(6,2) = .952881708647D-06, OBAS(6,2) = .161247203944D-05, OBAC(6,3) = .951313518098D-06, OBAS(6,3) = .244050571795D-06, OBAC(6,4) = .103496966548D-05, OBAS(6,4) = .265185330216D-05, OBAC(6,5) = .178175240614D-05, OBAS(6,5) = .162897120977D-05, OBAC(6,6) = .278529844665D-05, OBAS(6,6) = .785346403849D-06, OBAC(7,1) = .114392658047D-05, OBAS(7,1) = -.121424715130D-06, OBAC(7,2) = .279913674214D-05, OBAS(7,2) = -.731916050571D-06, OBAC(7,3) = .840389648008D-06, OBAS(7,3) = -.423723215581D-06, OBAC(7,4) = .239819519371D-05, OBAS(7,4) = -.525983697776D-06, OBAC(7,5) = -.308772049354D-06, OBAS(7,5) = -.133474272819D-05, OBAC(7,6) = -.572301952896D-06, OBAS(7,6) = -.193627126643D-05, OBAC(7,7) = .419198548050D-06, OBAS(7,7) = -.177122313587D-05, OBAC(8,1) = .202856025184D-06, OBAS(8,1) = .626151101085D-06, OBAC(8,2) = .166759972810D-05, OBAS(8,2) = .659128506006D-06, OBAC(8,3) = -.108712385793D-05, OBAS(8,3) = -.132729727828D-05, OBAC(8,4) = .162651101420D-05, OBAS(8,4) = .415430115159D-07, OBAC(8,5) = -.279554256497D-05, OBAS(8,5) = -.162629432881D-05, OBAC(8,6) = -.100692473264D-05, OBAS(8,6) = -.176741453509D-05, OBAC(8,7) = -.493709063200D-06, OBAS(8,7) = .165618103486D-05, OBAC(8,8) = -.306068555105D-06, OBAS(8,8) = -.263871691654D-06, $ $ Love number for Mars: $ $ 1) Global Earth Physics - A Handbook of Physical Constants, $ AGU Reference Shelf 1, American Geophysical Union, 1995. $ $ See the section by Charles F. Yoder (JPL): $ "Astrometric and Geodetic Properties of Earth and the Solar System" $ $ These values are based on a planetary (Mars) structure model: $ LOVENO(2,0,4) = 0.1400D0, LOVENO(2,1,4) = 0.1400D0, LOVENO(2,2,4) = 0.1400D0, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Resonant harmonics: $ $ This model may be used to input (and solve for) harmonic terms higher than $ the gravity field specified -- e.g. for harmonics which may be large due $ to gravity field resonance. $ $ For example, suppose one was using a 20x20 gravity field (defined in OBF), $ and there should be gravity resonance at this orbit around the 51st $ harmonic order. One may set: $ $ RESNAM(1) = '4J51', 4C51_50', $ $ and input the appropriate nominal values in RESJCS. $ These parameters may also be estimated using the usual naming convention $ for gravity harmonic partials. $ RESNAM( 1) = 20*' ', RESJCS( 1) = 20*0.0D0, $ $ Lumped sum gravity parameters: $ $ This model allows one to generate a partial (LSGM?) for a lumped sum $ gravity field: $ $ LSGMD = d/dJi(dr/dtdt) * DELJi + d/dJi(dr/dtdt) * DELCnm $ $ The partial is specified by the user inputting values for the DELJi, $ DELCnm, DELSnm for use in the above equation, through the GIN inputs $ DELJ(i), DELC(i,j), DELS(i,j). $ $ NOTE: This model has no effect on the trajectory. It just defines how $ to compute a partial. One cannot iterate on the estimated value $ for LSGMD. Therefore its usefulness is very limited. It was put $ into the ODP at the request of section 335(?) for study purposes. $ $ The DELC & DELS parameters are stored in the GIN file as DELCS. $ DELJ(1) = 50*0.0D0, DELC(1,1) = 2500*0.0D0, DELS(1,1) = 2500*0.0D0, DELRES(1) = 20*0.0D0, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Coordinate transformation data: $ $ For precession values (J2000 coordinate transformation): $ $ 1) J. H. Lieske et al, "Expressions for the Precession Quantities $ Based Upon the IAU (1976) System of Astronomical Constants", $ Table 5, Astronomy & Astrophysics, Vol. 58, 1977. $ $ 2) J. H. Lieske, 'Precession Matrix Based on IAU (1976) System of $ Astronomical Constants," Astronomy & Astrophysics, Vol. 73, $ pp. 282-284, 1979. $ $ For obliquity values: $ $ 3) The Astronomical Almanac for the Year 1996, Page B18. $ Units (C=Century): ', '/C, '/(C**2), '/(C**3) $ $ For sidereal values: $ $ 4) T. D. Moyer, "Proposed Changes to ODP Transformation Between $ Body-Fixed and Space-Fixed Coordinates for the Planets and $ the Sun," JPL EM 314-271, June 16, 1982. $ $ For north pole & prime meridian directions: $ $ 5) Davies, M. E., et al., "Report of the IAU/IAG/COSPAR Working Group $ on Cartographic Coordinates and Rotational Elements of the Planets $ and Satellites: 1994," Celestial Mechanics and Dynamical Astronomy, $ Vol. 63, 1996, pp. 127-148. $ $ Coefficients for Earth precession polynomials: $ PRECES(1,1) = 2306.2181D0, 0.301880D0, 0.017998D0, $ ZETA(A) 2004.3109D0, -0.426650D0, -0.041833D0, $ THETA(A) 2306.2181D0, 1.094680D0, 0.018203D0, $ Z(A) $ OBLQTY(1) = 84381.45000D0, -46.81500D0, -0.00060D0, 0.00181D0, $ $ Coefficients for Earth mean sidereal time polynomials: $ SIDERL(1) = 67310.54841D0, 3.164400184812866D9, 0.093104D0, -0.620D-5, $ $ Interpolate the Earth's nutation from the planetary ephemeris: $ (.TRUE. => compute values) $ NUTCMP = .FALSE., $ $ If NUTCMP is TRUE, set the following parameters: $ NFUND( 1, 1) = 20*0.0D0, NUTAMP(1,1,1) = 424*0.0D0, NUTARG( 1, 1) = 530*0, $ $ North pole and prime meridian direction of the planets and Sun. $ The sets of 'PLCOF's below mean the following: $ $ 1,1 RA of mean North Pole at January 1.5, 2000 in EME2000, degrees. $ 2,1 RA DOT, same epoch as above, degree/Julian century. $ 1,2 DEC of mean North Pole at January 1.5, 2000 in EME2000, degrees. $ 2,2 DEC DOT, same epoch as above, degree/Julian century. $ 1,3 Angle from the ascending node to planet prime meridian, degrees. $ 2,3 Mean sidereal rotation rate, degree/day. $ PLREF(1) = 9*0.0D0, $ Seconds past the reference epoch for PLCOF. PLCOF(1,1,1) = 54*0.D0, $ Initialize 2x3x9 array $ PLCOF(1,1,1) = 281.01D0, $ Mercury PLCOF(2,1,1) =-0.033D0, PLCOF(1,2,1) = 61.450D0, PLCOF(2,2,1) =-0.005D0, PLCOF(1,3,1) = 329.68D0, PLCOF(2,3,1) = 6.1385025D0, $ PLCOF(1,1,2) = 272.76D0, $ Venus PLCOF(2,1,2) = 0.0D0, PLCOF(1,2,2) = 67.16D0, PLCOF(2,2,2) = 0.0D0, PLCOF(1,3,2) = 160.20D0, PLCOF(2,3,2) =-1.4813688D0, $ PLCOF(1,1,3) = 317.681D0, $ Mars PLCOF(2,1,3) =-0.108D0, PLCOF(1,2,3) = 52.886D0, PLCOF(2,2,3) =-0.061D0, PLCOF(1,3,3) = 176.901D0, PLCOF(2,3,3) = 350.8919830D0, $ PLCOF(1,1,4) = 268.05D0, $ Jupiter PLCOF(2,1,4) =-0.009D0, PLCOF(1,2,4) = 64.49D0, PLCOF(2,2,4) = 0.003D0, PLCOF(1,3,4) = 284.95D0, PLCOF(2,3,4) = 870.5360000D0, $ PLCOF(1,1,5) = 40.589D0, $ Saturn PLCOF(2,1,5) =-0.036D0, PLCOF(1,2,5) = 83.537D0, PLCOF(2,2,5) =-0.004D0, PLCOF(1,3,5) = 38.90D0, PLCOF(2,3,5) = 810.7939024D0, $ PLCOF(1,1,6) = 257.311D0, $ Uranus PLCOF(2,1,6) = 0.0D0, PLCOF(1,2,6) =-15.175D0, PLCOF(2,2,6) = 0.0D0, PLCOF(1,3,6) = 203.81D0, PLCOF(2,3,6) =-501.1600928D0, $ PLCOF(1,1,7) = 299.36D0, $ Neptune (trigonometric terms ignored) PLCOF(2,1,7) = 0.0D0, PLCOF(1,2,7) = 43.46D0, PLCOF(2,2,7) = 0.0D0, PLCOF(1,3,7) = 253.18D0, PLCOF(2,3,7) = 536.3128492D0, $ $ PLCOF(1,1,8) = 313.02D0, $ Pluto (NOT USED) $ PLCOF(2,1,8) = 0.0D0, $ PLCOF(1,2,8) = 9.09D0, $ PLCOF(2,2,8) = 0.0D0, $ PLCOF(1,3,8) = 236.77D0, $ PLCOF(2,3,8) = -56.3623195D0, $ PLCOF(1,1,8) = 313.02D0, $ Eros PLCOF(2,1,8) = 0.0D0, PLCOF(1,2,8) = 9.09D0, PLCOF(2,2,8) = 0.0D0, PLCOF(1,3,8) = 167.18D0, $ W(J2000.0), deg, 11/25/98 PLCOF(2,3,8) = 1639.392193D0, $ Wdot (deg/day), 11/25/98 $ PLCOF(1,1,9) = 286.13D0, $ Sol PLCOF(2,1,9) = 0.0D0, PLCOF(1,2,9) = 63.87D0, PLCOF(2,2,9) = 0.0D0, PLCOF(1,3,9) = 84.10D0, PLCOF(2,3,9) = 14.1844000D0, $ $ North pole and prime meridian direction of the Moon. There are $ additional terms in the model which are not implemented in ODP. $ LUNREF = 0.0D0, $ The reference epoch is J2000. $ LUNCOF(1,1) = 269.9949D0, $ RA, constant term LUNCOF(2,1) = 0.0031D0, $ RA, linear term LUNCOF(3,1) = 0.0D0, $ RA, quadratic term LUNCOF(4,1) = -3.8787D0, $ RA, coefficient of SIN(E1) LUNCOF(5,1) = -0.1204D0, $ RA, coefficient of SIN(E2) LUNCOF(6,1) = 0.0700D0, $ RA, coefficient of SIN(E3) LUNCOF(7,1) = -0.0172D0, $ RA, coefficient of SIN(E4) LUNCOF(8,1) = 0.0D0, $ RA, coefficient of SIN(E5) $ LUNCOF(1,2) = 66.5392D0, $ DEC, constant term LUNCOF(2,2) = 0.013D0, $ DEC, linear term LUNCOF(3,2) = 0.0D0, $ DEC, quadratic term LUNCOF(4,2) = 1.5419D0, $ DEC, coefficient of COS(E1) LUNCOF(5,2) = 0.0239D0, $ DEC, coefficient of COS(E2) LUNCOF(6,2) = -0.0278D0, $ DEC, coefficient of COS(E3) LUNCOF(7,2) = 0.0068D0, $ DEC, coefficient of COS(E4) LUNCOF(8,2) = 0.0D0, $ DEC, coefficient of COS(E5) $ LUNCOF(1,3) = 38.3213D0, $ W, constant term LUNCOF(2,3) = 13.17635815D0,$ W, linear term LUNCOF(3,3) = 0.0D0, $ W, quadratic term LUNCOF(4,3) = 3.5610D0, $ W, coefficient of SIN(E1) LUNCOF(5,3) = 0.1208D0, $ W, coefficient of SIN(E2) LUNCOF(6,3) = -0.0642D0, $ W, coefficient of SIN(E3) LUNCOF(7,3) = 0.0158D0, $ W, coefficient of SIN(E4) LUNCOF(8,3) = 0.0252D0, $ W, coefficient of SIN(E5) $ LUNCF2(1,1) = 125.045D0, $ E1, constant term LUNCF2(2,1) = -0.0529921D0, $ E1, linear term LUNCF2(3,1) = 0.0D0, $ E1, quadratic term $ LUNCF2(1,2) = 250.089D0, $ E2, constant term LUNCF2(2,2) = -0.1059842D0, $ E2, linear term LUNCF2(3,2) = 0.0D0, $ E2, quadratic term $ LUNCF2(1,3) = 260.008D0, $ E3, constant term LUNCF2(2,3) = -13.0120009D0,$ E3, linear term LUNCF2(3,3) = 0.0D0, $ E3, quadratic term $ LUNCF2(1,4) = 176.625D0, $ E4, constant term LUNCF2(2,4) = 13.3407154D0, $ E4, linear term LUNCF2(3,4) = 0.0D0, $ E4, quadratic term $ LUNCF2(1,5) = 357.529D0, $ E5, constant term LUNCF2(2,5) = -0.9856003D0, $ E5, linear term LUNCF2(3,5) = 0.0D0, $ E5, quadratic term $ $ Phobos and Deimos RA, DEC and W angle data: $ MSREF( 1) = 0.0D0, 0.0D0, $ Reference epochs are J2000. $ MSCOF(1,1,1) = 317.68D0, -0.108D0, 0.0D0, $ RA 1.79D0, 0.0D0, 0.0D0, 0.0D0, 0.0D0, MSCOF(1,2,1) = 52.90D0, -0.061D0, 0.0D0, $ DEC -1.080D0, 0.0D0, 0.0D0, 0.0D0, 0.0D0, MSCOF(1,3,1) = 35.06D0, 1128.8445850D0, 0.66443D-08, $ W -1.42D0, -0.78D0, 0.0D0, 0.0D0, 0.0D0, $ MSCF2(1,1,1) = 169.51D0, 0.435764D0, 0.0D0, $ M1 192.93D0, 1128.4096700D0, 6.644300993057D-09,$ M2 53.47D0, -0.0181510D0, 0.0D0, $ M3 $ MSCOF(1,1,2) = 316.65D0, -0.108D0, 0.0D0, $ RA 0.0D0, 0.0D0, 2.98D0, 0.0D0, 0.0D0, MSCOF(1,2,2) = 53.52D0, -0.061D0, 0.0D0, $ DEC 0.0D0, 0.0D0, -1.78D0, 0.0D0, 0.0D0, MSCOF(1,3,2) = 79.41D0, 285.161897D0, -0.389783D-09, $ W 0.0D0, 0.0D0, -2.58D0, 0.19D0, 0.0D0, $ MSCF2(1,1,2) = 169.51D0, 0.435764D0, 0.0D0, $ M1 192.93D0, 1128.40967D0, 6.644300993057D-09, $ M2 53.47D0, -0.018151D0, 0.0D0, $ M3 143.47D0, -0.018151D0, 0.0D0, $ M3 + 90 $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Perturbing bodies: $ PERB( 1) = 11*1, $ Newtonian point masses for planets, Sun & Moon. PERB( 5) = 2, $ Turns on relativistic influence of Jupiter. PERB(10) = 2, $ Turns on relativistic influence of Sun. $ SAPERB(1) = 22*0, $ Satellite perturbations are OFF $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Initial conditions: $ CENT = 'SUN' $ The ICs will be Sun centered. GEOFRM = .FALSE., $ Use the solar system barycenter reference frame. PLANET = 'YES', $ NO => Barycentric ; YES => Planet centered. $ $ When Earth is center, 'PLANET' is always 'YES', i.e., the PLANET flag $ doesn't affect the Earth state vector. In the Earth-Moon system it is $ always Earth centered regardless of the PLANET flag. $ $ Input coordinate system for ICs: $ IEQX = '2000', IMES = 'CARTES', IXAX = 'SPACE', IZAX = 'EARTH','MEAN','EQUATO', $ $ Output coordinate system: $ OCEN = 'SUN', OEQX = '2000', OMES = 'CARTES', OXAX = 'SPACE', OZAX = 'EARTH','MEAN','EQUATO', $ $ Print rotation matrices/angles when transforming ICs: $ GINBUG = .TRUE., $ $ Note: these initial conditions are given as an example only. $ $ ITIM = '12-FEB-1998 00:00:00.00000 ET', IC(1) = -1.21614904748071700D+08, $ X (km) IC(2) = 8.11510855294633360D+07, $ Y IC(3) = 2.43586850288667380D+07, $ Z IC(4) = -2.03601424696443870D+01, $ X DOT (km/s) IC(5) = -2.20724287414060070D+01, $ Y DOT IC(6) = -1.56541767565315690D+01, $ Z DOT TEND = '01-MAR-1998 00:00:00.0000 ET', $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Integration control: $ PVBUG(1) = 0, $ No acceleration or A matrix printout is requested. PVBUG(2) = 0, $ Stop PV debug print at the trajectory end. PVBUG(3) = 1, $ Print S/C block parameters for antenna pointing $ events, solar panel tilt change events and for $ start & end of finite motor burns. PVBUG(4) = 0, $ Standard diagnostic print. MAKEPV = .TRUE., $ A P/PV file is written out (on 16). RUNOUT = -1, $ Terminate post convergence on time or radius, $ whichever comes first. $ $ Spheres of influence (km): $ (Inside this radius, PVDRIVE switches center of integration. For Mathilde, $ we want this to remain the Sun) $ RSPH( 1) = 1.1241000D5, RSPH( 2) = 6.1626900D5, RSPH( 3) = 9.2464900D5, RSPH( 4) = 5.7723200D5, RSPH( 5) = 4.8208797D7, RSPH( 6) = 5.4563002D7, RSPH( 7) = 5.1744166D7, RSPH( 8) = 8.6626753D7, $ RSPH( 9) = 3.2995530D6, $ Pluto (NOT USED) RSPH( 9) = 0.0D0, $ Eros RSPH(10) = 0.0D0, $ Placeholder for Sun (not used) RSPH(11) = 6.6183000D4, $ $ The above spheres of influence were calculated using a formula attributed $ to Laplace. It's derivation can be found in Richard Battin's book: $ $ "An Introduction to the Mathematics and Methods of Astrodynamics" $ $ chapter 8, pages 395-398. The GMs used were from DE403. $ $ The traditional values: $ $ RSPH( 1) = 0.5D6, 2.5D6, 2.5D6, 2.0D6, 5.0D7, 5.0D7, $ 5.0D7, 8.0D7, 4.0D7, 0.0D0, 4.0D4, $ $ Integration independent variable: $ BASE0 = .TRUE., $ $ BASE0 = .TRUE. sets the independent variable to seconds past the trajectory $ epoch. This is the default and recommended value. Fred Krogh says that $ this will be better for the integrator. $ $ BASE0 = .FALSE. sets the independent variable to seconds past the reference $ epoch. If an old GIN file is converted to a new one using GINCONVERT, $ BASE0 is set to .FALSE., which is consistent with the old integrator. $ $ State equation tolerance; local absolute integration error (km/sec): $ EPS = 1.0D-11, $ $ Voyager NAV: EPS = 1.0D-9 $ Magellan: EPS = 1.0D-9 $ Galileo NAV: EPS = 1.0D-9 $ Ulysses NAV: EPS = 1.0D-9 $ TOPEX PVT: EPS = 7.0D-13 $ MGS NAV: EPS = 1.0D-10 $ NEAR NAV: EPS = 1.0D-9 (1.D-11 in lock-file) $ $ Tolerance for variational equations (recommended value): $ EPSV = 1.0D12, $ $ Scale factors for EPSV: $ EPSCAL(1) = 200*1.0D0, $ $ If EPSCAL = 0.0D0, the ODP uses EPSCAL = 1.0D0. $ If MASCONS are included in the partials list, set the EPSCAL factors for $ them at 1.0D0 for disk and point, and 1.0D-5 for curved mascons. $ For flat mascons, 1.0D5 is maximum! $ $ Maximum step size in seconds (5 days): $ HMAX = 432000.0D0, $ $ Minimum step size in seconds: $ HMIN = 0.005D0, $ $ Integration restarts: $ RESTRT(1) = .FALSE., $ No restart for shadow events. RESTRT(2) = .FALSE., $ No restart for attitude change events. RESTRT(3) = .FALSE., $ No restart for small force events. RESTRT(4) = .FALSE., $ No restart in the exponential atmosphere model. $ $ Termination control DISABLED for EROS: $ DRVL = 0.0D0, $ Begin testing for closest approach (km). DRBD = 'PLUTO', $ Terminate integration 'TMPC' secs after cl appr. TMPC = 9.999D99, $ Do NOT stop integrating after cl appr to DRBD. RVAL = 0.0D0, $ Radius (km) at which to end the integration. RBOD = 'PLUTO', $ Terminate integration at radius 'RVAL' from RBOD. $ $ Trajectory end time: $ TEND = '01-MAR-1999 00:00:00.0000 ET', $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Spacecraft mass: $ MASS = 800.72257, $ Mass of S/C (kg) (1997 Jun 12 16:23 gin file) $ $ (tube://usr2/nnav/mirage/solns/tcm5_n0c/gin16152.nio $ $ Historical: $ MASS = 804.57, $ NEAR injection mass minus 1kg de-spin yo-yo's $ (Larry Mosher 2/1/96) $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Solar radiation pressure (SRP) model: $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Zero out and initialize the SRP & orientation model parameters: $ ACANO(1,1) = 120*-1.0D30, $ Inertial reference direction. ANGL = 0.0D0, $ Angle about the Sun-S/C axis. ANGLS(1,1) = 600*0.0D0, $ Euler rotation angles. COMP(1) = 10*' ', $ Component type declarations (i.e. sphere). CSIZE(1,1) = 20*0.0D0, $ Component dimensions. DELFM(1,1) = 30*0.0D0, $ Effective area change increments. DUPRC(1,1,1) = 6000*0.0D0, $ Component orientation definitions. DUPRS(1,1) = 600*0.0D0, $ Direction of the S/C Z* axis. GANG(1) = 36*0.0D0, $ Antenna model: theta angles for GCO & GCOP. GCO(1,1) = 180*0.0D0, $ Antenna model: integral tables. GCONO(1) = 2*0, $ Antenna model: Chebyshev polynomial degree. GCOP(1,1) = 90*0.0D0, $ Antenna model: integral tables. ITDFC(1,1) = 1000*' ', $ Reflectivity degradation change epochs. $ or use: TDFC(1,1) = 1000*-1.0D30 ITDFM(1) = 10*' ', $ Effective area change epochs. $ or use: TDFM(1) = 10*-1.0D30 KMNC(1,1,1) = 4000*1.0D0, $ Component reflectivity degradation factors. REFBS(1,1) = 400*' ', $ Reference direction to compute X* & Y*. SCOFC(1,1) = 40*0.0D0, $ Component reflectivity coefficients. STABLE(1) = 2*0, $ Transformations of the S/C X*, Y*, Z* axes. TABVAL(1,1) = 200*0.0D0, $ Rotation angles applied in STABLE. TCANO(1) = 40*' ', $ Start time for ACANO interval. $ or use: DTCANO(1) = 40*-1.0D30 TUPRS(1) = 200*' ', $ S/C orientation change epochs. $ or use: DTUPRS(1) = 200*-1.0D30 UPRC(1,1) = 2000*' ', $ S/C component orientation reference. UPRS(1) = 200*' ', $ Direction of the S/C Z* axis. $ $ Other parameters required for the SRP model: $ $ GCOFL, MASS, MASDEC, P0A, P1A, REFB, SC, SHDFLG, SRPFLG, TTYPE, USECMP $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Activate the solar radiation pressure model: $ SRPFLG = .TRUE., SHDWFL = 0, $ 0 -> shadow model with integration restarts. $ 1 -> shadow model without restarts. SOLCOF = 1.0D0, $ General SRP scale factor. SOLSCL(1) = 10*1.0D0, $ Spacecraft component scale factors. $ ICMPTM( 1) = '01-FEB-1996 00:00:00 ET', ICMPTM( 2) = '01-MAR-1999 00:00:00 ET', $ $ No mass decrements are applied & all specified components are used: $ MASDEC( 1) = 0.0D0, USECMP(1,1) = 1,2,3,4,5, $ MASDEC( 2) = 0.0D0, USECMP(1,2) = 1,2,3,4,5, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Solar flux at 1 AU (kgkm3/m2s2): $ $ SC = (L*d*d/c) * (1000 m/km) * (1 km^3 / (1000 m)^3 ) where $ L = luminosity at 1 AU (1369 W/m^2) (1 W = 1 kg m^2/s^3 ) $ d = 149.6 Mkm/AU = 149597870.691 km/AU $ c = light speed = 299792.458 km/s $ $ SC = 1.020506244D8, $ MGS/TOPEX/Poseidon value: L = 1367.053608 W/m2 $ SC = 1.032200000D8, $ Magellan and PVO value. $ SC = 1.013048D8, $ NEAR NAV value SC = 1.01994367581D8, $ L=1366.3 W/m2 (6/97), S. Dewitte, DIARAD/VIRGO/SOHO $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ S/C component definitions: $ $ The following S/C components are all fixed in the ODP's S/C coordinate $ system: $ $ X* ---> NEAR spacecraft X-axis $ Y* ---> NEAR spacecraft Y-axis $ Z* ---> NEAR spacecraft Z-axis $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ NEAR S/C components & properties updated with JPL IOM 312.B-95-682 values. $ COMP(1)='ANTENNA', $ High gain CSIZE(1,1)=0.233D0, $ ... depth (m) CSIZE(2,1)=0.86027349D0, $ ... radius (m) SCOFC(1,1)=0.0375, 0.0D0, $ ... spec (fr & bk) 0.258333D0, 0.0D0, $ ... diff (fr & bk) $ COMP(2)='FLAT PLATEF', $ Front of solar panels CSIZE(1,2)=8.92D0, $ ... area (m^2) SCOFC(1,2)=0.05625D0, 0.0408333D0, $ ... spec & diff $ COMP(3)='FLAT PLATEB', $ Back of solar panels CSIZE(1,3)=8.92D0, $ ... area (m^2) SCOFC(1,3)=0.0375D0, 0.258333D0, $ ... spec & diff $ COMP(4)='FLAT PLATEF', $ Backside of s/c bus CSIZE(1,4)=2.33D0, $ ... area (m^2) SCOFC(1,4)=0.0375D0, 0.258333D0, $ ... spec & diff $ COMP(5)='CYLINDER', $ S/C body CSIZE(1,5)=1.452D0, $ ... length (m) CSIZE(2,5)=0.778D0, $ ... radius (m) SCOFC(1,5)=0.0295D0, 0.2316667D0, $ ... spec & diff $ $ Chebyshev transformation parameters: $ $ Note that the numerical integral tables -- GCO & GCOP & GANG -- were $ calculated for the NEAR high gain antenna. They were calculated from $ the ODP Utility program "ANTTAB" written by Rick Sunseri. $ $ radius= 0.86027349 m, depth= 0.233 m $ (omega= arctan(2*depth/radius)) $ $ P0A If the angle between the antenna pointing direction and $ the spacecraft-Sun direction is less than P0A, then the $ antenna front is under full illumination (deg) $ $ P1A If the angle between the antenna pointing direction and $ the spacecraft-Sun direction is between P1A and 180 $ degrees, then the antenna back is under full illumination $ (deg) $ P0A = 61.556118, $ Angle limit between full/partial front illumination. P1A = 118.44389 , $ Angle limit between full/partial back illumination. $ GCOFL = 1, $ GCO, GCOP tables are Chebyshev polynomial coefficients. GCONO = 12, 7, $ Polynomial degree for back (GCO) & front (GCOP). $ $ Backside: $ The first two rows below equal (P1A+P0A)/2, (P1A-P0A)/2. $ $ I21 I22 I31 I32 I33 GCO(1,1) = 0.90000000E+02, 0.90000000E+02, 0.90000000E+02, 0.90000000E+02, 0.90000000E+0 0.28443884E+02, 0.28443884E+02, 0.28443884E+02, 0.28443884E+02, 0.28443884E+0 -0.26155570E+00,-0.29125383E+00, 0.18434623E+00, 0.16779085E+00, 0.17778791E+0 -0.38103083E+00,-0.38020518E+00, 0.29237321E+00, 0.25141585E+00, 0.24065098E+0 -0.13048425E+00,-0.76069325E-01, 0.14044109E+00, 0.98506585E-01, 0.61787140E-0 -0.38353868E-02, 0.16647017E-01, 0.34320455E-01, 0.13107652E-01,-0.25099039E-0 0.77821305E-02, 0.31406560E-02, 0.79130131E-03,-0.20920534E-02,-0.12092999E-0 0.41518494E-03,-0.20942891E-03,-0.11815116E-02,-0.27759821E-03, 0.77593158E-0 -0.15108149E-03, 0.34480565E-03,-0.46769565E-04, 0.17433082E-04,-0.18146055E-0 0.38328904E-04, 0.12406651E-05, 0.16228323E-04,-0.20481782E-04,-0.12965002E-0 0.15267527E-05, 0.55911853E-04,-0.31315326E-05,-0.88088917E-07,-0.27820495E-0 0.47232952E-05,-0.10664182E-07,-0.12803476E-06,-0.23968007E-05,-0.26717537E-0 -0.10781563E-07, 0.12031040E-04,-0.29109935E-06,-0.22984232E-08,-0.59725503E-0 0.70813815E-06,-0.87677127E-09, 0.16407470E-08,-0.35437390E-06,-0.23237412E-0 -0.25287881E-08, 0.30184353E-05,-0.29843989E-07, 0.19690543E-08,-0.15008067E-0 $ $ Frontside: $ $ I21P I22P I31P I32P I33P GCOP(1,1) = 0.75778061E+02, 0.75778061E+02, 0.75778061E+02, 0.75778061E+02, 0.75778061E+0 0.14221941E+02, 0.14221941E+02, 0.14221941E+02, 0.14221941E+02, 0.14221941E+0 0.37802729E+00, 0.38885963E+00, 0.27412271E+00, 0.24418947E+00, 0.24190886E+0 -0.38505456E+00,-0.36731386E+00,-0.31958723E+00,-0.26198807E+00,-0.23876369E+0 0.63697062E-02,-0.25083797E-01, 0.51728338E-01, 0.19997321E-01,-0.37648750E-0 0.56982721E-03, 0.35894278E-02,-0.60934629E-02,-0.23039875E-02, 0.61530527E-0 0.45956298E-04,-0.99189065E-05,-0.32436440E-03, 0.51315754E-04, 0.48326851E-0 0.73560725E-04,-0.43227799E-04, 0.15717626E-03, 0.68185684E-04,-0.47059081E-0 -0.35789351E-04, 0.54123097E-06, 0.14567665E-05,-0.15404394E-04,-0.12586420E-0 0.39581369E-05, 0.12013402E-05,-0.48121838E-05, 0.11929963E-05,-0.14064504E-0 $ $ Values for the attack angle, theta, corresponding to GCO & GCOP entries. $ Only needed when GCOFL=0 (for linear interpolation) $ $ GANG = $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ S/C attitude definitions: $ ANGL = 0.0D0 $ Angle about Sun-S/C axis. REFB = 'STAR', $ Ref direction is wrt this body ACANO(1,1)= -1.D0, 0.0, 0.0, $ Inertial ref. dir. in xyz EME200 TCANO(1) = '01-JAN-1996 0:00:00.0 ET', $ Beginning of ACANO ref system $ Spacecraft orientation changes occur at specific epochs. TTYPE(1) = 'TIME', TTYPE(2) = ' ' $ $ TUPRS: defines the epoch of the S/C orientation change. $ UPRS: defines the direction in which Z* points. $ REFBS: defines the direction of the reference vector, R. $ R is used to compute X* and Y*: $ Y* = R x Z* $ X* = Y* x Z* = (R x Z*) x Z* $ ANGLS: defines a set of Euler rotations about Z*, X*', Z*'' $ TUPRS(1) = '01-JAN-1996 0:00:00.0 ET', UPRS(1) = 'SUN', $ S/C nom. -> Sun during cruise REFBS(1,1) = 'STAR', ANGLS(1,1) = 0.0D0, 0.0D0, 0.0D0, $ No rotations $ DUPRS(1,1) = 0.0, 0.0, 1.0, $ S/C z-dir (unused; UPRS is body) UPRC(1,1) = 'SC ANG', DUPRC(1,1,1)=0.0D0, 0.0D0, 1.0D0, $ Antenna UPRC(1,2) = 'SC ANG', DUPRC(1,1,2)=0.0D0, 0.0D0, 1.0D0, $ F. solar panel UPRC(1,3) = 'SC ANG', DUPRC(1,1,3)=0.0D0, 0.0D0, 1.0D0, $ B. solar panel UPRC(1,4) = 'SC ANG', DUPRC(1,1,4)=0.0D0, 0.0D0,-1.0D0, $ B. s/c bus UPRC(1,5) = 'SC ANG', DUPRC(1,1,5)=0.0D0, 0.0D0, 1.0D0, $ s/c body $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Reflectivity coefficient degradation model. $ $ Linearly interpolate the degradation factors: $ INDEG = 1, $ $ Degradation intervals and factors for each component: $ ITDFC(1, 1) = '01-JAN-1996 00:00:00 ET', ITDFC(2, 1) = '01-JUN-2000 00:00:00 ET', KMNC(1,1,1) = 1.0D0, 1.0D0, KMNC(1,2,1) = 1.0D0, 1.0D0, $ ITDFC(1, 2) = '01-JAN-1996 00:00:00 ET', ITDFC(2, 2) = '01-JUN-2000 00:00:00 ET', KMNC(1,1,2) = 1.0D0, 1.0D0, KMNC(1,2,2) = 1.0D0, 1.0D0, $ ITDFC(1, 3) = '01-JAN-1996 00:00:00 ET', ITDFC(2, 3) = '01-JUN-2000 00:00:00 ET', KMNC(1,1,3) = 1.0D0, 1.0D0, KMNC(1,2,3) = 1.0D0, 1.0D0, $ ITDFC(1, 4) = '01-JAN-1996 00:00:00 ET', ITDFC(2, 4) = '01-JUN-2000 00:00:00 ET', KMNC(1,1,4) = 1.0D0, 1.0D0, KMNC(1,2,4) = 1.0D0, 1.0D0, $ ITDFC(1, 5) = '01-JAN-1996 00:00:00 ET', ITDFC(2, 5) = '01-JUN-2000 00:00:00 ET', KMNC(1,1,5) = 1.0D0, 1.0D0, KMNC(1,2,5) = 1.0D0, 1.0D0, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Planetary radiation model: $ $ The planetary radiation model accounts for the forces on s/c due to a $ nearby planet's albedo and infrared emissivity. $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Zero out and initialize planetary radiation model parameters: $ RPBOD = ' ', $ Radiating planetary body: NONE $ If no planet is set, the model is off. $ ALBCOF = 1.0D0, $ General albedo scale factor. ALBSCL(1) = 10*1.0D0, $ S/C component area scale factors (albedo). ALCOFC(1,1) = 40*0.0D0, $ CAL(0,0) = 100*0.0D0, $ C(n,m) albedo series coefficient. CEP(0,0) = 100*0.0D0, $ C(n,m) infrared emission series coefficient. EPSIMP = 1.0D-4, $ Relative epsilon of convergence. IFRCOF = 1.0D0, $ General infrared scale factor. IFRSCL(1) = 10*1.0D0, $ S/C component area scale factors (IR). IRCOFC(1,1) = 40*0.0D0, $ LMXAL = 0, $ Degree of the albedo series. LMXEP = 0, $ Degree of the infared emission series. MXSIMP = 5, $ Maximum iterations in the quadrature. NPRING = 0, $ Number of rings in the albedo/IR model. SAL(0,0) = 100*0.0D0, $ S(n,m) albedo series coefficient. SEP(0,0) = 100*0.0D0, $ S(n,m) infrared emission series coefficient. $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ The following example inputs for the Mars albedo model were taken from: $ $ 1) Creel, D. D., "General Inputs for DPTRAJ/ODP Planetary Radiation Model", $ IOM 314.6-1321, August 6, 1991. $ $ RPBOD = 'MARS', $ LMXAL = 7, $ Degree of the albedo series. $ $ CAL(0,0) = 0.294838D0, $ Mars perihelion albedo coefficients. $ CAL(1,0) = 0.046034D0, $ CAL(2,0) = 0.049287D0, $ CAL(3,0) = 0.009035D0, $ CAL(4,0) = 0.031791D0, $ CAL(5,0) =-0.004347D0, $ CAL(6,0) =-0.012938D0, $ CAL(7,0) =-0.012793D0, $ $ CAL(0,0) = 0.231281D0, $ Mars aphelion albedo coefficients. $ CAL(1,0) =-0.040753D0, $ CAL(2,0) = 0.031974D0, $ CAL(3,0) =-0.032247D0, $ CAL(4,0) = 0.021980D0, $ CAL(5,0) =-0.025561D0, $ CAL(6,0) =-0.008054D0, $ CAL(7,0) = 0.005228D0, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Thermal imbalance model: $ THMCMP = .FALSE., $ The thermal imbalance acceleration is off. $ EMISS( 1) = 10*0.0D0, $ S/C component emissivity coefficients. $ FACE( 1) = 10*' ', $ Parameter only used by TOPEX/Poseidon. THAREA( 1) = 10*0.0D0, $ Thermal imbalance S/C component areas. THMCOF(1,1) = 50*0.0D0, $ Thermal coefficients for each component. $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Maneuver and Nongravitational acceleration models: $ $ Zero out and initialize the maneuver & nongrav model parameters: $ $ STABLE(1) = 0, 0, $ TABVAL(1,1) = 200*0.0D0, $ List of times when 'STABLE' events occur. $ SAAT(1,1) = 1998*' ', SAAP(1,1) = 8991*0.0D0, ISTREX(1) = 100*' ', ISTPEX(1) = 100*' ', AR(1) = 100*0.0D0, AX(1) = 100*0.0D0, AY(1) = 100*0.0D0, BB(1) = 100*0.0D0, DELVB1(1) = 99*0.0D0, MB1T(1) = 99*' ', MB1V(1,1) = 297*0.0D0, MB1P(1) = 99*0.0D0, MA1A(1,1) = 990*0.0D0, MA1D(1) = 99*0.0D0, MA1K(1) = 99*0.0D0, MA1F(1,1) = 495*0.0D0, MA1M(1,1) = 396*0.0D0, MA1T(1) = 99*' ', BURN(1) = 99*0, LPLANE(1) = 99*' ', TPEQ(1) = 99*0.0D0, C3(1) = 99*0.0D0, DELV(1) = 99*0.0D0, ISMFTM(1) = 1000*' ', SMFDR(1,1) = 3000*0.0D0, SMFDV(1,1) = 3000*0.0D0, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Quadratic acceleration model: $ $ Start and stop epochs: $ $ SAAT(1,1) = '17-FEB-1996 00:00:00.0000 ET', $ SAAT(2,1) = '01-FEB-1999 00:00:00.0000 ET', $ $ Accelerations (I,J): $ SAAP(1,1) = $ Index I = 1 => acceleration in R (ATAR nominal) $ SAAP(4,1) = $ Index I = 4 => acceleration in X (ATAX nominal) $ SAAP(7,1) = $ Index I = 7 => acceleration in Y (ATAY nominal) $ Index J provides a time table. $ $ Exponential acceleration model: $ $ Start and stop epochs: $ $ ISTREX(1) = '17-FEB-1996 00:00:00.0000 ET', $ ISTPEX(1) = '01-FEB-1999 00:00:00.0000 ET', $ $ Exponent coefficients: $ AR(1) = $ R (GLAR nominal) $ AX(1) = $ X (GLAX nominal) $ AY(1) = $ Y (GLAY nominal) $ BB(1) = $ Time scale factor (GLBT nominal) $ $ Impulsive burn maneuvers: $ BRNCRD(1) = 99*1, $ 1 => delta-V wrt S/C X*,Y*,Z* $ $ MB1T(1) = '02-MAR-1996 00:00:00.0000 UTC', $ $ Delta velocity components: $ DELVB1(1) = $ Burn magnitude (km/s). $ MB1D(1) = $ Burn duration (s). $ MB1V(1,1) = $ Delta-V increments (IDLX,Y,Z nominals $ MB1P(1) = $ Mass decrement (kg). $ $ Finite burn maneuvers: $ ITPEQ(1) = 99*'2000', $ Epoch of burn coordinate system. LPLANE(1) = 99*' ', $ Thrust vector reference system. MA1K(1) = 99*1.0D-03, $ Conversion factors for finite burns. $ COORS(1,1) = ' ','SPACE','EARTH','MEAN','EQUATO', COORS(1,2) = ' ','SPACE','EARTH','MEAN','EQUATO', COORS(1,3) = ' ','SPACE','EARTH','MEAN','EQUATO', COORS(1,4) = ' ','SPACE','EARTH','MEAN','EQUATO', COORS(1,5) = ' ','SPACE','EARTH','MEAN','EQUATO', $ $ The following example inputs were generated from SEPV and used biased $ Mars Mean Equator of Date B-plane targets: $ $ BDOTT = -44000.0 km BDOTR = -52000.0 km +3 hrs in flight time $ $ The thrust and mass flow rate values came from the following: $ $ 1) Dominick, S., "Updated Thrust Levels for Main Engine and Thrusters", $ Lockheed Martin IOM, March 25, 1996. $ $ MA1T(1) = '21-NOV-1996 22:00:00.0000 UTC', $ $ BURN(1) = 1, $ Termination flag (DURAT, DV, C3). $ MA1F(1,1) = 656.0D0, $ Thrust coefficients (kilo-Newtons). $ 4*0.0D0, $ MA1M(1,1) = 0.2107D0, $ Mass flow rate (kg/s). $ 3*0.0D0, $ MA1A(1,1) = 249.6836008603889D0, $ RA coefficients (degree). $ 4*0.0D0, $ MA1A(6,1) = -48.06990205194584D0, $ DEC coefficients (degree). $ 4*0.0D0, $ MA1D(1) = 0.1126066527720419D0, $ Burn duration cutoff (s). $ $ DELV(1) = 0.0D0, $ DV magnitude cutoff. $ ACELC(1,1) = 0.0D0, 0.0D0, 0.0D0, $ Thruster misalign coeffs, DV stop. $ BRD(1) = $ Reference planet, C3 cutoff. $ C3(1) = $ Twice energy per unit mass limit. $ $ Gyro control: $ $ ITVDIL(1) = $ Inertial lock epoch. $ ITVTRN(1) = $ Turn epoch. $ LDYN(1) = $ Thrust vector reference plane flag. $ TVDGDR(1,1) = $ Pitch, Yaw, Roll rates. $ TVDORA(1,1) = $ Turn angles. $ TVDORT(1,1) = $ Turn sequences. $ TVEPS(1,1) = $ Pitch, Yaw, Roll offsets. $ $ Gyro drift: $ IROLLX(1) = 99*0, $ Impulsive burn not under gyros. ROLLAX(1) = 99*0, $ Finite burn not under gyros. $ $ Angular momentum desaturation events: $ $ 1) "NEAR Thruster Location and Utilization Matrix", provided by $ Cliff Helfrich, Aug 14, 1997. $ $ Thruster orientation is in the ODP's s/c X*,Y*,Z* system. $ $ NOTE: No 2b thruster. 3b and 4b fired in pairs at 50%. $ THRSTR(1, 1) = 60*0.0D0, $ THRSTR(1, 1) = 1.000D0, 0.000D0, 0.000D0, $ 1a ( 21 N) THRSTR(1, 2) = 1.000D0, 0.000D0, 0.000D0, $ 2a ( 21 N) THRSTR(1, 3) = 1.000D0, 0.000D0, 0.000D0, $ 3a ( 21 N) THRSTR(1, 4) = 1.000D0, 0.000D0, 0.000D0, $ 4a ( 21 N) THRSTR(1, 5) = 0.000D0, 0.000D0, 1.000D0, $ 5a ( 3.5 N) THRSTR(1, 6) = 0.000D0, 0.000D0, 1.000D0, $ 6a ( 3.5 N) THRSTR(1, 7) = -1.000D0, 0.000D0, 0.000D0, $ 1b ( 3.5 N) THRSTR(1, 8) = -1.000D0, 0.000D0, 0.000D0, $ 3b ( 3.5 N) THRSTR(1, 9) = -1.000D0, 0.000D0, 0.000D0, $ 4b ( 3.5 N) THRSTR(1,10) = 0.000D0, 0.000D0, -1.000D0, $ 5b ( 3.5 N) THRSTR(1,11) = 0.000D0, 0.000D0, -1.000D0, $ 6b ( 3.5 N) THRSTR(1,12) = 1.000D0, 0.000D0, 0.000D0, $ LVA (467 N) $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ TWIST $ $ Standard print control: $ BARYFL = 0, $ Get the barycenter shift vector from: $ 0 => internal computation $ 1 => satellite ephemeris DATAFL = 0, $ Read constants for TWIST from: $ 0 => the P/PV file $ 1 => the GIN file PCBPRT = 2, $ Reference center for TWIST print: $ 0 => use the planet center $ 1 => use the barycenter $ 2 => use both PBUG(1) = 10*0, $ Turn off TWIST debugging print. $ PBUG(3) = 1, for aerobraking data HPEP = 3600.0D0, $ Interval to check trigger (seconds) TPWANT = 'UTC', $ Time listed in ET & UTC. $ $ Print termination control: $ FAPSIS = -1, $ Terminate print at periapsis. CLOS = 'PLUTO', CRBD = 'PLUTO', CRFL = 'INTERN', $ Closest approach testing within 'CRAD'. CRAD = 1.0D8, $ Radius for closest approach test (km). EBOD = 'PLUTO', EDIS = 0.0D0, $ Distance from EBOD to end print (km). ELIS(1) = 5, 6, 4*0, $ Print at time supplied in ETIM. $ ETIM = '31-MAR-2000 00:00:00 ET', $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ The print lists are given below. The arrays PHSTRL(J,I), PHENDL, MOA1, $ etc. are assigned to integers which reference the lists. The index 'I' $ denotes 'PHASE', that part of the trajectory when the body in PCBBOD $ corresponds to the primary body (integration center) of the trajectory. $ $ Phase (integration center) order for the launch & cruise: $ PCBBOD(1) = 'EARTH', 'SUN', 'PLUTO', 2*' ', $ $ Geometric & phase events: $ EQUTXL(1,1) = 30*0, $ Print at equator crossings. NPOLXL(1,1) = 30*0, $ Print at north pole minimum range. PCBCAL(1,1) = 30*0, $ Print at body closest approach. PCBCAL(1,1) = 1, PCBCAL(1,3) = 3, PCBDST(1) = 5*0.0D0, $ Distance for print from PCBBOD(I). PCBDSL(1,1) = 30*0, $ Print lists for PCBDST. PCBGOL(1,1) = 30*0, $ Print at geocentric occultations. PCBGOL(1,1) = 0, PCBGOL(1,2) = 0, PCBGOL(1,3) = 3, ATMRAD( 4) = 25.9D0, $ Mathilde radius + 0 km. PCBSOC(1,1,1) = 150*0, $ Print at star occultations. OCSTAR(1) = 5*' ', $ Star names. STARDC(1) = 5*0.0D0, $ DEC of stars in OCSTAR (degrees). STARRA(1) = 5*0.0D0, $ RA of stars in OCSTAR (degrees). PCBTRG = 0, $ -1 => print at each periapsis. $ 0 => print at apoapsis & periapsis. $ 1 => print at each apoapsis. PHENDL(1,1) = 30*0, $ Print at the phase end. PHSTRL(1,1) = 30*0, $ Print at the phase start. PHSTRL(1,1) = 1, PHSTRL(1,2) = 2, PHSTRL(1,3) = 3, SPOLXL(1,1) = 30*0, $ Print at south pole minimum range. TERMXL(1,1) = 30*0, $ Print at terminator crossings. TANOM(1) = 0.0D0, $ True anomaly value at which to print. TPPERI = 0.0D0, $ Time after periapsis at which to print. PPERI(1) = 6*0, $ Print lists for TANOM and TPPERI. $ $ Physical model & S/C events: $ ATMPR(1,1) = 30*0, $ Print for atmospheric lift & drag. ATPR(1) = 6*0, $ Print for quadratic gas leaks. GLPRT(1) = 6*0, $ Print for exponential gas leaks. MOA1(1) = 6*0, $ Print at finite maneuvers. MOA1(1) = 1, MOB1(1) = 6*0, $ Print at instantaneous maneuvers. MSCOPR(1,1) = 30*0, $ Print for MASCON sphere. OBPRTL(1,1) = 30*0, $ Print for oblateness sphere. OBPRTL(1,1) = 1, OBPRTL(1,2) = 0, OBPRTL(1,3) = 3, PCBSHL(1,1) = 30*0, $ Print for SRP shadowing events. $ $ Absolute epoch print: $ ABSF(1,1) = 60*0, $ Print at epochs in 'ABST'. ABST(1) = 10*' ', $ $ Radius-Delta-Radius (RDR) print: $ PCBRDR(1,1,1) = 75*0.0D0, PCBRDR(1,1,1) = 0.0D0, $ Start radius for RDR print (km). PCBRDR(2,1,1) = 0.0D0, $ Delta radius (increase) (km). PCBRDR(3,1,1) = 0.0D0, $ Stop radius for RDR print (km). PCBRDL(1,1) = 30*0, $ Print lists for RDR events. $ $ Time-Delta-Time (TDT) print: $ PCBTHW(1) = 'ET', $ HAVE time-type for TDT print. IPCBTD(1,1,1) = 150*' ', $ TDT print in phase 'I'. IPCBTD(1,1,1) = ' ', $ Start times for TDT print. IPCBTD(2,1,1) = ' ', $ Delta times. IPCBTD(3,1,1) = ' ', $ Stop times for TDT print. PCBTDL(1,1) = 30*0, $ No default print lists. PCBTDF(1) = 2, $ Phase independent print. $ $ Satellite event print: $ CLOSAT(1) = 10*' ', CLOLSX(1,1) = 7, CLOLSX(1,2) = 8, RADSAT(1) = 5.0D4, 5.0D4, $ Distance to monitor closest approach (km). $ ECLSAT(1) = 10*' ', $ Satellites for eclipse events. OCSATG(1) = 10*' ', $ Satellites for Earth occultations. OCSATH(1) = 10*' ', $ Satellites for Sun occultations. OCSATS(1,1) = 50*' ', $ Satellites for star occultations. TRNSAT(1) = 10*' ', $ Satellites for occultations & transits. CLOLST(1) = 6*0, $ Print lists of OCSATG, OCSATH, OCSTAR. $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Initialize and define the print lists: $ BODCOR(1,1, 1) = 360*' ', BODEQX( 1, 1) = 45*'2000', $ Specifies the coordinate system epoch. BODINF( 1, 1) = 45*1, $ The "of date" systems will be inertial. CONCEN( 1) = 15*' ', CONCOR(1,1, 1) = 240*' ', CONEQX( 1, 1) = 60*'2000', $ Nominally J2000 (see below) ANGLEB( 1, 1) = 60*' ', $ $ Print list #1 $ BODCOR(1,1, 1) = 'EARTH','EARTH','MEAN','EQUATO','PLUTO' CONCEN( 1) = 'EARTH', CONCOR(1,1, 1) = 'SPACE','EARTH','MEAN','EQUATO', CONCOR(1,2, 1) = 'SPACE','EARTH','MEAN','ORBITA', ANGLEB( 1, 1) = 'PRINT','PLUTO', $ $ Print list #2 $ BODCOR(1,1,2)= 'SUN','EARTH','MEAN','EQUATO','PLUTO', CONCEN(2) = 'SUN', CONCOR(1,1,2)= 'SPACE','EARTH','MEAN','EQUATO', CONCOR(1,2,2)= 'SPACE','EARTH','MEAN','ORBITA', ANGLEB(1,2) = 'PRINT','PLUTO', $ $ Print list #3 $ BODCOR(1,1,3)= 'PLUTO','EARTH','MEAN','EQUATO', CONCEN(3) = 'PLUTO', CONCOR(1,1,3)= 'SPACE','EARTH','MEAN','EQUATO', CONCOR(1,2,3)= 'SPACE','EARTH','MEAN','ORBITA', CONCOR(1,3,3)= 'SPACE','PLUTO','TRUE','EQUATO', CONEQX(1,3) = '2000','2000','DATE', ANGLEB(1,3) = 'PRINT', $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ SAVE file generation: $ FERP = 31, $ Fixed variable output frame: 31 => EME2000 SPABT(1) = 10*' ', $ Absolute epoch to write out. SPBOD(1) = 'EARTH', $ Extra body name for fixed output SPDBUG = 0, $ Do not print SAVE file data records. SPTAPF = 0, $ >0 => Turn on writing of save tape SPTDT(1,1) = 30*' ', $ TDT times to write out. SPHWTM = 'ET', $ Time type of epochs in SPABT HWSPT = 'ET', $ Time type of epochs in SPTDT $ $ Print lists to examine for PRGVAR names: $ SAPLIS(1) = 1,2,3, $ PRGVAR(1,1) = 400*' ', $ $ PRGVAR(1,1) = 'SMA','ECC','TA','LAN1','APF1','INC1','PER', $ 'ALTP1','DR1','RIP1','VIP1','LATP1','LONP1', $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ OPTG file generation: $ $ OPTG file title & labels: $ OTITLE = 'NEAR Radio Science GIN Lock File: OPTG File', NAMEXT = 'NEAR Radio Science Team', OPTMIS = '93', $ $ Note: If one wants an event printed on the OPTG file, one must also have $ it printed out on TWIST. $ $ First specify TWIST print begin & end times. These define the absolute $ limits of the OPTG file -- it cannot start before or end after these times. $ Now define default OPTG begin & end times. If they are outside of TWIST $ print limits (or blank), then they will be set to the TWIST limits. $ OPTBEG = '01-Jan-1996 00:00:00 ET', OPTEND = '31-Mar-2000 00:00:00 ET', $ OPTBOD(1) = 5*' ', $ OPTG file central body or 'CRUISE'. $ OPTBOD = ' ' turns off OPTG file creation. OBDEVT = ' ', $ Event defining orbit boundary. $ OBDEVT = ' ' defaults to periapsis. OPTGPH = 'CRUISE', $ Mission phase label. CONANG = 0, $ SEP angle denoting conjunction. INORBN = 0, $ Initial orbit number. $ $ W A R N I N G ! ==> OCCRAD & ATMRAD are EQUIVALENT input parameters. $ In the source code, they are "equivalenced". $ OCCRAD( 4) = 0.0D0, $ Radius for atmosphere occultation. $ $ Specify which events to print out on the OPTG file: $ OPTEVT( 1,1) = .TRUE., $ CONST: Write a record with planet constants. OPTEVT( 2,1) = .TRUE., $ PERIAP: Periapsis. OPTEVT( 3,1) = .TRUE., $ APOAP: Apoapsis. OPTEVT( 4,1) = .TRUE., $ EOCCAB: Begin geocen. atmos occult by OPTBOD. OPTEVT( 5,1) = .TRUE., $ EOCCAE: End geocen. atmos occult by OPTBOD. OPTEVT( 6,1) = .FALSE., $ SOCCAB: Begin heliocen. atmos occult by OPTBOD. OPTEVT( 7,1) = .FALSE., $ SOCCAE: End heliocen. atmos occult by OPTBOD. OPTEVT( 8,1) = .TRUE., $ EOCCSB: Begin geocen. surface occult by OPTBOD. OPTEVT( 9,1) = .TRUE., $ EOCCSE: End geocen. surface occult by OPTBOD. OPTEVT(10,1) = .TRUE., $ SOCCSB: Begin heliocen. surface occult by OPTBOD. OPTEVT(11,1) = .TRUE., $ SOCCSE: End heliocen. surface occult by OPTBOD. OPTEVT(12,1) = .TRUE., $ AEQUAX: Ascending OPTBOD equator crossing. OPTEVT(13,1) = .TRUE., $ DEQUAX: Descending OPTBOD equator crossing. OPTEVT(14,1) = .TRUE., $ DLTERM: Dark to light terminator crossing. OPTEVT(15,1) = .TRUE., $ LDTERM: Light to dark terminator crossing. OPTEVT(16,1) = .TRUE., $ NPOLEX: North pole minimum slant range. OPTEVT(17,1) = .TRUE., $ SPOLEX: South pole minimum slant range. $ CONEVT( 1) = .TRUE., $ SCONB: Begin superior conjunction. CONEVT( 2) = .TRUE., $ SCONE: End superior conjunction. CONEVT( 3) = .TRUE., $ ICONB: Begin inferior conjunction. CONEVT( 4) = .TRUE., $ ICONE: End inferior conjunction. CONEVT( 5) = .TRUE., $ SCONJ: Cross integral angle boundary (SUP CONJ). CONEVT( 6) = .TRUE., $ ICONJ: Cross integral angle boundary (INF CONJ). CONEVT( 7) = .TRUE., $ ICONM: Minimum inferior conjunction SEP angle. CONEVT( 8) = .TRUE., $ SCONM: Minimum superior conjunction SEP angle. $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ CRSPOST $ $ Celestial reference set (CRS). S/C centered state placed on output for $ each CRS body: $ CRSBOD(1) = 'PLUTO', 'EARTH', 'SUN', $ CRSM = 0, $ No print. CRSPRT = 1, $ Print CRS Constants, 1st & last data records $ IPSTM = ' ', $ Printout start epoch. $ ETIM = ' ', $ Printout end epoch. SPTDT(1,1) = 30*' ', $ Times to write 'SAVE TAPE' $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ LITIME $ $ Geocentric or topocentric one-way light times (OWLT) calculated for $ specified time increments during some span: $ ITITLE = 'NEAR Radio Scienc GIN Lock File: LITIME File', NAMEXT = 'NEAR Radio Science Team', IHEAD = ' ', ICOMNT = ' ', $ IMISSN = 'NEAR', ISCID = 'NEAR', IOPT = 3, $ Get printout and file. ISTRT = ' ', $ Start time, SCET in GMT. IEND = ' ', $ End time, SCET in GMT. $ STANO(1) = 15, 45, 65, $ Stations for topocentric OWLT. $ 3 ==> geocentric OWLT. TINT = 0.0D0, $ OWLT computation interval (seconds). TOL = 1.0D-6, $ OWLT convergence tolerance (seconds). $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ STATRJ $ $ Generate geocentric and tropocentric information for the DSN. $ STALAB = 2*' ', STALAB(1) = ' ', HVFILE = 'NO', $ Station polynomial file is generated. TRJPRT = 'NO', $ No GEO or TOPO print during burns. STANUM(1) = 12, 14, 15, 42, 43, 45, 46, 61, 63, 65, 10*0, STABEG = ' ', $ Start epoch (UTC) of the file. STASTP = ' ', $ End epoch (UTC) of the file. OCCBOD = 'PLUTO', $ Extra body for geometric calculations. VPACC = 1.0D0, $ Tolerance (min) in rise/set iterations. LTACC = 0.01D0, $ Tolerance (sec) in LT iteration. $ $ Numerical control parameters: $ $ Note: These quantities specify polynomial coefficients for the $ RA & DEC or the AZ & EL for the station-to-S/C vector. $ NSECIT = 5, $ Max # of secant iterations for rise/set. NDEG = 10, $ Degree of polynomials on file. STAPTS = 13, $ Number of points in polynomials. LSPH(1) = 50.0D3, 200.0D3, $ Radii of near & far Earth phases (km). ESPH(1) = 50.0D3, 200.0D3, $ Radii of near & far "PLUTO" phases (km). PSPANS(1) = 0.025D0, $ Geocentric near Earth span (days). PSPANS(2) = 0.1D0, $ Geocentric far Earth span (days). PSPANS(3) = 1.0D0, $ Geocentric cruise span (days). PSPANS(4) = 0.1D0, $ Geocentric far "PLUTO" span (days). PSPANS(5) = 0.025D0, $ Geocentric near "PLUTO" span (days). NPERP(1) = 7, $ TOPO spans/pass, near Earth. NPERP(2) = 3, $ TOPO spans/pass, far Earth. NPERP(3) = 1, $ TOPO spans/pass, cruise. NPERP(4) = 3, $ TOPO spans/pass, far "PLUTO". NPERP(5) = 7, $ TOPO spans/pass, near "PLUTO". NPERP(6) = 3, $ TOPO spans/pass, max ELV > 70 degrees. VPTBLE(1,1) = 1.0D4, 3.0D0, $ Monitor rise/set every 3 min. < 10K km. VPTBLE(1,2) = 2.5D4, 20.0D0, $ Monitor rise/set every 20 min. < 25K km. VPTBLE(1,3) = 5.0D4, 40.0D0, $ Monitor rise/set every 40 min. < 50K km. VPTBLE(1,4) = 1.0D5, 50.0D0, $ Monitor rise/set every 50 min. < 100K km. VPTBLE(1,5) = 1.0D20, 60.0D0, $ Monitor rise/set every 60 min. > 100K km. $ $ Print control parameters: $ STADBG = 'NO', $ No debug print. PRTBEG = ' ', $ Begin STATRJ print (time in UTC). PRTSTP = ' ', $ End STATRJ print (time in UTC). PRTHED = 'YES', $ Print the header records. RISPRT = 'NO', $ Don't print station rise/set events. SUMTAB = 'YES', $ Print rise/set events. $ 'ONLY' => Summary table only. GPRT(1) = 20*1, $ Print all 20 geocentric quantities. TPRT(1) = 0, 24*1, $ Print all 25 topocentric quantities. STADEL(1,1) =30*' ', $ 10 TDT print sequences. STATIM(1) = 10*' ', $ Absolute epoch (UTC) prints. STAPRT(1) = 15, 45, 65, $ Stations to print. $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Station locations: $ $ 1) Folkner, W. M., "Current DSN Station Locations," JPL IOM 335.1-95-027, $ October 16, 1995. $ $ Modified: 7 Nov 1996; DSS 66 updated, DSS 34, 54 not yet surveyed $ Modified: 25 Nov 1996; DSS 34 survey included $ Modified: 13 May 1997; DSS 54 survey included $ Modified: 09 Jun 1997; error in DSS 54 corrected $ $ Corrections for auto-focusing of the sub-reflector have been applied her $ for the 70m and HEF antennas, so their positions are 7cm and 1.5 cm $ respectively lower in elevation than in IOM 335.1-95-027. $ Station locations are consistent with the ITRF93 system. $ $ Station locations are for use with J2000 ephemerides (i.e. DE403). $ $ Stations included are : 12,13,14,15,16,17, $ 23,24,25,26,27,28, $ 33,34,42,43,45,46, $ 53,54,61,63,65,66. $ $ The following station location and mask data is consistent with the ITRF93 $ reference standard: $ ESTRF = 'ITRF93', $ ESLABL = 'FOLKNER: JPL IOM 335.1-95-027', $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Zero out and initialize the plate motion parameters: $ ECPLAT(1) = 300*' ', ECNUM(1) = 300*0, ECRATE(1,1) = 900*0.0D0, $ ECEPOC(1) = 300*'01-JAN-1993 00:00:00', PLATEM = 'LINEAR', $ $ North East Vertical $ ECNUM( 1) = 10, ECRATE(1,1) = -0.57, -1.98, -0.01, $Goldstone ECNUM( 2) = 20, ECRATE(1,2) = -0.57, -1.98, -0.01, $ ECNUM( 3) = 30, ECRATE(1,3) = +5.06, +1.97, +0.01, $Canberra ECNUM( 4) = 40, ECRATE(1,4) = +5.06, +1.97, +0.01, $ ECNUM( 5) = 50, ECRATE(1,5) = +2.55, +2.11, +0.11, $Madrid ECNUM( 6) = 60, ECRATE(1,6) = +2.55, +2.11, +0.11, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ REGRES will compute antenna offset corrections as follows: $ ANTENA = .TRUE., ANTARM(1) = 6.7060D0, $ For 26-M H-D or 34-M H-D (m). ANTARM(2) = 0.9144D0, $ For 26-M A-E (m). ANTARM(3) = 6.7060D0, $ For 26-M X'-Y' (m). ANTARM(4) = 2.4380D0, $ For 9-M X-Y (m). ANTARM(5) = 1.8288D0, $ For 34-M HSB (m). $ $ Antenna corrections are not required for 34-M BWG & 11m VLBI stations. $ ESOFFR = 0.39838D0, $ Offset radius for the 11m VLBI stations. $ $ TROPND(1) = 0.0D0, $ Dry troposphere range correction (m). $ TROPNW(1) = 0.0D0, $ Wet troposphere range correction (m). $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Zero out and initialize station location parameters: $ ESNUM( 1) = 300*0, ESTYPE( 1) = 300*' ', ESLOCT( 1) = 300*' ', ESLOC(1, 1) = 900*0.0D0, ESNAME( 1) = 300*' ', ESCPLX( 1) = 300*0, $ ESNUM( 1) = 12, ESTYPE( 1) = '34-H-D', ESLOCT( 1) = 'CYLIND', ESLOC(1, 1) = 243.194513046D0, 3665.630988D0, 5212.0544722D0, ESNAME( 1) = 'GOLDSTONE ECHO 34-H-D', ESCPLX( 1) = 10, $ ESNUM( 2) = 13, ESTYPE( 2) = '34-BWG', ESLOCT( 2) = 'CYLIND', ESLOC(1, 2) = +243.2055430, +3660.912787, +5215.524535, ESNAME( 2) = 'GOLDSTONE VENUS 34-BWG', ESCPLX( 2) = 10, $ ESNUM( 3) = 14, ESTYPE( 3) = '70-A-E', ESLOCT( 3) = 'CYLIND', ESLOC(1, 3) = 243.110463799D0, 3677.052330D0, 5203.9968973D0, ESNAME( 3) = 'GOLDSTONE MARS 64-A-E', ESCPLX( 3) = 10, $ ESNUM( 4) = 15, ESTYPE( 4) = '34-HEF', ESLOCT( 4) = 'CYLIND', ESLOC(1, 4) = 243.112806935D0, 3676.670034D0, 5204.2343194D0, ESNAME( 4) = 'GOLDSTONE 34M 34-HEF', ESCPLX( 4) = 10, $ ESNUM( 5) = 16, ESTYPE( 5) = '26-X-Y', ESLOCT( 5) = 'CYLIND', ESLOC(1, 5) = 243.126352287D0, 3669.387069D0, 5209.3707151D0, ESNAME( 5) = 'GDS5 26-X-Y', ESCPLX( 5) = 10, $ ESNUM( 6) = 17, ESTYPE( 6) = '9-X-Y' , ESLOCT( 6) = 'CYLIND', ESLOC(1, 6) = 243.126496674D0, 3669.440659D0, 5209.3240561D0, ESNAME( 6) = 'GOLDSTONE 9M 9-X-Y', ESCPLX( 6) = 10, $ ESNUM( 7) = 23, ESTYPE( 7) = '11VLBI', ESLOCT( 7) = 'CYLIND', ESLOC(1, 7) = 243.127139009D0, 3669.207824D0, 5209.4995031D0, ESNAME( 7) = 'GOLDSTONE 11M 11VLBI', ESCPLX( 7) = 10, $ ESNUM( 8) = 24, ESTYPE( 8) = '34-BWG', ESLOCT( 8) = 'CYLIND', ESLOC(1, 8) = 243.125207895D0, 3669.242317D0, 5209.4824863D0, ESNAME( 8) = 'GOLDSTONE 34M 34-BWG', ESCPLX( 8) = 10, $ ESNUM( 9) = 25, ESTYPE( 9) = '34-BWG', ESLOCT( 9) = 'CYLIND', ESLOC(1, 9) = 243.124638433D0, 3669.040895D0, 5209.6359783D0, ESNAME( 9) = 'GOLDSTONE 34M 34-BWG', ESCPLX( 9) = 10, $ ESNUM( 10) = 26, ESTYPE( 10) = '34-BWG', ESLOCT( 10) = 'CYLIND', ESLOC(1,10) = 243.126984880D0, 3668.872212D0, 5209.7669713D0, ESNAME( 10) = 'GOLDSTONE 34M 34-BWG', ESCPLX( 10) = 10, $ ESNUM( 11) = 27, ESTYPE( 11) = '34-HSB', ESLOCT( 11) = 'CYLIND', ESLOC(1,11) = 243.223351581D0, 3660.096529D0, 5216.0792441D0, ESNAME( 11) = 'GOLDSTONE 34M 34-HSB', ESCPLX( 11) = 10, $ ESNUM( 12) = 28, ESTYPE( 12) = '34-HSB', ESLOCT( 12) = 'CYLIND', ESLOC(1,12) = 243.221110863D0, 3660.103577D0, 5216.0891761D0, ESNAME( 12) = 'GOLDSTONE 34M 34-HSB', ESCPLX( 12) = 10, $ ESNUM( 13) = 33, ESTYPE( 13) = '11VLBI', ESLOCT( 13) = 'CYLIND', ESLOC(1,13) = 148.983089455D0, -3674.570392D0, 5205.3723669D0, ESNAME( 13) = 'CANBERRA 11M 11VLBI', ESCPLX( 13) = 40, $ ESNUM( 14) = 34, ESTYPE( 14) = '34-BWG', ESLOCT( 14) = 'CYLIND', ESLOC(1,14) = +148.9819620, -3674.393542, +5205.507750, ESNAME( 14) = 'CANBERRA 34M 34-BWG', ESCPLX( 14) = 40, $ ESNUM( 15) = 42, ESTYPE( 15) = '34-H-D', ESLOCT( 15) = 'CYLIND', ESLOC(1,15) = 148.981264988D0, -3674.582072D0, 5205.3524323D0, ESNAME( 15) = 'CANBERRA 34-H-D', ESCPLX( 15) = 40, $ ESNUM( 16) = 43, ESTYPE( 16) = '70-A-E', ESLOCT( 16) = 'CYLIND', ESLOC(1,16) = 148.981264989D0, -3674.748540D0, 5205.2515219D0, ESNAME( 16) = 'BELLIMA 64-A-E', ESCPLX( 16) = 40, $ ESNUM( 17) = 45, ESTYPE( 17) = '34-HEF', ESLOCT( 17) = 'CYLIND', ESLOC(1,17) = 148.977683311D0, -3674.381393D0, 5205.4946968D0, ESNAME( 17) = 'CANBERRA 34M 34-HEF', ESCPLX( 17) = 40, $ ESNUM( 18) = 46, ESTYPE( 18) = '26-X-Y', ESLOCT( 18) = 'CYLIND', ESLOC(1,18) = 148.983079363D0, -3674.975508D0, 5205.0754964D0, ESNAME( 18) = 'CAN4 26-X-Y', ESCPLX( 18) = 40, $ ESNUM( 19) = 53, ESTYPE( 19) = '11VLBI', ESLOCT( 19) = 'CYLIND', ESLOC(1,19) = 355.750345311D0, 4114.758758D0, 4862.6994697D0, ESNAME( 19) = 'MADRID 11M 11VLBI', ESCPLX( 19) = 60, $ ESNUM( 20) = 54, ESTYPE( 20) = '34-BWG', ESLOCT( 20) = 'CYLIND', ESLOC(1,20) = +355.7459008, +4114.618643, +4862.832239, ESNAME( 20) = 'MADRID 34M 34-BWG', ESCPLX( 20) = 60, $ ESNUM( 21) = 61, ESTYPE( 21) = '34-H-D', ESLOCT( 21) = 'CYLIND', ESLOC(1,21) = 355.750975313D0, 4114.884445D0, 4862.6103559D0, ESNAME( 21) = 'ROBLEDO 34-H-D', ESCPLX( 21) = 60, $ ESNUM( 22) = 63, ESTYPE( 22) = '70-A-E', ESLOCT( 22) = 'CYLIND', ESLOC(1,22) = 355.751988973D0, 4115.109067D0, 4862.4509267D0, ESNAME( 22) = 'ROBLEDO 210-FT 64-A-E', ESCPLX( 22) = 60, $ ESNUM( 23) = 65, ESTYPE( 23) = '34-HEF', ESLOCT( 23) = 'CYLIND', ESLOC(1,23) = 355.748579509D0, 4114.748765D0, 4862.7172271D0, ESNAME( 23) = 'MADRID 34M 34-HEF', ESCPLX( 23) = 60, $ ESNUM( 24) = 66, ESTYPE( 24) = '26-X-Y', ESLOCT( 24) = 'CYLIND', ESLOC(1,24) = +355.7485798, +4114.995021, +4862.528531, ESNAME( 24) = 'MAD3 26-X-Y', ESCPLX( 24) = 60, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Station horizon masks: $ $ 1) Wolf, A. A., "50-Segment vs. 11-Segment Masks for DSN Stations $ in NAV Software," JPL IOM MGN-NAV-89-04, January 20, 1989. $ $ 2) Enright, S., "DSN Horizon Masks," JPL IOM OEA.18/12.18.E.0, $ January 7, 1991. $ $ 3) Sunseri, R. F., "New Station Masks for DSS 12, 14, 15, 16, 17, 42, $ 43, 45, 46, 61, 63, 65, AND 66," JPL IOM 314.9/91-619, March 18, 1991. $ $ ESMASK(J,K,N): $ $ ESMASK entries 'J' are in the following order (per sector): $ constraint type (where 1 = EL, 2 = HA, 3 = DEC) as a function of AZ; $ starting AZ (degrees); the five 4th degree polynomial coefficients; $ the ending AZ (degrees). $ $ Entries 'K' enumerate the sectors or the discrete polynomial segments $ (from 1 to 11) describing the horizon silhouette. $ $ Entries 'N' denote the stations. $ ESMASK(1, 1, 1) = 26400*0.0D0, $ $ Horizon mask for station 12 GOLDSTONE ECHO 34M HA-DEC $ ESMASK(1, 1, 1) = 0.20000000E+01, 0.00000000E+00, 0.26770001E+03, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.78272552E+02, ESMASK(1, 2, 1) = 0.10000000E+01, 0.78272552E+02, -0.95303301E+04, 0.34640482E+03, -0.41888137E+01, 0.16859710E-01, 0.00000000E+00, 0.89003731E+02, ESMASK(1, 3, 1) = 0.10000000E+01, 0.89003731E+02, 0.69569359E+05, -0.27941345E+04, 0.41989853E+02, -0.27979159E+00, 0.69741247E-03, 0.10533190E+03, ESMASK(1, 4, 1) = 0.10000000E+01, 0.10533190E+03, 0.10633186E+07, -0.38247000E+05, 0.51556805E+03, -0.30868518E+01, 0.69263014E-02, 0.11632820E+03, ESMASK(1, 5, 1) = 0.10000000E+01, 0.11632820E+03, 0.42380308E+04, -0.12654492E+03, 0.14084842E+01, -0.69273664E-02, 0.12707357E-04, 0.15477820E+03, ESMASK(1, 6, 1) = 0.10000000E+01, 0.15477820E+03, -0.16075879E+04, 0.32044701E+02, -0.24533567E+00, 0.86667429E-03, -0.11988418E-05, 0.19936530E+03, ESMASK(1, 7, 1) = 0.10000000E+01, 0.19936530E+03, -0.21919068E+05, 0.39109232E+03, -0.26111150E+01, 0.77328146E-02, -0.85710362E-05, 0.25539819E+03, ESMASK(1, 8, 1) = 0.10000000E+01, 0.25539819E+03, 0.42327228E+06, -0.49249419E+04, 0.19097824E+02, -0.24681104E-01, 0.00000000E+00, 0.26459210E+03, ESMASK(1, 9, 1) = 0.10000000E+01, 0.26459210E+03, 0.79551706E+06, -0.89334912E+04, 0.33436848E+02, -0.41711859E-01, 0.00000000E+00, 0.27229779E+03, ESMASK(1,10, 1) = 0.10000000E+01, 0.27229779E+03, -0.33448823E+04, 0.23990385E+02, -0.42939007E-01, 0.00000000E+00, 0.00000000E+00, 0.28144791E+03, ESMASK(1,11, 1) = 0.20000000E+01, 0.28144791E+03, 0.91800003E+02, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 13 GOLDSTONE 34 M BWG $ ESMASK(1, 1, 2) = .10000000E+01, .00000000E+00, .88413235E+01, -.10041944E+01, .15172188E+00, -.66063348E-02, .00000000E+00, .13000000E+02, ESMASK(1, 2, 2) = .10000000E+01, .13000000E+02, .70000000E+01, .00000000E+00, .00000000E+00, .00000000E+00, .00000000E+00, .31600000E+03, ESMASK(1, 3, 2) = .10000000E+01, .31600000E+03, -.54634507E+05, .64535163E+03, -.28650581E+01, .56665820E-02, -.42124064E-05, .36000000E+03, $ $ Horizon mask for station 14 GOLDSTONE MARS 70M AZ-EL (6 degrees) $ ESMASK(1, 1, 3) = 0.10000000E+01, 0.00000000E+00, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 15 GOLDSTONE 34M HEF - from R. F. Sunseri $ ESMASK(1, 1, 4) = 0.10000000E+01, 0.00000000E+00, 0.70000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.14000000E+03, ESMASK(1, 2, 4) = 0.10000000E+01, 0.14000000E+03, 0.31488140E+06, -0.86396767E+04, 0.88866488E+02, -0.40612354E+00, 0.69580420E-03, 0.15000000E+03, ESMASK(1, 3, 4) = 0.10000000E+01, 0.15000000E+03, -0.14169734E+04, 0.26758388E+02, -0.16661819E+00, 0.34425245E-03, 0.00000000E+00, 0.17400000E+03, ESMASK(1, 4, 4) = 0.10000000E+01, 0.17400000E+03, -0.98703660E+04, 0.21707469E+03, -0.17883522E+01, 0.65457028E-02, -0.89800872E-05, 0.19100000E+03, ESMASK(1, 5, 4) = 0.10000000E+01, 0.19100000E+03, 0.45917977E+05, -0.94315447E+03, 0.72575468E+01, -0.24790218E-01, 0.31712773E-04, 0.20400000E+03, ESMASK(1, 6, 4) = 0.10000000E+01, 0.20400000E+03, 0.70000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 16 GDS5 26M X-Y $ ESMASK(1, 1, 5) = 0.10000000E+01, 0.00000000E+00, 0.42000000E+01, 0.39159119E-01, -0.37419274E-02, 0.60352892E-04, -0.21321540E-06, 0.76400000E+02, ESMASK(1, 2, 5) = 0.10000000E+01, 0.76400000E+02, -0.13565604E+05, 0.60215993E+03, -0.10026011E+02, 0.74290449E-01, -0.20669569E-03, 0.10370000E+03, ESMASK(1, 3, 5) = 0.10000000E+01, 0.10370000E+03, 0.41643831E+04, -0.13807078E+03, 0.17075052E+01, -0.93242171E-02, 0.18971043E-04, 0.14600000E+03, ESMASK(1, 4, 5) = 0.10000000E+01, 0.14600000E+03, 0.78648803E+01, -0.20605789E-01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.23110000E+03, ESMASK(1, 5, 5) = 0.10000000E+01, 0.23110000E+03, -0.35610148E+03, 0.30029595E+01, -0.62691000E-02, 0.00000000E+00, 0.00000000E+00, 0.25550000E+03, ESMASK(1, 6, 5) = 0.10000000E+01, 0.25550000E+03, -0.13182052E+07, 0.19524051E+05, -0.10844433E+03, 0.26772248E+00, -0.24786650E-03, 0.28430000E+03, ESMASK(1, 7, 5) = 0.10000000E+01, 0.28430000E+03, 0.99904725E+05, -0.10313754E+04, 0.35485840E+01, -0.40690104E-02, 0.00000000E+00, 0.29870000E+03, ESMASK(1, 8, 5) = 0.10000000E+01, 0.29870000E+03, -0.44732224E+02, 0.26238413E+00, -0.35128134E-03, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 17 GOLDSTONE 9M X-Y $ ESMASK(1, 1, 6) = .10000000E+01, .00000000E+00, .75710559E+01, .56745785E+00, -.16053176E+00, -.23797009E-01, .31366550E-02, .90000000E+01, ESMASK(1, 2, 6) = .10000000E+01, .90000000E+01, .30154251E+01, -.27452108E-01, .39314569E-03, .00000000E+00, .00000000E+00, .53000000E+02, ESMASK(1, 3, 6) = .10000000E+01, .53000000E+02, -.31640010E+02, .10188766E+01, -.56055673E-02, -.44994674E-04, .33612912E-06, .10000000E+03, ESMASK(1, 4, 6) = .10000000E+01, .10000000E+03, .39290136E+02, -.15288311E+01, .17916687E-01, -.62774104E-04, .00000000E+00, .14100000E+03, ESMASK(1, 5, 6) = .10000000E+01, .14100000E+03, -.17838515E+04, .33960661E+02, -.21419689E+00, .44869942E-03, .00000000E+00, .17400000E+03, ESMASK(1, 6, 6) = .10000000E+01, .17400000E+03, -.22633994E+06, .47924163E+04, -.38073951E+02, .13452245E+00, -.17834495E-03, .20400000E+03, ESMASK(1, 7, 6) = .10000000E+01, .20400000E+03, .95227542E+05, -.17275105E+04, .11744646E+02, -.35464648E-01, .40133387E-04, .24100000E+03, ESMASK(1, 8, 6) = .10000000E+01, .24100000E+03, .36036412E+05, -.53049295E+03, .29272307E+01, -.71755618E-02, .65933505E-05, .29600000E+03, ESMASK(1, 9, 6) = .10000000E+01, .29600000E+03, -.14245175E+07, .18945540E+05, -.94435372E+02, .20909275E+00, -.17351398E-03, .30500000E+03, ESMASK(1,10, 6) = .10000000E+01, .30500000E+03, .20434410E+05, -.24924857E+03, .11418414E+01, -.23282504E-02, .17827921E-05, .35400000E+03, ESMASK(1,11, 6) = .10000000E+01, .35400000E+03, -.18034422E+05, .96878159E+02, -.11989286E+00, -.27777778E-04, .00000000E+00, .36000000E+03, $ $ Horizon mask for station 23 GOLDSTONE 11VLBI (6 degrees) $ ESMASK(1, 1, 7) = 0.10000000E+01, 0.00000000E+00, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 24 GOLDSTONE 34M BWG (6 degrees) $ ESMASK(1, 1, 8) = 0.10000000E+01, 0.00000000E+00, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 25 GOLDSTONE 34M BWG (6 degrees) $ ESMASK(1, 1, 9) = 0.10000000E+01, 0.00000000E+00, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 26 GOLDSTONE 34M BWG (6 degrees) $ ESMASK(1, 1,10) = 0.10000000E+01, 0.00000000E+00, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 27 GOLDSTONE 34M HSB (6 degrees) $ ESMASK(1, 1,11) = 0.10000000E+01, 0.00000000E+00, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 28 GOLDSTONE 34M HSB (6 degrees) $ ESMASK(1, 1,12) = 0.10000000E+01, 0.00000000E+00, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 33 CANBERRA 11VLBI (6 degrees) $ ESMASK(1, 1,13) = 0.10000000E+01, 0.00000000E+00, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 34 CANBERRA 34M BWG (6 degrees) $ ESMASK(1, 1,14) = 0.10000000E+01, 0.00000000E+00, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 42 CANBERRA 34M HA-DEC $ ESMASK(1, 1,15) = 0.10000000E+01, 0.00000000E+00, 0.75000000E+01, -0.21720202E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.15331349E+02, ESMASK(1, 2,15) = 0.10000000E+01, 0.15331349E+02, -0.44611259E+01, 0.11000934E+01, -0.48064202E-01, 0.94749819E-03, -0.63933544E-05, 0.69000000E+02, ESMASK(1, 3,15) = 0.10000000E+01, 0.69000000E+02, 0.53716763E+02, -0.10629115E+01, 0.27988004E-02, 0.80397658E-04, -0.46864056E-06, 0.12132450E+03, ESMASK(1, 4,15) = 0.20000000E+01, 0.12132450E+03, 0.25726401E+03, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.18000000E+03, ESMASK(1, 5,15) = 0.20000000E+01, 0.18000000E+03, 0.10026200E+03, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.24639012E+03, ESMASK(1, 6,15) = 0.10000000E+01, 0.24639012E+03, -0.27832537E+02, 0.31988880E+00, -0.85958838E-03, 0.29368644E-06, 0.51562044E-09, 0.33679230E+03, ESMASK(1, 7,15) = 0.10000000E+01, 0.33679230E+03, -0.10488942E+03, 0.31219283E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 43 BELLIMA 70M AZ-EL $ ESMASK(1, 1,16) = 0.10000000E+01, 0.00000000E+00, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.42562500E+02, ESMASK(1, 2,16) = 0.10000000E+01, 0.42562500E+02, -0.25039934E+03, 0.16166534E+02, -0.37341598E+00, 0.37759678E-02, -0.14128269E-04, 0.87000000E+02, ESMASK(1, 3,16) = 0.10000000E+01, 0.87000000E+02, 0.63776440E+03, -0.19990196E+02, 0.21002880E+00, -0.73100743E-03, 0.00000000E+00, 0.11292578E+03, ESMASK(1, 4,16) = 0.10000000E+01, 0.11292578E+03, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.23267383E+03, ESMASK(1, 5,16) = 0.10000000E+01, 0.23267383E+03, -0.25119053E+05, 0.30341229E+03, -0.12195134E+01, 0.16314239E-02, 0.00000000E+00, 0.24874512E+03, ESMASK(1, 6,16) = 0.10000000E+01, 0.24874512E+03, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 45 CANBERRA 34M HEF - from R. F. Sunseri $ ESMASK(1, 1,17) = 0.10000000E+01, 0.00000000E+00, 0.70000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.68000000E+02, ESMASK(1, 2,17) = 0.10000000E+01, 0.68000000E+02, 0.24097240E+05, -0.12958382E+04, 0.26076850E+02, -0.23268148E+00, 0.77684081E-03, 0.80000000E+02, ESMASK(1, 3,17) = 0.10000000E+01, 0.80000000E+02, 0.94633318E+04, -0.42512078E+03, 0.71609700E+01, -0.53555049E-01, 0.15001960E-03, 0.95000000E+02, ESMASK(1, 4,17) = 0.10000000E+01, 0.95000000E+02, 0.70000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.10000000E+03, ESMASK(1, 5,17) = 0.10000000E+01, 0.10000000E+03, 0.49878000E+04, -0.14455800E+03, 0.13975000E+01, -0.45000000E-02, 0.00000000E+00, 0.10300000E+03, ESMASK(1, 6,17) = 0.10000000E+01, 0.10300000E+03, -0.14829500E+03, 0.30540000E+01, -0.15000000E-01, 0.00000000E+00, 0.00000000E+00, 0.10500000E+03, ESMASK(1, 7,17) = 0.10000000E+01, 0.10500000E+03, 0.70000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.11300000E+03, ESMASK(1, 8,17) = 0.10000000E+01, 0.11300000E+03, -0.15984760E+05, 0.41046000E+03, -0.35100000E+01, 0.10000000E-01, 0.00000000E+00, 0.11600000E+03, ESMASK(1, 9,17) = 0.10000000E+01, 0.11600000E+03, 0.70000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.19900000E+03, ESMASK(1,10,17) = 0.10000000E+01, 0.19900000E+03, -0.60328490E+04, 0.60400000E+02, -0.15100000E+00, 0.00000000E+00, 0.00000000E+00, 0.20100000E+03, ESMASK(1,11,17) = 0.10000000E+01, 0.20100000E+03, 0.70000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 46 CAN4 26M X-Y $ ESMASK(1, 1,18) = 0.10000000E+01, 0.00000000E+00, 0.25380811E+01, 0.18499543E+00, -0.11241838E-02, 0.00000000E+00, 0.00000000E+00, 0.78400000E+02, ESMASK(1, 2,18) = 0.10000000E+01, 0.78400000E+02, -0.30596504E+03, 0.71438678E+01, -0.39664356E-01, 0.00000000E+00, 0.00000000E+00, 0.10500000E+03, ESMASK(1, 3,18) = 0.10000000E+01, 0.10500000E+03, -0.60752000E+03, 0.14670667E+02, -0.11480000E+00, 0.29333333E-03, 0.00000000E+00, 0.13000000E+03, ESMASK(1, 4,18) = 0.10000000E+01, 0.13000000E+03, 0.57527477E+03, -0.12406421E+02, 0.99000311E-01, -0.34531242E-03, 0.44508798E-06, 0.25400000E+03, ESMASK(1, 5,18) = 0.10000000E+01, 0.25400000E+03, -0.29045635E+06, 0.42961485E+04, -0.23855177E+02, 0.58938691E-01, -0.54669509E-04, 0.28600000E+03, ESMASK(1, 6,18) = 0.10000000E+01, 0.28600000E+03, -0.49227926E+06, 0.65000900E+04, -0.32160346E+02, 0.70665762E-01, -0.58183973E-04, 0.32300000E+03, ESMASK(1, 7,18) = 0.10000000E+01, 0.32300000E+03, 0.80000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.33300000E+03, ESMASK(1, 8,18) = 0.10000000E+01, 0.33300000E+03, -0.32022727E+03, 0.18055556E+01, -0.25252525E-02, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 53 MADRID 11VLBI (6 degrees) $ ESMASK(1, 1,19) = 0.10000000E+01, 0.00000000E+00, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 54 MADRID 34M BWG (6 degrees) $ ESMASK(1, 1,20) = 0.10000000E+01, 0.00000000E+00, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 61 ROBLEDO 34M HA-DEC (LABELED 26-H-D) $ ESMASK(1, 1,21) = 0.20000000E+01, 0.00000000E+00, 0.25805301E+03, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.65831207E+02, ESMASK(1, 2,21) = 0.10000000E+01, 0.65831207E+02, 0.10459758E+02, -0.77675313E-01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.90000000E+02, ESMASK(1, 3,21) = 0.10000000E+01, 0.90000000E+02, 0.56644519E+03, -0.18895845E+02, 0.23353083E+00, -0.12591545E-02, 0.24992182E-05, 0.16023386E+03, ESMASK(1, 4,21) = 0.10000000E+01, 0.16023386E+03, -0.98384564E+03, 0.18665325E+02, -0.13708907E+00, 0.47358446E-03, -0.65782143E-06, 0.20398195E+03, ESMASK(1, 5,21) = 0.10000000E+01, 0.20398195E+03, 0.64192671E+04, -0.11018304E+03, 0.70383865E+00, -0.19836526E-02, 0.20831314E-05, 0.26500000E+03, ESMASK(1, 6,21) = 0.10000000E+01, 0.26500000E+03, -0.75402046E+04, 0.81173515E+02, -0.29088956E+00, 0.34728320E-03, 0.00000000E+00, 0.29311069E+03, ESMASK(1, 7,21) = 0.20000000E+01, 0.29311069E+03, 0.10022400E+03, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 63 ROBLEDO 210-FT 70M AZ-EL $ ESMASK(1, 1,22) = 0.10000000E+01, 0.00000000E+00, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.28389001E+03, ESMASK(1, 2,22) = 0.10000000E+01, 0.28389001E+03, -0.13014862E+06, 0.18010964E+04, -0.93353033E+01, 0.21476801E-01, -0.18501985E-04, 0.31964001E+03, ESMASK(1, 3,22) = 0.10000000E+01, 0.31964001E+03, 0.25367563E+06, -0.29985869E+04, 0.13277709E+02, -0.26100073E-01, 0.19215948E-04, 0.35531900E+03, ESMASK(1, 4,22) = 0.10000000E+01, 0.35531900E+03, 0.60000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 65 MADRID 34M HEF - from R. F. Sunseri $ ESMASK(1, 1,23) = 0.10000000E+01, 0.00000000E+00, 0.70000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.32000000E+02, ESMASK(1, 2,23) = 0.10000000E+01, 0.32000000E+02, -0.16166024E+05, 0.19434577E+04, -0.87669750E+02, 0.17593333E+01, -0.13250000E-01, 0.36000000E+02, ESMASK(1, 3,23) = 0.10000000E+01, 0.36000000E+02, 0.70000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.24900000E+03, ESMASK(1, 4,23) = 0.10000000E+01, 0.24900000E+03, -0.19311109E+02, 0.10555152E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.25800000E+03, ESMASK(1, 5,23) = 0.10000000E+01, 0.25800000E+03, 0.14227085E+04, -0.10694387E+02, 0.20196429E-01, 0.00000000E+00, 0.00000000E+00, 0.26500000E+03, ESMASK(1, 6,23) = 0.10000000E+01, 0.26500000E+03, 0.70000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.27000000E+03, ESMASK(1, 7,23) = 0.10000000E+01, 0.27000000E+03, -0.56504197E+06, 0.80384227E+04, -0.42879921E+02, 0.10165405E+00, -0.90364797E-04, 0.28900000E+03, ESMASK(1, 8,23) = 0.10000000E+01, 0.28900000E+03, 0.70000000E+01, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.00000000E+00, 0.29300000E+03, ESMASK(1, 9,23) = 0.10000000E+01, 0.29300000E+03, 0.11498156E+06, -0.11651606E+04, 0.39355734E+01, -0.44306527E-02, 0.00000000E+00, 0.30200000E+03, ESMASK(1,10,23) = 0.10000000E+01, 0.30200000E+03, 0.25471217E+06, -0.32142283E+04, 0.15208546E+02, -0.31979315E-01, 0.25214378E-04, 0.33800000E+03, ESMASK(1,11,23) = 0.10000000E+01, 0.33800000E+03, 0.34906007E+05, -0.30158654E+03, 0.86946695E+00, -0.83614067E-03, 0.00000000E+00, 0.36000000E+03, $ $ Horizon mask for station 66 MAD3 26M X-Y $ ESMASK(1, 1,24) = 0.10000000E+01, 0.00000000E+00, 0.12000000E+02, 0.24993513E+00, -0.40909202E-01, 0.20481065E-02, -0.29618674E-04, 0.35000000E+02, ESMASK(1, 2,24) = 0.10000000E+01, 0.35000000E+02, 0.16752528E+03, -0.10797192E+02, 0.27681503E+00, -0.31351753E-02, 0.13126965E-04, 0.75800000E+02, ESMASK(1, 3,24) = 0.10000000E+01, 0.75800000E+02, -0.64016276E+04, 0.28364077E+03, -0.47262108E+01, 0.35182332E-01, -0.98704395E-04, 0.10520000E+03, ESMASK(1, 4,24) = 0.10000000E+01, 0.10520000E+03, 0.26199076E+02, -0.53202228E+00, 0.40564820E-02, -0.95542674E-05, 0.00000000E+00, 0.19080000E+03, ESMASK(1, 5,24) = 0.10000000E+01, 0.19080000E+03, 0.93291735E+04, -0.16469364E+03, 0.10866030E+01, -0.31750667E-02, 0.34686632E-05, 0.25460000E+03, ESMASK(1, 6,24) = 0.10000000E+01, 0.25460000E+03, -0.25411207E+04, 0.18953525E+02, -0.35119688E-01, 0.00000000E+00, 0.00000000E+00, 0.28500000E+03, ESMASK(1, 7,24) = 0.10000000E+01, 0.28500000E+03, -0.25640911E+04, 0.26376951E+02, -0.90468716E-01, 0.10380442E-03, 0.00000000E+00, 0.32880000E+03, ESMASK(1, 8,24) = 0.10000000E+01, 0.32880000E+03, -0.23553326E+05, 0.20709546E+03, -0.60558409E+00, 0.58930594E-03, 0.00000000E+00, 0.36000000E+03, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ BEGIN ODP $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ PV generates partial derivatives of the state with respect to the $ other dynamic parameters. The matrix is 6 X N where N <= 200. $ PARTLS( 1) = 200*' ', $ $ State partials: $ PARTLS( 1) = 'X','Y','Z','DX','DY','DZ', $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ REGRES $ $ REGRES generates observables and partials of the observables wrt to $ the parameters listed in PARTLS for each data point on the orbit $ data file. $ $ Frequency constants: $ $ 1) DPTRAJ-ODP User's Reference Manual, Vol. 1, July 1, 1990. $ UPBAND(1,1) = 14*0.0D0, SCBAND(1) = 7*0.0D0, BNDRAT(1,1) = 49*0.0D0, $ UPBAND(1,1) = 0.0D0, 96.0D0, $ S-Band up UPBAND(1,2) = 6.5D9, 32.0D0, $ X-Band up UPBAND(1,4) = 0.0D0, 232.0D0, $ C-Band up SCBAND(1) = 1.0D0, $ F1 S-Band SCBAND(2) = 3.66666666666666667D0, $ F1 X-Band BNDRAT(1,1) = 1.08597285067873303D0, $ S-Up/S-Down band ratio, 240/221 BNDRAT(1,2) = 3.98190045248868777D0, $ S-Up/X-Down band ratio, 880/221 BNDRAT(2,1) = 0.32042723631508678D0, $ X-Up/S-Down band ratio, 240/749 BNDRAT(2,2) = 1.17489986648865153D0, $ X-Up/X-Down band ratio, 880/749 BNDRAT(4,3) = 0.33480176211453744D0, $ L-Up/C-Down band ratio, 228/681 $ STNCOR = 2, $ STNMOD( 1) = 20*.FALSE., $ $ STNMOD( 1) = .TRUE., $ The solid earth tide model is on. $ STNMOD( 4) = .TRUE., $ Polar motion. $ STNMOD( 6) = .TRUE., $ Lorentz contraction / relativistic scaling. $ STNMOD(10) = .TRUE., $ The solid earth tides are to 1st order. $ STNMOD(12) = .TRUE., $ ET - TAI "vector" calculation. $ STNMOD(1) = .TRUE. $ solid tides on STNMOD(2) = .TRUE. $ pole tide on STNMOD(3) = .TRUE. $ ocean loading on STNMOD(4) = .TRUE. $ polar motion on STNMOD(5) = .TRUE. $ vector ET-TAI conversion STNMOD(6) = .TRUE. $ convert geocentric to barycentric when necessary STNMOD(7) = .TRUE. $ plate motion STNMOD(8) = .FALSE. $ supplied coordinates are w.r.t center of mass STNMOD(9) = .FALSE. $ permanent solid tide included in solid tide model STNMOD(10)= .TRUE. $ first order solid tide STNMOD(11)= .TRUE. $ second order solid tide STNMOD(12)= .TRUE. $ use vector formulation ET-TAI STNMOD(13)=8*.FALSE. $ not used as of 20 October 1996 version of REGRES $ TIDLOV(1) = 0.6090D0, TIDLOV(2) = 0.0852D0, TIDEPS = 0.0D0, $ Phase offset for the Earth tide (degrees). $ REFCOR = .TRUE., $ Troposphere refraction correction. LTCRIT = 0.1D0, $ LT convergence criterion (seconds, recommended). NOLT = 4, $ LT iterations (recommended). RLTBOD( 4) = .FALSE., $ Relativistic LT delay due to Mars is off. RLTBOD( 5) = .TRUE., $ Relativistic LT delay due to Jupiter is on. RLTBOD( 6) = .FALSE., $ Relativistic LT delay due to Saturn is off. RLTBOD(10) = .TRUE., $ Relativistic LT delay due to Sol is on. $ $ High Gain Antenna model (this model nominally for Mars Observer only and $ is turned off here): $ HGAON = .FALSE., $ The high gain antenna model is off. HGAON2 = .FALSE., HGAS2H = 0.0D0, $ Coordinates of the s/c HGA gimbal axes in the 0.0D0, $ S/C body coordinate system. 0.0D0, HGAH2A = 0.0D0, $ HGA phase center coordinates. 0.0D0, 0.0D0, HGAGAM = 0.0D0, $ Angle to transform between the s/c body coordinate $ system to the s/c gimbal coordinate system. $ HGATIM(1) = '17-FEB-1996 00:00:00.0000', $ $ Center of mass wrt the S/C body coordinate system: $ HGAS2C(1,1) = 300*0.0D0, $ $ Range (SRA) biases: $ FRC(1) = 15, 45, 65, ODRC(1) = '17-FEB-1996 00:00:00', DRC(2,1) = 0.0D0, ODRC(2) = '17-FEB-1996 00:00:00', DRC(2,2) = 0.0D0, ODRC(3) = '17-FEB-1996 00:00:00', DRC(2,3) = 0.0D0, $ $ One-way Doppler (F1) drift: $ DRIFT(1,1) = 204*0.0D0, ODRIFT(1) = '17-FEB-1996 00:00:00', ODRIFT(2) = '31-MAR-2000 00:00:00', $ $ Corrections between UTC and each station: $ FSTPOL(1) = 15, 45, 65, ODSTPO(1) = 100*' ', DSTPOL(1,1) = 400*0.0D0, $ $ Basically, an epoch offset between station time and UTC causes an error $ in the geometry of the computed observable. The data from the Frequency $ & Timing System Clock Reports will correct the computed observables for $ Doppler (F2) and differenced Doppler (F2MF3). $ $ The FTS Clock Reports provide the following clock epoch offset data: $ $ SPC10 - UTC; SPC40 - SPC10; SPC60 - SPC10 $ $ and this data should be applied in this manner: $ $ DSTPOL(2,1) = (SPC10 - UTC) $ DSS 15. $ DSTPOL(2,2) = (SPC10 - UTC) + (SPC40 - SPC10) $ DSS 45. $ DSTPOL(2,3) = (SPC10 - UTC) + (SPC60 - SPC10) $ DSS 65. $ $ The STOIC information file: $ UT1TYP = 'UT1R', $ $ Timing deck $ 1 - 37: A1-UTC: EPOCH(SEC), UTC(SEC), DUTC(SEC/SEC) $ 40 - 148: A1-UT1: EPOCH(SEC), UT1(SEC), DUTC(SEC/SEC) $ 151 - 331: MOTION: EPOCH(SEC), X1(ARC S), DX1(ARC S/UTC S) $ Y1(ARC S), DY1(ARC S/UTC SEC) $ TIMPOL='STOIC/KEOF.LD961024/PT970104 . PREDICTS->970104. UT1TYP=UT1R.', IT( 1)=950415,TP( 1)= -148824000., 29.000000, 0.0000E-10, IT( 4)=960101,TP( 4)= -126273600., 30.000000, 0.0000E-10, IT( 7)=100101,TP( 7)= 315576000., 45.000000, 0.0000E-10, IT( 10)=991231,TP( 10)= 0., 0.000000, 0.0000E-10, IT( 13)=991231,TP( 13)= 0., 0.000000, 0.0000E-10, IT( 16)=991231,TP( 16)= 0., 0.000000, 0.0000E-10, IT( 19)=991231,TP( 19)= 0., 0.000000, 0.0000E-10, IT( 22)=991231,TP( 22)= 0., 0.000000, 0.0000E-10, IT( 25)=991231,TP( 25)= 0., 0.000000, 0.0000E-10, IT( 28)=991231,TP( 28)= 0., 0.000000, 0.0000E-10, IT( 31)=991231,TP( 31)= 0., 0.000000, 0.0000E-10, IT( 34)=991231,TP( 34)= 0., 0.000000, 0.0000E-10, IT( 37)=991231,TP( 37)= 0., 0.000000, 0.0000E-10, IT( 40)=950415,TP( 40)= -148824000., 28.882050, 318.4430E-10, IT( 43)=950503,TP( 43)= -147268800., 28.931231, 315.7280E-10, IT( 46)=950521,TP( 46)= -145713600., 28.978901, 272.6700E-10, IT( 49)=950608,TP( 49)= -144158400., 29.019630, 249.3340E-10, IT( 52)=950626,TP( 52)= -142603200., 29.055031, 188.8750E-10, IT( 55)=950714,TP( 55)= -141048000., 29.081930, 161.7040E-10, IT( 58)=950801,TP( 58)= -139492800., 29.104891, 139.0660E-10, IT( 61)=950819,TP( 61)= -137937600., 29.130329, 189.7410E-10, IT( 64)=950906,TP( 64)= -136382400., 29.164141, 237.0330E-10, IT( 67)=950924,TP( 67)= -134827200., 29.202829, 275.7090E-10, IT( 70)=951012,TP( 70)= -133272000., 29.246260, 276.5130E-10, IT( 73)=951030,TP( 73)= -131716800., 29.286970, 276.0720E-10, IT( 76)=951117,TP( 76)= -130161600., 29.331030, 297.2430E-10, IT( 79)=951205,TP( 79)= -128606400., 29.377390, 290.5410E-10, IT( 82)=951223,TP( 82)= -127051200., 29.422079, 277.4880E-10, IT( 85)=960110,TP( 85)= -125496000., 29.461220, 226.2200E-10, IT( 88)=960128,TP( 88)= -123940800., 29.493389, 199.7020E-10, IT( 91)=960215,TP( 91)= -122385600., 29.527870, 232.5780E-10, IT( 94)=960304,TP( 94)= -120830400., 29.566561, 274.8540E-10, IT( 97)=960322,TP( 97)= -119275200., 29.607840, 251.3290E-10, IT(100)=960409,TP(100)= -117720000., 29.648899, 275.4130E-10, IT(103)=960427,TP(103)= -116164800., 29.689569, 263.9790E-10, IT(106)=960515,TP(106)= -114609600., 29.732430, 268.0240E-10, IT(109)=960602,TP(109)= -113054400., 29.767660, 194.0750E-10, IT(112)=960620,TP(112)= -111499200., 29.798000, 171.8010E-10, IT(115)=960708,TP(115)= -109944000., 29.820910, 124.6940E-10, IT(118)=960726,TP(118)= -108388800., 29.842600, 152.7400E-10, IT(121)=960813,TP(121)= -106833600., 29.863831, 119.1660E-10, IT(124)=960831,TP(124)= -105278400., 29.884670, 157.4230E-10, IT(127)=960918,TP(127)= -103723200., 29.911221, 199.7500E-10, IT(130)=961006,TP(130)= -102168000., 29.944510, 218.5800E-10, IT(133)=961024,TP(133)= -100612800., 29.980659, 233.6580E-10, IT(136)=961111,TP(136)= -99057600., 30.016769, 230.8480E-10, IT(139)=961129,TP(139)= -97502400., 30.051840, 218.1720E-10, IT(142)=961217,TP(142)= -95947200., 30.084591, 203.0600E-10, IT(145)=970104,TP(145)= -94392000., 30.115240, 192.8490E-10, IT(148)=100101,TP(148)= 315576000., 45.000000, 317.0000E-10, IT(151)=950415,TP(151)= -148824000.,0.07510,0.38670E-07,0.55570,-.44320E-08, IT(156)=950503,TP(156)= -147268800.,0.14070,0.40160E-07,0.54060,-.17720E-07, IT(161)=950521,TP(161)= -145713600.,0.19770,0.22970E-07,0.51090,-.28180E-07, IT(166)=950608,TP(166)= -144158400.,0.24040,0.32210E-07,0.46110,-.32090E-07, IT(171)=950626,TP(171)= -142603200.,0.27470,0.84680E-08,0.40250,-.41350E-07, IT(176)=950714,TP(176)= -141048000.,0.28750,0.30190E-09,0.33270,-.41240E-07, IT(181)=950801,TP(181)= -139492800.,0.27970,-.10230E-07,0.26350,-.45310E-07, IT(186)=950819,TP(186)= -137937600.,0.25330,-.23650E-07,0.19940,-.33180E-07, IT(191)=950906,TP(191)= -136382400.,0.21250,-.30580E-07,0.15200,-.22910E-07, IT(196)=950924,TP(196)= -134827200.,0.15870,-.36580E-07,0.11380,-.17730E-07, IT(201)=951012,TP(201)= -133272000.,0.09430,-.43800E-07,0.09170,-.16710E-07, IT(206)=951030,TP(206)= -131716800.,0.03190,-.40000E-07,0.08130,0.21000E-09, IT(211)=951117,TP(211)= -130161600.,-.03320,-.48690E-07,0.08950,0.16200E-07, IT(216)=951205,TP(216)= -128606400.,-.10880,-.48410E-07,0.11660,0.22620E-07, IT(221)=951223,TP(221)= -127051200.,-.15880,-.22450E-07,0.16290,0.38870E-07, IT(226)=960110,TP(226)= -125496000.,-.18870,-.21160E-07,0.21750,0.31270E-07, IT(231)=960128,TP(231)= -123940800.,-.21570,-.17900E-07,0.27680,0.43600E-07, IT(236)=960215,TP(236)= -122385600.,-.22000,0.85190E-08,0.33880,0.46450E-07, IT(241)=960304,TP(241)= -120830400.,-.21260,0.20650E-07,0.41000,0.47690E-07, IT(246)=960322,TP(246)= -119275200.,-.17720,0.23060E-07,0.47710,0.40180E-07, IT(251)=960409,TP(251)= -117720000.,-.13510,0.30810E-07,0.52430,0.29190E-07, IT(256)=960427,TP(256)= -116164800.,-.07630,0.48150E-07,0.56520,0.18930E-07, IT(261)=960515,TP(261)= -114609600.,-.00370,0.43910E-07,0.59080,0.93990E-08, IT(266)=960602,TP(266)= -113054400.,0.06990,0.49410E-07,0.59480,-.86340E-08, IT(271)=960620,TP(271)= -111499200.,0.14150,0.41660E-07,0.56880,-.20610E-07, IT(276)=960708,TP(276)= -109944000.,0.20340,0.45430E-07,0.52780,-.25920E-07, IT(281)=960726,TP(281)= -108388800.,0.24690,0.18930E-07,0.47690,-.33870E-07, IT(286)=960813,TP(286)= -106833600.,0.28010,0.23550E-07,0.41480,-.39570E-07, IT(291)=960831,TP(291)= -105278400.,0.29720,-.37760E-08,0.34700,-.52110E-07, IT(296)=960918,TP(296)= -103723200.,0.28370,-.93420E-08,0.27420,-.46990E-07, IT(301)=961006,TP(301)= -102168000.,0.25800,-.22830E-07,0.20870,-.39030E-07, IT(306)=961024,TP(306)= -100612800.,0.21450,-.30960E-07,0.15840,-.26540E-07, IT(311)=961111,TP(311)= -99057600.,0.16170,-.36830E-07,0.12370,-.17720E-07, IT(316)=961129,TP(316)= -97502400.,0.10140,-.40240E-07,0.10390,-.75830E-08, IT(321)=961217,TP(321)= -95947200.,0.03800,-.40790E-07,0.10040,0.30660E-08, IT(326)=970104,TP(326)= -94392000.,-.02400,-.38450E-07,0.11330,0.13470E-07, IT(331)=100101,TP(331)= 315576000.,0.00000,0.00000E+00,0.25000,0.00000E+00, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Earth Orientation Parameter (EOP) File $ $ 1) Herbert Royden, Section 335, JPL. $ $ A model of Earth motions. Values are updated about twice a week by TSAC. $ This file replaces the older time & polar motion (STOIC) files produced by $ TSAC in the past. A typical element follows: $ $ JPL Earth Orientation Parameter File $ Last Data Point 22-SEP-1997 $ Predicts to 28-OCT-1997 $ EOPLBL='EOP. LAST DATUM 22-SEP-1997. PREDICTS->28-OCT-1997, UT1TYP=UT1. ' EOPFNG='Enter MAKE_EOP 23-SEP-1997 23:31:53 linked 14-MAR-1996 23:32:11 EOPUT1='UT1' EOPTYP='EOP' EOPTIM='23-SEP-1997 23:31:53 ' EOPTRF='ITRF93' EOPCRF='ICRF93' $ $ MJD PM x PM y TAI-UT1 TAI-UTC dPsi dEps $ (mas) (mas) (sec) (sec) (mas) (mas) EOP= 50383.0, 206.30, 148.70, 29.988020, 30.0, -40.53, -7.38, $ 27-OCT-1996 50384.0, 204.10, 145.80, 29.990050, 30.0, -40.50, -7.33, $ 28-OCT-1996 50385.0, 201.80, 142.90, 29.991930, 30.0, -40.46, -7.19, $ 29-OCT-1996 50386.0, 199.50, 140.00, 29.993670, 30.0, -40.35, -7.13, $ 30-OCT-1996 50387.0, 196.80, 137.10, 29.995340, 30.0, -40.08, -7.22, $ 31-OCT-1996 50388.0, 194.00, 134.10, 29.996960, 30.0, -39.62, -7.42, $ 1-NOV-1996 50389.0, 191.10, 131.20, 29.998570, 30.0, -39.07, -7.58, $ 2-NOV-1996 50390.0, 188.00, 128.30, 30.000270, 30.0, -38.60, -7.62, $ 3-NOV-1996 50391.0, 184.70, 125.80, 30.002080, 30.0, -38.35, -7.55, $ 4-NOV-1996 50392.0, 181.30, 123.60, 30.004010, 30.0, -38.32, -7.44, $ 5-NOV-1996 50393.0, 177.50, 121.80, 30.006060, 30.0, -38.41, -7.34, $ 6-NOV-1996 50394.0, 173.60, 120.00, 30.008200, 30.0, -38.51, -7.19, $ 7-NOV-1996 50395.0, 169.70, 118.20, 30.010390, 30.0, -38.59, -6.97, $ 8-NOV-1996 50396.0, 165.80, 116.20, 30.012570, 30.0, -38.68, -6.69, $ 9-NOV-1996 50397.0, 161.90, 114.40, 30.014690, 30.0, -38.77, -6.46, $ 10-NOV-1996 50398.0, 158.10, 112.70, 30.016790, 30.0, -38.77, -6.44, $ 11-NOV-1996 50399.0, 154.10, 111.30, 30.018830, 30.0, -38.61, -6.65, $ 12-NOV-1996 50400.0, 149.90, 110.00, 30.020840, 30.0, -38.32, -6.92, $ 13-NOV-1996 50401.0, 145.50, 108.70, 30.022810, 30.0, -38.10, -7.05, $ 14-NOV-1996 50402.0, 141.10, 107.10, 30.024700, 30.0, -38.05, -6.93, $ 15-NOV-1996 50403.0, 137.00, 105.40, 30.026540, 30.0, -38.16, -6.67, $ 16-NOV-1996 50404.0, 133.40, 103.50, 30.028450, 30.0, -38.27, -6.42, $ 17-NOV-1996 50405.0, 130.30, 101.80, 30.030490, 30.0, -38.26, -6.25, $ 18-NOV-1996 50406.0, 127.40, 100.40, 30.032580, 30.0, -38.14, -6.13, $ 19-NOV-1996 50407.0, 124.50, 99.30, 30.034730, 30.0, -38.02, -6.02, $ 20-NOV-1996 50408.0, 121.60, 98.50, 30.036880, 30.0, -38.04, -5.95, $ 21-NOV-1996 50409.0, 118.60, 97.70, 30.039000, 30.0, -38.24, -5.99, $ 22-NOV-1996 50410.0, 115.40, 96.90, 30.040970, 30.0, -38.48, -6.10, $ 23-NOV-1996 50411.0, 112.00, 96.10, 30.042810, 30.0, -38.53, -6.20, $ 24-NOV-1996 50412.0, 108.40, 95.20, 30.044540, 30.0, -38.33, -6.22, $ 25-NOV-1996 50413.0, 104.60, 94.30, 30.046190, 30.0, -38.03, -6.16, $ 26-NOV-1996 50414.0, 100.80, 93.60, 30.047790, 30.0, -37.80, -6.09, $ 27-NOV-1996 50415.0, 96.80, 93.10, 30.049370, 30.0, -37.59, -6.08, $ 28-NOV-1996 50416.0, 92.90, 92.60, 30.050950, 30.0, -37.26, -6.15, $ 29-NOV-1996 50417.0, 89.10, 92.10, 30.052550, 30.0, -36.85, -6.22, $ 30-NOV-1996 50418.0, 85.30, 91.40, 30.054200, 30.0, -36.54, -6.21, $ 1-DEC-1996 50419.0, 81.70, 90.70, 30.055890, 30.0, -36.43, -6.14, $ 2-DEC-1996 50420.0, 78.00, 90.10, 30.057600, 30.0, -36.42, -6.05, $ 3-DEC-1996 50421.0, 74.20, 89.60, 30.059320, 30.0, -36.43, -5.95, $ 4-DEC-1996 50422.0, 70.20, 89.00, 30.061100, 30.0, -36.52, -5.88, $ 5-DEC-1996 50423.0, 66.00, 88.30, 30.062930, 30.0, -36.76, -5.78, $ 6-DEC-1996 50424.0, 61.80, 87.40, 30.064730, 30.0, -37.02, -5.63, $ 7-DEC-1996 50425.0, 57.60, 86.50, 30.066490, 30.0, -37.12, -5.47, $ 8-DEC-1996 50426.0, 53.70, 85.50, 30.068180, 30.0, -37.00, -5.43, $ 9-DEC-1996 50427.0, 49.80, 84.70, 30.069820, 30.0, -36.76, -5.63, $ 10-DEC-1996 50428.0, 46.10, 84.20, 30.071440, 30.0, -36.54, -5.96, $ 11-DEC-1996 50429.0, 42.50, 83.90, 30.073110, 30.0, -36.39, -6.13, $ 12-DEC-1996 50430.0, 39.20, 83.80, 30.074840, 30.0, -36.35, -5.96, $ 13-DEC-1996 50431.0, 36.20, 84.00, 30.076670, 30.0, -36.40, -5.55, $ 14-DEC-1996 50432.0, 33.20, 84.50, 30.078640, 30.0, -36.51, -5.17, $ 15-DEC-1996 50433.0, 30.30, 85.20, 30.080730, 30.0, -36.61, -4.99, $ 16-DEC-1996 50434.0, 27.30, 86.00, 30.082880, 30.0, -36.68, -4.97, $ 17-DEC-1996 50435.0, 24.10, 86.70, 30.085040, 30.0, -36.75, -5.03, $ 18-DEC-1996 50436.0, 20.90, 87.50, 30.087190, 30.0, -36.89, -5.15, $ 19-DEC-1996 50437.0, 17.70, 88.10, 30.089290, 30.0, -37.12, -5.31, $ 20-DEC-1996 50438.0, 14.70, 88.60, 30.091250, 30.0, -37.37, -5.44, $ 21-DEC-1996 50439.0, 11.80, 89.10, 30.093080, 30.0, -37.45, -5.48, $ 22-DEC-1996 50440.0, 9.20, 89.60, 30.094840, 30.0, -37.28, -5.46, $ 23-DEC-1996 50441.0, 6.70, 90.10, 30.096560, 30.0, -37.00, -5.42, $ 24-DEC-1996 50442.0, 3.90, 90.60, 30.098220, 30.0, -36.82, -5.38, $ 25-DEC-1996 50443.0, 0.90, 91.00, 30.099900, 30.0, -36.73, -5.37, $ 26-DEC-1996 50444.0, -2.60, 91.40, 30.101590, 30.0, -36.59, -5.40, $ 27-DEC-1996 50445.0, -6.50, 91.80, 30.103350, 30.0, -36.34, -5.42, $ 28-DEC-1996 50446.0, -10.70, 92.40, 30.105180, 30.0, -36.14, -5.43, $ 29-DEC-1996 50447.0, -15.10, 93.10, 30.107090, 30.0, -36.10, -5.41, $ 30-DEC-1996 50448.0, -19.50, 93.80, 30.109050, 30.0, -36.10, -5.38, $ 31-DEC-1996 50449.0, -23.60, 94.60, 30.111020, 30.0, -36.07, -5.36, $ 1-JAN-1997 50450.0, -27.30, 95.40, 30.113030, 30.0, -36.17, -5.37, $ 2-JAN-1997 50451.0, -31.00, 96.20, 30.115040, 30.0, -36.53, -5.44, $ 3-JAN-1997 50452.0, -34.50, 97.20, 30.117020, 30.0, -36.97, -5.49, $ 4-JAN-1997 50453.0, -37.90, 98.40, 30.118940, 30.0, -37.16, -5.42, $ 5-JAN-1997 50454.0, -41.40, 99.60, 30.120830, 30.0, -37.05, -5.30, $ 6-JAN-1997 50455.0, -44.80, 101.00, 30.122670, 30.0, -36.87, -5.32, $ 7-JAN-1997 50456.0, -48.00, 102.20, 30.124510, 30.0, -36.81, -5.54, $ 8-JAN-1997 50457.0, -51.00, 103.40, 30.126380, 30.0, -36.81, -5.74, $ 9-JAN-1997 50458.0, -53.90, 104.60, 30.128340, 30.0, -36.72, -5.64, $ 10-JAN-1997 50459.0, -56.60, 105.70, 30.130410, 30.0, -36.54, -5.28, $ 11-JAN-1997 50460.0, -59.30, 106.90, 30.132580, 30.0, -36.38, -4.92, $ 12-JAN-1997 50461.0, -62.00, 108.20, 30.134790, 30.0, -36.34, -4.76, $ 13-JAN-1997 50462.0, -64.40, 109.60, 30.137030, 30.0, -36.49, -4.75, $ 14-JAN-1997 50463.0, -66.50, 111.20, 30.139240, 30.0, -36.78, -4.83, $ 15-JAN-1997 50464.0, -68.60, 113.20, 30.141340, 30.0, -37.07, -5.01, $ 16-JAN-1997 50465.0, -70.60, 115.30, 30.143320, 30.0, -37.28, -5.27, $ 17-JAN-1997 50466.0, -72.60, 117.40, 30.145150, 30.0, -37.38, -5.50, $ 18-JAN-1997 50467.0, -74.80, 119.60, 30.146810, 30.0, -37.42, -5.60, $ 19-JAN-1997 50468.0, -77.30, 121.70, 30.148340, 30.0, -37.38, -5.59, $ 20-JAN-1997 50469.0, -79.90, 123.70, 30.149770, 30.0, -37.27, -5.58, $ 21-JAN-1997 50470.0, -82.70, 125.70, 30.151190, 30.0, -37.16, -5.60, $ 22-JAN-1997 50471.0, -85.40, 127.50, 30.152640, 30.0, -37.06, -5.63, $ 23-JAN-1997 50472.0, -88.20, 129.30, 30.154110, 30.0, -36.95, -5.64, $ 24-JAN-1997 50473.0, -91.10, 131.10, 30.155600, 30.0, -36.76, -5.65, $ 25-JAN-1997 50474.0, -94.00, 132.90, 30.157110, 30.0, -36.59, -5.68, $ 26-JAN-1997 50475.0, -97.10, 134.70, 30.158680, 30.0, -36.54, -5.74, $ 27-JAN-1997 50476.0, -100.20, 136.50, 30.160320, 30.0, -36.56, -5.81, $ 28-JAN-1997 50477.0, -103.30, 138.40, 30.162000, 30.0, -36.63, -5.87, $ 29-JAN-1997 50478.0, -106.40, 140.40, 30.163610, 30.0, -36.82, -5.95, $ 30-JAN-1997 50479.0, -109.30, 142.40, 30.165140, 30.0, -37.24, -6.11, $ 31-JAN-1997 50480.0, -112.30, 144.40, 30.166640, 30.0, -37.69, -6.28, $ 1-FEB-1997 50481.0, -115.20, 146.50, 30.168010, 30.0, -37.87, -6.29, $ 2-FEB-1997 50482.0, -117.90, 148.70, 30.169310, 30.0, -37.76, -6.12, $ 3-FEB-1997 50483.0, -120.50, 151.00, 30.170570, 30.0, -37.64, -5.97, $ 4-FEB-1997 50484.0, -123.00, 153.30, 30.171890, 30.0, -37.73, -6.05, $ 5-FEB-1997 50485.0, -125.20, 155.70, 30.173330, 30.0, -37.91, -6.26, $ 6-FEB-1997 50486.0, -127.20, 158.10, 30.174940, 30.0, -37.89, -6.30, $ 7-FEB-1997 50487.0, -129.10, 160.60, 30.176760, 30.0, -37.59, -6.13, $ 8-FEB-1997 50488.0, -131.00, 163.30, 30.178730, 30.0, -37.16, -5.93, $ 9-FEB-1997 50489.0, -132.80, 166.10, 30.180760, 30.0, -36.89, -5.87, $ 10-FEB-1997 50490.0, -134.70, 168.90, 30.182840, 30.0, -36.97, -5.87, $ 11-FEB-1997 50491.0, -136.60, 171.70, 30.184910, 30.0, -37.38, -5.86, $ 12-FEB-1997 50492.0, -138.70, 174.30, 30.186860, 30.0, -37.82, -5.93, $ 13-FEB-1997 50493.0, -140.80, 177.00, 30.188640, 30.0, -38.00, -6.18, $ 14-FEB-1997 50494.0, -143.20, 179.70, 30.190300, 30.0, -37.94, -6.51, $ 15-FEB-1997 50495.0, -145.70, 182.50, 30.191920, 30.0, -37.88, -6.76, $ 16-FEB-1997 50496.0, -148.20, 185.20, 30.193440, 30.0, -37.94, -6.87, $ 17-FEB-1997 50497.0, -150.80, 187.70, 30.194960, 30.0, -37.95, -6.94, $ 18-FEB-1997 50498.0, -153.30, 190.00, 30.196520, 30.0, -37.75, -7.01, $ 19-FEB-1997 50499.0, -155.60, 192.30, 30.198140, 30.0, -37.42, -7.02, $ 20-FEB-1997 50500.0, -157.60, 194.60, 30.199820, 30.0, -37.12, -6.95, $ 21-FEB-1997 50501.0, -159.40, 197.00, 30.201600, 30.0, -36.92, -6.86, $ 22-FEB-1997 50502.0, -160.90, 199.70, 30.203480, 30.0, -36.78, -6.84, $ 23-FEB-1997 50503.0, -162.50, 202.70, 30.205430, 30.0, -36.73, -6.93, $ 24-FEB-1997 50504.0, -164.10, 205.80, 30.207450, 30.0, -36.81, -7.08, $ 25-FEB-1997 50505.0, -165.90, 209.10, 30.209480, 30.0, -37.00, -7.22, $ 26-FEB-1997 50506.0, -168.20, 212.30, 30.211480, 30.0, -37.29, -7.33, $ 27-FEB-1997 50507.0, -170.60, 215.60, 30.213470, 30.0, -37.64, -7.48, $ 28-FEB-1997 50508.0, -172.70, 218.80, 30.215500, 30.0, -37.90, -7.68, $ 1-MAR-1997 50509.0, -174.40, 221.90, 30.217530, 30.0, -37.91, -7.78, $ 2-MAR-1997 50510.0, -175.60, 225.10, 30.219560, 30.0, -37.65, -7.69, $ 3-MAR-1997 50511.0, -176.40, 228.40, 30.221610, 30.0, -37.40, -7.53, $ 4-MAR-1997 50512.0, -177.20, 231.80, 30.223720, 30.0, -37.37, -7.53, $ 5-MAR-1997 50513.0, -178.00, 235.10, 30.225980, 30.0, -37.52, -7.67, $ 6-MAR-1997 50514.0, -179.20, 238.40, 30.228410, 30.0, -37.59, -7.75, $ 7-MAR-1997 50515.0, -180.90, 241.60, 30.231010, 30.0, -37.42, -7.69, $ 8-MAR-1997 50516.0, -182.80, 244.70, 30.233810, 30.0, -37.08, -7.63, $ 9-MAR-1997 50517.0, -184.70, 247.70, 30.236670, 30.0, -36.82, -7.70, $ 10-MAR-1997 50518.0, -186.10, 250.80, 30.239520, 30.0, -36.87, -7.78, $ 11-MAR-1997 50519.0, -187.00, 254.00, 30.242260, 30.0, -37.26, -7.75, $ 12-MAR-1997 50520.0, -187.40, 257.50, 30.244850, 30.0, -37.71, -7.69, $ 13-MAR-1997 50521.0, -187.60, 261.30, 30.247300, 30.0, -37.86, -7.81, $ 14-MAR-1997 50522.0, -187.70, 265.20, 30.249670, 30.0, -37.68, -8.12, $ 15-MAR-1997 50523.0, -188.00, 269.10, 30.252010, 30.0, -37.53, -8.43, $ 16-MAR-1997 50524.0, -188.40, 272.90, 30.254360, 30.0, -37.58, -8.66, $ 17-MAR-1997 50525.0, -188.90, 276.60, 30.256730, 30.0, -37.63, -8.79, $ 18-MAR-1997 50526.0, -189.20, 280.20, 30.259130, 30.0, -37.37, -8.84, $ 19-MAR-1997 50527.0, -189.50, 283.90, 30.261560, 30.0, -36.87, -8.79, $ 20-MAR-1997 50528.0, -189.70, 287.50, 30.264020, 30.0, -36.47, -8.61, $ 21-MAR-1997 50529.0, -189.80, 291.10, 30.266530, 30.0, -36.32, -8.40, $ 22-MAR-1997 50530.0, -189.90, 294.80, 30.269070, 30.0, -36.33, -8.28, $ 23-MAR-1997 50531.0, -189.90, 298.60, 30.271630, 30.0, -36.39, -8.31, $ 24-MAR-1997 50532.0, -189.90, 302.40, 30.274210, 30.0, -36.53, -8.44, $ 25-MAR-1997 50533.0, -190.10, 306.40, 30.276770, 30.0, -36.78, -8.62, $ 26-MAR-1997 50534.0, -190.50, 310.40, 30.279280, 30.0, -37.04, -8.78, $ 27-MAR-1997 50535.0, -191.00, 314.20, 30.281720, 30.0, -37.23, -8.94, $ 28-MAR-1997 50536.0, -191.60, 317.90, 30.284140, 30.0, -37.28, -9.11, $ 29-MAR-1997 50537.0, -192.00, 321.30, 30.286550, 30.0, -37.18, -9.24, $ 30-MAR-1997 50538.0, -192.10, 324.60, 30.288940, 30.0, -36.92, -9.26, $ 31-MAR-1997 50539.0, -191.70, 328.00, 30.291360, 30.0, -36.60, -9.20, $ 1-APR-1997 50540.0, -191.00, 331.60, 30.293870, 30.0, -36.33, -9.15, $ 2-APR-1997 50541.0, -190.00, 335.50, 30.296480, 30.0, -36.19, -9.14, $ 3-APR-1997 50542.0, -189.00, 339.40, 30.299230, 30.0, -36.15, -9.07, $ 4-APR-1997 50543.0, -188.00, 343.20, 30.302130, 30.0, -36.15, -8.91, $ 5-APR-1997 50544.0, -186.90, 346.80, 30.305110, 30.0, -36.17, -8.84, $ 6-APR-1997 50545.0, -186.00, 350.30, 30.308050, 30.0, -36.25, -8.97, $ 7-APR-1997 50546.0, -185.10, 353.80, 30.310900, 30.0, -36.46, -9.17, $ 8-APR-1997 50547.0, -184.20, 357.40, 30.313620, 30.0, -36.81, -9.24, $ 9-APR-1997 50548.0, -183.30, 361.00, 30.316180, 30.0, -37.10, -9.17, $ 10-APR-1997 50549.0, -182.30, 364.60, 30.318580, 30.0, -37.13, -9.16, $ 11-APR-1997 50550.0, -181.40, 368.30, 30.320870, 30.0, -36.91, -9.33, $ 12-APR-1997 50551.0, -180.70, 372.10, 30.323090, 30.0, -36.72, -9.61, $ 13-APR-1997 50552.0, -180.10, 375.90, 30.325280, 30.0, -36.76, -9.86, $ 14-APR-1997 50553.0, -179.60, 379.50, 30.327470, 30.0, -36.84, -10.01, $ 15-APR-1997 50554.0, -179.00, 382.80, 30.329680, 30.0, -36.68, -10.05, $ 16-APR-1997 50555.0, -178.40, 385.90, 30.331950, 30.0, -36.29, -9.94, $ 17-APR-1997 50556.0, -177.60, 389.00, 30.334250, 30.0, -36.02, -9.74, $ 18-APR-1997 50557.0, -176.60, 392.30, 30.336600, 30.0, -36.05, -9.54, $ 19-APR-1997 50558.0, -175.70, 395.70, 30.338940, 30.0, -36.26, -9.39, $ 20-APR-1997 50559.0, -174.80, 399.30, 30.341310, 30.0, -36.47, -9.32, $ 21-APR-1997 50560.0, -174.10, 402.90, 30.343650, 30.0, -36.66, -9.36, $ 22-APR-1997 50561.0, -173.40, 406.50, 30.345900, 30.0, -36.88, -9.50, $ 23-APR-1997 50562.0, -172.50, 410.00, 30.348050, 30.0, -37.04, -9.69, $ 24-APR-1997 50563.0, -171.10, 413.40, 30.350130, 30.0, -37.06, -9.90, $ 25-APR-1997 50564.0, -169.50, 416.70, 30.352150, 30.0, -36.97, -10.07, $ 26-APR-1997 50565.0, -167.90, 419.80, 30.354120, 30.0, -36.92, -10.16, $ 27-APR-1997 50566.0, -166.50, 422.80, 30.356080, 30.0, -36.92, -10.14, $ 28-APR-1997 50567.0, -165.30, 425.60, 30.358050, 30.0, -36.84, -10.07, $ 29-APR-1997 50568.0, -164.20, 428.20, 30.360100, 30.0, -36.59, -9.99, $ 30-APR-1997 50569.0, -163.00, 430.80, 30.362270, 30.0, -36.23, -9.86, $ 1-MAY-1997 50570.0, -161.50, 433.40, 30.364550, 30.0, -35.93, -9.65, $ 2-MAY-1997 50571.0, -159.50, 436.00, 30.366920, 30.0, -35.85, -9.38, $ 3-MAY-1997 50572.0, -157.00, 438.80, 30.369400, 30.0, -36.07, -9.21, $ 4-MAY-1997 50573.0, -154.20, 441.80, 30.371920, 30.0, -36.52, -9.28, $ 5-MAY-1997 50574.0, -151.40, 445.00, 30.374400, 30.0, -37.03, -9.51, $ 6-MAY-1997 50575.0, -148.70, 448.30, 30.376810, 30.0, -37.39, -9.72, $ 7-MAY-1997 50576.0, -145.80, 451.40, 30.379050, 30.0, -37.49, -9.75, $ 8-MAY-1997 50577.0, -142.80, 454.40, 30.381170, 30.0, -37.34, -9.70, $ 9-MAY-1997 50578.0, -139.70, 457.30, 30.383230, 30.0, -37.08, -9.73, $ 10-MAY-1997 50579.0, -136.90, 460.20, 30.385210, 30.0, -36.93, -9.89, $ 11-MAY-1997 50580.0, -134.30, 462.90, 30.387170, 30.0, -36.95, -10.12, $ 12-MAY-1997 50581.0, -132.10, 465.60, 30.389130, 30.0, -37.04, -10.28, $ 13-MAY-1997 50582.0, -130.10, 468.10, 30.391080, 30.0, -37.02, -10.31, $ 14-MAY-1997 50583.0, -128.00, 470.40, 30.393040, 30.0, -36.89, -10.23, $ 15-MAY-1997 50584.0, -125.70, 472.50, 30.395010, 30.0, -36.83, -10.08, $ 16-MAY-1997 50585.0, -123.00, 474.50, 30.397020, 30.0, -36.97, -9.96, $ 17-MAY-1997 50586.0, -120.00, 476.70, 30.399070, 30.0, -37.29, -9.85, $ 18-MAY-1997 50587.0, -117.00, 479.20, 30.401150, 30.0, -37.64, -9.74, $ 19-MAY-1997 50588.0, -114.00, 481.80, 30.403250, 30.0, -37.94, -9.63, $ 20-MAY-1997 50589.0, -111.20, 484.60, 30.405350, 30.0, -38.16, -9.60, $ 21-MAY-1997 50590.0, -108.70, 487.20, 30.407390, 30.0, -38.23, -9.72, $ 22-MAY-1997 50591.0, -106.30, 489.60, 30.409400, 30.0, -38.14, -9.95, $ 23-MAY-1997 50592.0, -104.10, 491.90, 30.411360, 30.0, -38.00, -10.14, $ 24-MAY-1997 50593.0, -101.90, 494.10, 30.413340, 30.0, -38.01, -10.17, $ 25-MAY-1997 50594.0, -99.70, 496.30, 30.415350, 30.0, -38.22, -10.01, $ 26-MAY-1997 50595.0, -97.30, 498.40, 30.417430, 30.0, -38.47, -9.78, $ 27-MAY-1997 50596.0, -94.80, 500.50, 30.419660, 30.0, -38.53, -9.60, $ 28-MAY-1997 50597.0, -92.50, 502.60, 30.422030, 30.0, -38.33, -9.49, $ 29-MAY-1997 50598.0, -90.20, 504.60, 30.424520, 30.0, -37.98, -9.38, $ 30-MAY-1997 50599.0, -88.00, 506.60, 30.427050, 30.0, -37.74, -9.21, $ 31-MAY-1997 50600.0, -85.60, 508.50, 30.429550, 30.0, -37.86, -9.06, $ 1-JUN-1997 50601.0, -83.10, 510.40, 30.431990, 30.0, -38.41, -9.06, $ 2-JUN-1997 50602.0, -80.60, 512.20, 30.434260, 30.0, -39.14, -9.21, $ 3-JUN-1997 50603.0, -78.20, 513.80, 30.436320, 30.0, -39.67, -9.41, $ 4-JUN-1997 50604.0, -75.80, 515.20, 30.438180, 30.0, -39.77, -9.52, $ 5-JUN-1997 50605.0, -73.50, 516.40, 30.439850, 30.0, -39.54, -9.54, $ 6-JUN-1997 50606.0, -71.10, 517.40, 30.441400, 30.0, -39.26, -9.52, $ 7-JUN-1997 50607.0, -68.70, 518.10, 30.442880, 30.0, -39.12, -9.57, $ 8-JUN-1997 50608.0, -65.80, 518.70, 30.444340, 30.0, -39.12, -9.67, $ 9-JUN-1997 50609.0, -62.50, 519.30, 30.445820, 30.0, -39.20, -9.77, $ 10-JUN-1997 50610.0, -58.80, 520.00, 30.447340, 30.0, -39.32, -9.79, $ 11-JUN-1997 50611.0, -55.00, 521.20, 30.448900, 30.0, -39.44, -9.75, $ 12-JUN-1997 50612.0, -51.40, 522.70, 30.450510, 30.0, -39.53, -9.68, $ 13-JUN-1997 50613.0, -47.70, 524.30, 30.452110, 30.0, -39.69, -9.64, $ 14-JUN-1997 50614.0, -44.20, 525.80, 30.453700, 30.0, -40.02, -9.60, $ 15-JUN-1997 50615.0, -40.50, 526.90, 30.455250, 30.0, -40.54, -9.50, $ 16-JUN-1997 50616.0, -36.80, 527.80, 30.456700, 30.0, -41.08, -9.32, $ 17-JUN-1997 50617.0, -33.10, 528.50, 30.458030, 30.0, -41.42, -9.13, $ 18-JUN-1997 50618.0, -29.40, 529.20, 30.459210, 30.0, -41.47, -9.07, $ 19-JUN-1997 50619.0, -25.70, 529.90, 30.460290, 30.0, -41.34, -9.19, $ 20-JUN-1997 50620.0, -21.80, 530.60, 30.461290, 30.0, -41.20, -9.40, $ 21-JUN-1997 50621.0, -17.80, 531.20, 30.462270, 30.0, -41.20, -9.46, $ 22-JUN-1997 50622.0, -13.70, 531.70, 30.463310, 30.0, -41.40, -9.24, $ 23-JUN-1997 50623.0, -9.70, 532.20, 30.464450, 30.0, -41.73, -8.88, $ 24-JUN-1997 50624.0, -5.70, 532.60, 30.465700, 30.0, -42.06, -8.64, $ 25-JUN-1997 50625.0, -1.80, 532.90, 30.467040, 30.0, -42.23, -8.62, $ 26-JUN-1997 50626.0, 2.10, 533.30, 30.468400, 30.0, -42.19, -8.71, $ 27-JUN-1997 50627.0, 6.10, 533.60, 30.469740, 30.0, -42.04, -8.81, $ 28-JUN-1997 50628.0, 10.20, 534.00, 30.470980, 30.0, -42.02, -8.86, $ 29-JUN-1997 50629.0, 14.50, 534.50, 30.472090, 30.0, -42.35, -8.91, $ 30-JUN-1997 50630.0, 18.70, 535.10, 30.473030, 31.0, -42.98, -8.98, $ 1-JUL-1997 50631.0, 22.80, 535.60, 30.473820, 31.0, -43.59, -9.09, $ 2-JUL-1997 50632.0, 26.80, 535.80, 30.474460, 31.0, -43.86, -9.20, $ 3-JUL-1997 50633.0, 30.50, 535.70, 30.475000, 31.0, -43.73, -9.27, $ 4-JUL-1997 50634.0, 34.30, 535.40, 30.475510, 31.0, -43.46, -9.28, $ 5-JUL-1997 50635.0, 38.10, 534.90, 30.476070, 31.0, -43.24, -9.24, $ 6-JUL-1997 50636.0, 42.10, 534.30, 30.476720, 31.0, -43.14, -9.17, $ 7-JUL-1997 50637.0, 46.20, 533.70, 30.477450, 31.0, -43.20, -9.11, $ 8-JUL-1997 50638.0, 50.30, 533.20, 30.478280, 31.0, -43.42, -9.06, $ 9-JUL-1997 50639.0, 54.30, 532.80, 30.479180, 31.0, -43.71, -9.07, $ 10-JUL-1997 50640.0, 58.00, 532.40, 30.480140, 31.0, -43.87, -9.12, $ 11-JUL-1997 50641.0, 61.60, 531.80, 30.481180, 31.0, -43.93, -9.19, $ 12-JUL-1997 50642.0, 65.00, 531.20, 30.482260, 31.0, -44.17, -9.23, $ 13-JUL-1997 50643.0, 68.50, 530.50, 30.483370, 31.0, -44.78, -9.21, $ 14-JUL-1997 50644.0, 72.00, 529.70, 30.484500, 31.0, -45.55, -9.10, $ 15-JUL-1997 50645.0, 75.20, 528.90, 30.485570, 31.0, -46.00, -8.89, $ 16-JUL-1997 50646.0, 78.10, 528.00, 30.486590, 31.0, -46.00, -8.68, $ 17-JUL-1997 50647.0, 81.00, 527.20, 30.487650, 31.0, -45.78, -8.63, $ 18-JUL-1997 50648.0, 84.00, 526.30, 30.488820, 31.0, -45.63, -8.79, $ 19-JUL-1997 50649.0, 87.30, 525.30, 30.490120, 31.0, -45.65, -8.93, $ 20-JUL-1997 50650.0, 91.00, 524.30, 30.491630, 31.0, -45.76, -8.83, $ 21-JUL-1997 50651.0, 94.80, 523.30, 30.493320, 31.0, -45.95, -8.53, $ 22-JUL-1997 50652.0, 98.50, 522.30, 30.495170, 31.0, -46.24, -8.31, $ 23-JUL-1997 50653.0, 101.80, 521.30, 30.497140, 31.0, -46.59, -8.31, $ 24-JUL-1997 50654.0, 104.80, 520.30, 30.499160, 31.0, -46.90, -8.46, $ 25-JUL-1997 50655.0, 107.50, 519.40, 30.501140, 31.0, -47.06, -8.61, $ 26-JUL-1997 50656.0, 109.90, 518.40, 30.502980, 31.0, -47.07, -8.75, $ 27-JUL-1997 50657.0, 112.20, 517.30, 30.504680, 31.0, -47.09, -8.90, $ 28-JUL-1997 50658.0, 114.50, 516.00, 30.506220, 31.0, -47.27, -9.04, $ 29-JUL-1997 50659.0, 117.00, 514.60, 30.507620, 31.0, -47.59, -9.12, $ 30-JUL-1997 50660.0, 119.70, 513.30, 30.508890, 31.0, -47.86, -9.19, $ 31-JUL-1997 50661.0, 122.70, 512.00, 30.510120, 31.0, -47.88, -9.26, $ 1-AUG-1997 50662.0, 125.80, 510.60, 30.511370, 31.0, -47.66, -9.27, $ 2-AUG-1997 50663.0, 128.90, 509.30, 30.512630, 31.0, -47.36, -9.15, $ 3-AUG-1997 50664.0, 131.90, 508.10, 30.513900, 31.0, -47.14, -8.91, $ 4-AUG-1997 50665.0, 134.70, 506.80, 30.515240, 31.0, -47.11, -8.65, $ 5-AUG-1997 50666.0, 137.20, 505.50, 30.516630, 31.0, -47.34, -8.51, $ 6-AUG-1997 50667.0, 139.60, 504.00, 30.518050, 31.0, -47.67, -8.57, $ 7-AUG-1997 50668.0, 141.80, 502.40, 30.519500, 31.0, -47.82, -8.76, $ 8-AUG-1997 50669.0, 144.10, 500.70, 30.520960, 31.0, -47.74, -8.94, $ 9-AUG-1997 50670.0, 146.40, 498.90, 30.522440, 31.0, -47.76, -9.05, $ 10-AUG-1997 50671.0, 148.60, 497.00, 30.523860, 31.0, -48.22, -9.10, $ 11-AUG-1997 50672.0, 150.70, 495.00, 30.525160, 31.0, -48.96, -9.10, $ 12-AUG-1997 50673.0, 152.70, 493.00, 30.526410, 31.0, -49.43, -8.99, $ 13-AUG-1997 50674.0, 154.80, 490.80, 30.527600, 31.0, -49.35, -8.77, $ 14-AUG-1997 50675.0, 156.80, 488.70, 30.528740, 31.0, -49.00, -8.61, $ 15-AUG-1997 50676.0, 158.80, 486.60, 30.529940, 31.0, -48.82, -8.64, $ 16-AUG-1997 50677.0, 160.60, 484.70, 30.531290, 31.0, -48.89, -8.78, $ 17-AUG-1997 50678.0, 162.50, 482.70, 30.532790, 31.0, -49.05, -8.79, $ 18-AUG-1997 50679.0, 164.50, 480.50, 30.534440, 31.0, -49.16, -8.64, $ 19-AUG-1997 50680.0, 166.50, 478.20, 30.536220, 31.0, -49.26, -8.51, $ 20-AUG-1997 50681.0, 168.70, 475.80, 30.538120, 31.0, -49.46, -8.49, $ 21-AUG-1997 50682.0, 171.00, 473.50, 30.540000, 31.0, -49.81, -8.47, $ 22-AUG-1997 50683.0, 173.40, 471.40, 30.541780, 31.0, -50.22, -8.38, $ 23-AUG-1997 50684.0, 175.80, 469.30, 30.543420, 31.0, -50.48, -8.35, $ 24-AUG-1997 50685.0, 178.30, 467.20, 30.544880, 31.0, -50.43, -8.51, $ 25-AUG-1997 50686.0, 180.70, 465.30, 30.546230, 31.0, -50.20, -8.81, $ 26-AUG-1997 50687.0, 183.10, 463.50, 30.547520, 31.0, -50.05, -9.06, $ 27-AUG-1997 50688.0, 185.40, 461.70, 30.548830, 31.0, -50.10, -9.16, $ 28-AUG-1997 50689.0, 187.80, 459.80, 30.550150, 31.0, -50.15, -9.17, $ 29-AUG-1997 50690.0, 190.10, 458.10, 30.551470, 31.0, -50.02, -9.12, $ 30-AUG-1997 50691.0, 192.40, 456.30, 30.552850, 31.0, -49.75, -8.94, $ 31-AUG-1997 50692.0, 194.80, 454.70, 30.554270, 31.0, -49.49, -8.62, $ 1-SEP-1997 50693.0, 197.10, 453.10, 30.555770, 31.0, -49.42, -8.27, $ 2-SEP-1997 50694.0, 199.50, 451.40, 30.557360, 31.0, -49.55, -8.07, $ 3-SEP-1997 50695.0, 201.80, 449.50, 30.558990, 31.0, -49.76, -8.13, $ 4-SEP-1997 50696.0, 203.90, 447.40, 30.560600, 31.0, -49.83, -8.37, $ 5-SEP-1997 50697.0, 205.70, 445.00, 30.562170, 31.0, -49.68, -8.61, $ 6-SEP-1997 50698.0, 207.40, 442.40, 30.563730, 31.0, -49.54, -8.73, $ 7-SEP-1997 50699.0, 209.00, 439.70, 30.565240, 31.0, -49.69, -8.78, $ 8-SEP-1997 50700.0, 210.50, 437.00, 30.566680, 31.0, -50.14, -8.83, $ 9-SEP-1997 50701.0, 212.00, 434.40, 30.568040, 31.0, -50.45, -8.84, $ 10-SEP-1997 50702.0, 213.40, 431.80, 30.569410, 31.0, -50.35, -8.73, $ 11-SEP-1997 50703.0, 214.80, 429.40, 30.570870, 31.0, -49.98, -8.56, $ 12-SEP-1997 50704.0, 215.90, 427.20, 30.572440, 31.0, -49.73, -8.47, $ 13-SEP-1997 50705.0, 216.70, 425.10, 30.574170, 31.0, -49.77, -8.47, $ 14-SEP-1997 50706.0, 217.10, 423.00, 30.576120, 31.0, -49.96, -8.43, $ 15-SEP-1997 50707.0, 217.30, 420.70, 30.578290, 31.0, -50.08, -8.32, $ 16-SEP-1997 50708.0, 217.50, 418.20, 30.580660, 31.0, -50.04, -8.27, $ 17-SEP-1997 50709.0, 217.80, 415.70, 30.583080, 31.0, -49.96, -8.29, $ 18-SEP-1997 50710.0, 218.30, 413.10, 30.585480, 31.0, -50.05, -8.21, $ 19-SEP-1997 50711.0, 218.90, 410.60, 30.587770, 31.0, -50.40, -7.93, $ 20-SEP-1997 50712.0, 219.60, 408.10, 30.589900, 31.0, -50.80, -7.67, $ 21-SEP-1997 50713.0, 220.30, 405.70, 30.591840, 31.0, -50.89, -7.75, $ 22-SEP-1997 50714.0, 221.00, 403.20, 30.593700, 31.0, -50.58, -8.15, $ 23-SEP-1997 50715.0, 221.60, 400.80, 30.595490, 31.0, -50.17, -8.60, $ 24-SEP-1997 50716.0, 222.10, 398.30, 30.597260, 31.0, -49.96, -8.84, $ 25-SEP-1997 50717.0, 222.70, 395.80, 30.599050, 31.0, -49.90, -8.84, $ 26-SEP-1997 50718.0, 223.10, 393.40, 30.600880, 31.0, -49.77, -8.70, $ 27-SEP-1997 50719.0, 223.60, 390.90, 30.602760, 31.0, -49.52, -8.47, $ 28-SEP-1997 50720.0, 224.00, 388.40, 30.604710, 31.0, -49.29, -8.16, $ 29-SEP-1997 50721.0, 224.40, 385.90, 30.606720, 31.0, -49.19, -7.85, $ 30-SEP-1997 50722.0, 224.70, 383.40, 30.608790, 31.0, -49.18, -7.63, $ 1-OCT-1997 50723.0, 225.00, 380.80, 30.610880, 31.0, -49.19, -7.60, $ 2-OCT-1997 50724.0, 225.20, 378.30, 30.612970, 31.0, -49.19, -7.73, $ 3-OCT-1997 50725.0, 225.40, 375.80, 30.615040, 31.0, -49.13, -7.89, $ 4-OCT-1997 50726.0, 225.60, 373.30, 30.617070, 31.0, -49.01, -7.99, $ 5-OCT-1997 50727.0, 225.70, 370.80, 30.619050, 31.0, -48.92, -8.02, $ 6-OCT-1997 50728.0, 225.80, 368.20, 30.621000, 31.0, -48.96, -8.08, $ 7-OCT-1997 50729.0, 225.90, 365.70, 30.622930, 31.0, -49.03, -8.14, $ 8-OCT-1997 50730.0, 225.90, 363.20, 30.624880, 31.0, -48.93, -8.13, $ 9-OCT-1997 50731.0, 225.90, 360.70, 30.626910, 31.0, -48.65, -8.01, $ 10-OCT-1997 50732.0, 225.80, 358.10, 30.629080, 31.0, -48.36, -7.84, $ 11-OCT-1997 50733.0, 225.70, 355.60, 30.631420, 31.0, -48.23, -7.65, $ 12-OCT-1997 50734.0, 225.60, 353.10, 30.633950, 31.0, -48.27, -7.44, $ 13-OCT-1997 50735.0, 225.40, 350.60, 30.636640, 31.0, -48.36, -7.22, $ 14-OCT-1997 50736.0, 225.20, 348.10, 30.639430, 31.0, -48.33, -7.17, $ 15-OCT-1997 50737.0, 224.90, 345.50, 30.642220, 31.0, -48.16, -7.31, $ 16-OCT-1997 50738.0, 224.60, 343.00, 30.644920, 31.0, -48.02, -7.39, $ 17-OCT-1997 50739.0, 224.30, 340.50, 30.647460, 31.0, -48.11, -7.22, $ 18-OCT-1997 50740.0, 223.90, 338.00, 30.649820, 31.0, -48.36, -6.93, $ 19-OCT-1997 50741.0, 223.50, 335.50, 30.652030, 31.0, -48.46, -6.87, $ 20-OCT-1997 50742.0, 223.10, 333.00, 30.654120, 31.0, -48.22, -7.18, $ 21-OCT-1997 50743.0, 222.60, 330.60, 30.656160, 31.0, -47.80, -7.63, $ 22-OCT-1997 50744.0, 222.10, 328.10, 30.658200, 31.0, -47.48, -7.93, $ 23-OCT-1997 50745.0, 221.50, 325.60, 30.660260, 31.0, -47.30, -7.94, $ 24-OCT-1997 50746.0, 220.90, 323.20, 30.662380, 31.0, -47.09, -7.75, $ 25-OCT-1997 50747.0, 220.30, 320.70, 30.664550, 31.0, -46.82, -7.49, $ 26-OCT-1997 50748.0, 219.60, 318.30, 30.666790, 31.0, -46.64, -7.20, $ 27-OCT-1997 50749.0, 218.90, 315.90, 30.669070, 31.0, -46.58, -6.95, $ 28-OCT-1997 $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Quasi-Stellar Radio sources: $ $ Since NEAR uses no VLBI data types, there is no list of quasars. $ QNUMBR(1) = 25*0, QNAME(1) = 25*' ', QRA(1) = 25*0.0D0, QDEC(1) = 25*0.0D0, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ ACCUME $ $ ACCUME accumulates all the partial derivatives from REGRES to form $ an information matrix consisting of state parameters & parameters $ specified in 'YPARAM' and 'RANDOM'. $ ACUPRT(1) = .TRUE., $ ACCUME print flags. ACUPRT(2) = .TRUE., ACUPRT(3) = 8*.FALSE., YPARAM(1) = 994*' ', $ Bias parameters (' ' = all parameters on regres) $ $ Note: YPARAM allows a parameter to be both random and bias. $ $ Instead of using a priori covariances, the ACCUME information array may $ be initialized from a previous ACCUME file: $ SCOLDR = 1.0D0, $ Input ACCUME file scale factor. $ $ Stochastic & sequential estimation inputs: $ COVARY = 100*0, $ Batch numbers to be smoothed. COVOPT = 0, $ Calculate smoothed covariance at batch 1. BCHTIM(1) = ' ', $ First batch will be at PV File epoch. BCHLEN(1) = ' ', $ ' ' => run in single batch mode. OUTBCH(1) = 1, $ List of batch #'s for which an information $ array should be output to ACCUME. $ RANDOM(1) = 20*' ', $ Specify the stochastic parameters. PSIGMA(1,1) = 2000*0.0D0, $ Sigmas of the stochastics. DAPW(1) = 20*0.0D0, $ Variances of the stochastics. MTAU(1) = 20*0.0D0, $ Correlation times in days. MTAUC(1) = 20*' ', NAP(1) = 100*0, NPSIG(1) = 100*0, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ SOLVE $ $ SOLVE uses the information matrix to estimate parameters while $ considering the effects of other parameters, and generates an $ epoch state covariance. $ SVD = .FALSE., $ TRUE => SVD, Singular Value Decomposition. $ FALSE => SRIF, Square Root Information Filter. EPS2 = 1.0D-30, $ Tolerance for Singular Value Decomposition. SALENT = .TRUE., $ Write salient information file (90). SMOFIL = .FALSE., $ No SMOOTH files are written. SMOSOL = 0, $ SOLUTN(1) = 25*0, $ 0's => "SOLVE" uses the last batch from accume $ to determine a solution. BATCH = 0, $ Initialize batch, solution & iteration numbers. SOLNO = 0, ITNO = 0, $ EST( 1) = 200*' ', CON( 1) = 200*' ', $ EST( 1) = 'X','Y','Z','DX','DY','DZ', $ APVNOM( 1) = 200*.TRUE., $ The a priori values for the EST parameters $ are not from the arrays APVALS or APVALi. $ APVALS( 1) = 200*0.0D0, $ A priori values of the parameters in APNAMS. APVAL1( 1) = 50*0.0D0, $ '' APNAM1. APVAL2( 1) = 50*0.0D0, $ '' APNAM2. APVAL3( 1) = 50*0.0D0, $ '' APNAM3. APVAL4( 1) = 50*0.0D0, $ '' APNAM4. APVAL5( 1) = 50*0.0D0, $ '' APNAM5. $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ a-priori covariances: $ $ Names of the parameters for which apriori covariances exist. $ These names correspond to values in the APQ arrays. $ APNAMS( 1) = 200*' ', APNAM1( 1) = 50*' ', APNAM2( 1) = 50*' ', APNAM3( 1) = 50*' ', APNAM4( 1) = 50*' ', APNAM5( 1) = 50*' ', $ $ Initialize the apriori covariances, APQ. $ APQCOV = .TRUE., $ APQ contains apriori covariances. $ APQ(1,1) = 40000*0.0D0, APQ1(1,1) = 2500*0.0D0, APQ2(1,1) = 2500*0.0D0, APQ3(1,1) = 2500*0.0D0, APQ4(1,1) = 2500*0.0D0, APQ5(1,1) = 2500*0.0D0, $ SCAPQ(1) = 200*1.0D0, $ APQ array scale factors. SCAPQ1(1) = 50*1.0D0, SCAPQ2(1) = 50*1.0D0, SCAPQ3(1) = 50*1.0D0, SCAPQ4(1) = 50*1.0D0, SCAPQ5(1) = 50*1.0D0, $ $ Parameter names corresponding DIAGQ or APQ values: $ APNAMS( 1) = 'X','Y','Z','DX','DY','DZ', $ APNAM1( 1) = 'SPEC01','DIFF01','AREA01', 'SPEC02','DIFF02','AREA02', APNAM1( 7) = 'DIFF03','AREA03', 'DIFF04','AREA04', 'DIFF05','AREA05', APNAM1(13) = 'NUF','NUB', $ APNAM2( 1) = 'GM3','GMM','GM9','J302','J402', APNAM2( 6) = 'ATAR','ATAX','ATAY', 'BTAR','BTAX','BTAY', 'CTAR','CTAX','CTAY', APNAM2(15) = 'DRB04','STB04','F004','ALP004','DLT004', 'DRB05','STB05','F005','ALP005','DLT005', 'DRB06','STB06','F006','ALP006','DLT006', 'DRB07','STB07','F007','ALP007','DLT007', 'DRB08','STB08','F008','ALP008','DLT008', $ APNAM3( 1) = 'TROPD1','TROPW1','IONOD1','IONON1', 'TROPD4','TROPW4','IONOD4','IONON4', 'TROPD6','TROPW6','IONOD6','IONON6', APNAM3(13) = 'RC01','RC02','RC03', $ $ APNAM4 parameter names are included with station locations. $ $ APNAM5 parameter names are included with the stn-loc & ephemeris covariance. $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ a-priori sigmas squared: $ DIAGQ( 1) = $ State uncertainties: 1.0D02, 1.0D02, 1.0D02, $ position (km) 1.0D12, 1.0D12, 1.0D12, $ velocity (km/s) $ DIAGQ1( 1) = $ SRP uncertainties: 4.0000D-4, 0.0289D-4, 0.0025D0, 4.0000D-4, 0.0289D-4, 0.0025D0, DIAGQ1( 7) = 8.5849D-4, 0.0025D0, 8.5849D-4, 0.0025D0, 8.5849D-4, 0.0100D0, DIAGQ1(13) = 8.5849D-4, 8.5849D-4, $ DIAGQ2( 1) = $ Gravity uncertainties: 2.500000D-3, $ Earth GM 1.476225D-6, $ Moon GM 8.1D-07, $ EROS GM (.0009^2 = 100%) 1.000000D-16, $ Earth J2 0.181162896275495D-15, $ Mars J2 (MARS50C) DIAGQ2( 6) = $ Non-gravity uncertainties: 9.0D-24, 9.0D-24, 9.0D-24, $ constant (km/s2) 1.0D-26, 1.0D-26, 1.0D-26, $ linear (km/s3) 1.0D-28, 1.0D-28, 1.0D-28, $ quadratic (km/s4) DIAGQ2(15) = $ Maneuver uncertainties: 6.2500D0, $ start (s) 3.6000D3, $ duration (s) 3.6169D-4, $ thrust (N) 1.7424D0, $ RA degrees 1.7424D0, $ DEC degrees DIAGQ2(20) = 6.2500D0, 3.6000D3, 3.6169D-4, 1.7424D0, 1.7424D0, 6.2500D0, 3.6000D3, 3.6169D-4, 1.7424D0, 1.7424D0, 6.2500D0, 3.6000D3, 3.6169D-4, 1.7424D0, 1.7424D0, $ DIAGQ3( 1) = $ Media uncertainties: 0.0001D0, 0.0016D0, $ dry & wet troposphere 0.5625D0, 0.0225D0, $ day & night ionosphere 0.0001D0, 0.0016D0, 0.5625D0, 0.0225D0, 0.0001D0, 0.0016D0, 0.5625D0, 0.0225D0, DIAGQ3(13) = 2.25D2, 2.25D2, 2.25D2, $ SRA biases (15 meters). $ $ This file contains a covariance matrix for DSN stations $ as documented in IOM 335.1-96-024, 21 October 1996. $ The positions of the 70m, HEF, and 34m standard have been $ determined by VLBI measurements, while the other stations $ have been tied in through a combination of GPS and conventional $ surveys, as described in IOM 335.1-95-027, 16 October 1995 $ and TDA progress Report 42-128, February 1997 $ http://edms-www.jpl.nasa.gov/tda/progress_report/42-128/128F.pdf $ This covariance reflects the appropriate relative uncertainties. $ Note that DSS 34 and DSS 54 uncertaintes are large since $ the definitive surveys are yet to be completed. $ An overall orientation uncertainty of 5 nanoradian is included $ to account for imperfections in relating the DSN stations $ to the IERS Earth orientation series (UT1 and polar motion). $ $ The uncertainty in Earth orientation for real-time solutions $ is not included in this covariance. That uncertainty $ should be accounted for separately with the parameters $ 'UT1','XPOLE','YPOLE'. $ $ Modified 25 Nov 1996; DSS 34 survey added $ Modified 13 May 1997; DSS 54 survey added $ APNAM4(1) = 'CU12 ', 'LO12 ', 'CV12 ', 'CU13 ', 'LO13 ', 'CV13 ', 'CU14 ', 'LO14 ', 'CV14 ', 'CU15 ', 'LO15 ', 'CV15 ', 'CU16 ', 'LO16 ', 'CV16 ', 'CU17 ', 'LO17 ', 'CV17 ', 'CU23 ', 'LO23 ', 'CV23 ', 'CU24 ', 'LO24 ', 'CV24 ', 'CU25 ', 'LO25 ', 'CV25 ', 'CU26 ', 'LO26 ', 'CV26 ', 'CU27 ', 'LO27 ', 'CV27 ', 'CU28 ', 'LO28 ', 'CV28 ', 'CU33 ', 'LO33 ', 'CV33 ', 'CU34 ', 'LO34 ', 'CV34 ', 'CU42 ', 'LO42 ', 'CV42 ', 'CU43 ', 'LO43 ', 'CV43 ', 'CU45 ', 'LO45 ', APNAM5(1) = 'CV45 ', 'CU46 ', 'LO46 ', 'CV46 ', 'CU53 ', 'LO53 ', 'CV53 ', 'CU54 ', 'LO54 ', 'CV54 ', 'CU61 ', 'LO61 ', 'CV61 ', 'CU63 ', 'LO63 ', 'CV63 ', 'CU65 ', 'LO65 ', 'CV65 ', 'CU66 ', 'LO66 ', 'CV66 ', APQ4(1, 1) = 9.541631906369D-10, APQ4(1, 2) = 1.607196046550D-12, 1.867404590425D-13, APQ4(1, 3) = -2.189946488273D-10, 4.081260243988D-13, 1.338311904633D-09, APQ4(1, 4) = 4.337957260149D-10, 3.832707404823D-13, -4.728817061803D-10, 2.407022960939D-09, APQ4(1, 5) = 3.368946976474D-13, 1.353779460550D-13, -4.446253899846D-13, 3.772975383008D-13, 2.443222622066D-13, APQ4(1, 6) = -4.699127504347D-10, -4.121271879039D-13, 8.219851266366D-10, 2.891654266574D-10, -4.266233883491D-13, 2.260617870176D-09, APQ4(1, 7) = 4.802709086880D-10, 2.791953433266D-13, -4.468318590969D-10, 4.264699353114D-10, 3.377689709191D-13, -4.766954782324D-10, 5.230734672599D-10, APQ4(1, 8) = 2.261455924981D-13, 1.364909062508D-13, -4.566904201606D-13, 3.579649622893D-13, 1.350789988838D-13, -4.463312809064D-13, 4.093978910466D-13, 1.431741958675D-13, APQ4(1, 9) = -4.498956054304D-10, -3.934071927372D-13, 8.397856466612D-10, -4.815747749611D-10, -4.705519335829D-13, 8.137279891861D-10, -4.421678461213D-10, -3.919996527954D-13, 9.237422751864D-10, APQ4(1,10) = 4.337957265111D-10, 3.832707409231D-13, -4.728817064872D-10, 4.445068731704D-10, 3.772975387188D-13, -4.665364309743D-10, 4.264699357882D-10, 3.579649626545D-13, -4.815747752913D-10, 4.445068736902D-10, APQ4(1,11) = 3.368946979506D-13, 1.353779461768D-13, -4.446253903848D-13, 3.772975386403D-13, 1.352349885968D-13, -4.266233887331D-13, 3.377689712231D-13, 1.350789990054D-13, -4.705519340064D-13, 3.772975390584D-13, 1.352349887185D-13, APQ4(1,12) = -4.699127507824D-10, -4.121271882067D-13, 8.219851274609D-10, -4.665364310154D-10, -4.266233886772D-13, 8.231339663556D-10, -4.766954785953D-10, -4.463312812775D-13, 8.137279899919D-10, -4.665364313090D-10, -4.266233890612D-13, 8.231339671863D-10, APQ4(1,13) = 4.337957247815D-10, 3.832707393818D-13, -4.728817059330D-10, 4.445068713337D-10, 3.772975372915D-13, -4.665364304798D-10, 4.264699341510D-10, 3.579649614789D-13, -4.815747746264D-10, 4.445068718535D-10, 3.772975376310D-13, -4.665364308146D-10, 7.587567077566D-09, APQ4(1,14) = 3.368946970747D-13, 1.353779458249D-13, -4.446253892287D-13, 3.772975376594D-13, 1.352349882452D-13, -4.266233876238D-13, 3.377689703449D-13, 1.350789986542D-13, -4.705519327830D-13, 3.772975380774D-13, 1.352349883669D-13, -4.266233879520D-13, 3.772975366501D-13, 2.685638780747D-13, APQ4(1,15) = -4.699127499886D-10, -4.121271875226D-13, 8.219851248434D-10, -4.665364302868D-10, -4.266233878855D-13, 8.231339637044D-10, -4.766954777317D-10, -4.463312802912D-13, 8.137279874585D-10, -4.665364305803D-10, -4.266233882695D-13, 8.231339645350D-10, 3.831517849570D-09, -4.266233871602D-13, 4.980073648585D-09, APQ4(1,16) = 4.337957247815D-10, 3.832707393818D-13, -4.728817059330D-10, 4.445068713337D-10, 3.772975372915D-13, -4.665364304798D-10, 4.264699341510D-10, 3.579649614789D-13, -4.815747746264D-10, 4.445068718535D-10, 3.772975376310D-13, -4.665364308146D-10, 6.445068669496D-10, 3.772975366500D-13, -4.665364318051D-10, 7.587567077566D-09, APQ4(1,17) = 3.368946970747D-13, 1.353779458249D-13, -4.446253892287D-13, 3.772975376594D-13, 1.352349882452D-13, -4.266233876238D-13, 3.377689703449D-13, 1.350789986542D-13, -4.705519327830D-13, 3.772975380774D-13, 1.352349883669D-13, -4.266233879520D-13, 3.772975366501D-13, 1.594766043431D-13, -4.266233871602D-13, 3.772975366500D-13, 2.685638780747D-13, APQ4(1,18) = -4.699127499886D-10, -4.121271875226D-13, 8.219851248434D-10, -4.665364302868D-10, -4.266233878855D-13, 8.231339637044D-10, -4.766954777317D-10, -4.463312802912D-13, 8.137279874585D-10, -4.665364305803D-10, -4.266233882695D-13, 8.231339645350D-10, -4.665364318051D-10, -4.266233871602D-13, 1.023133960011D-09, 3.831517849570D-09, -4.266233871602D-13, 4.980073648585D-09, APQ4(1,19) = 4.337957250418D-10, 3.832707396117D-13, -4.728817062167D-10, 4.445068716004D-10, 3.772975375178D-13, -4.665364307598D-10, 4.264699344069D-10, 3.579649616937D-13, -4.815747749154D-10, 4.445068721202D-10, 3.772975378574D-13, -4.665364310945D-10, 5.445068687249D-10, 3.772975368764D-13, -4.665364312254D-10, 5.445068687249D-10, 3.772975368764D-13, -4.665364312254D-10, 7.487567079668D-09, APQ4(1,20) = 3.368946972768D-13, 1.353779459061D-13, -4.446253894955D-13, 3.772975378857D-13, 1.352349883263D-13, -4.266233878798D-13, 3.377689705475D-13, 1.350789987352D-13, -4.705519330653D-13, 3.772975383038D-13, 1.352349884481D-13, -4.266233882079D-13, 3.772975368764D-13, 1.473557962573D-13, -4.266233874162D-13, 3.772975368764D-13, 1.473557962573D-13, -4.266233874162D-13, 3.772975371028D-13, 2.564430700773D-13, APQ4(1,21) = -4.699127502706D-10, -4.121271877699D-13, 8.219851253366D-10, -4.665364305667D-10, -4.266233881415D-13, 8.231339641982D-10, -4.766954780177D-10, -4.463312805590D-13, 8.137279879467D-10, -4.665364308603D-10, -4.266233885254D-13, 8.231339650289D-10, -4.665364312254D-10, -4.266233874162D-13, 9.231339614163D-10, -4.665364312254D-10, -4.266233874162D-13, 9.231339614163D-10, 3.831517849870D-09, -4.266233876722D-13, 4.880073650544D-09, APQ4(1,22) = 4.337957247815D-10, 3.832707393818D-13, -4.728817059330D-10, 4.445068713337D-10, 3.772975372915D-13, -4.665364304798D-10, 4.264699341510D-10, 3.579649614789D-13, -4.815747746264D-10, 4.445068718535D-10, 3.772975376310D-13, -4.665364308146D-10, 6.445068669496D-10, 3.772975366501D-13, -4.665364318051D-10, 6.445068669496D-10, 3.772975366501D-13, -4.665364318051D-10, 5.445068687249D-10, 3.772975368764D-13, -4.665364312254D-10, 7.587567077566D-09, APQ4(1,23) = 3.368946970747D-13, 1.353779458249D-13, -4.446253892287D-13, 3.772975376594D-13, 1.352349882452D-13, -4.266233876238D-13, 3.377689703449D-13, 1.350789986542D-13, -4.705519327830D-13, 3.772975380774D-13, 1.352349883669D-13, -4.266233879520D-13, 3.772975366501D-13, 1.594766043431D-13, -4.266233871602D-13, 3.772975366501D-13, 1.594766043431D-13, -4.266233871602D-13, 3.772975368764D-13, 1.473557962573D-13, -4.266233874162D-13, 3.772975366501D-13, 2.685638780747D-13, APQ4(1,24) = -4.699127499886D-10, -4.121271875226D-13, 8.219851248434D-10, -4.665364302868D-10, -4.266233878855D-13, 8.231339637044D-10, -4.766954777317D-10, -4.463312802912D-13, 8.137279874585D-10, -4.665364305803D-10, -4.266233882695D-13, 8.231339645350D-10, -4.665364318051D-10, -4.266233871602D-13, 1.023133960011D-09, -4.665364318051D-10, -4.266233871602D-13, 1.023133960011D-09, -4.665364312254D-10, -4.266233874162D-13, 9.231339614163D-10, 3.831517849570D-09, -4.266233871602D-13, 4.980073648585D-09, APQ4(1,25) = 4.337957247815D-10, 3.832707393818D-13, -4.728817059330D-10, 4.445068713337D-10, 3.772975372915D-13, -4.665364304798D-10, 4.264699341510D-10, 3.579649614789D-13, -4.815747746264D-10, 4.445068718535D-10, 3.772975376310D-13, -4.665364308146D-10, 6.445068669496D-10, 3.772975366501D-13, -4.665364318051D-10, 6.445068669496D-10, 3.772975366501D-13, -4.665364318051D-10, 5.445068687249D-10, 3.772975368764D-13, -4.665364312254D-10, 6.445068669496D-10, 3.772975366501D-13, -4.665364318051D-10, 7.587567077566D-09, APQ4(1,26) = 3.368946970747D-13, 1.353779458249D-13, -4.446253892287D-13, 3.772975376594D-13, 1.352349882452D-13, -4.266233876238D-13, 3.377689703449D-13, 1.350789986542D-13, -4.705519327830D-13, 3.772975380774D-13, 1.352349883669D-13, -4.266233879520D-13, 3.772975366501D-13, 1.594766043431D-13, -4.266233871602D-13, 3.772975366501D-13, 1.594766043431D-13, -4.266233871602D-13, 3.772975368764D-13, 1.473557962573D-13, -4.266233874162D-13, 3.772975366501D-13, 1.594766043431D-13, -4.266233871602D-13, 3.772975366501D-13, 2.685638780747D-13, APQ4(1,27) = -4.699127499886D-10, -4.121271875226D-13, 8.219851248434D-10, -4.665364302868D-10, -4.266233878855D-13, 8.231339637044D-10, -4.766954777317D-10, -4.463312802912D-13, 8.137279874585D-10, -4.665364305803D-10, -4.266233882695D-13, 8.231339645350D-10, -4.665364318051D-10, -4.266233871602D-13, 1.023133960011D-09, -4.665364318051D-10, -4.266233871602D-13, 1.023133960011D-09, -4.665364312254D-10, -4.266233874162D-13, 9.231339614163D-10, -4.665364318051D-10, -4.266233871602D-13, 1.023133960011D-09, 3.831517849570D-09, -4.266233871602D-13, 4.980073648585D-09, APQ4(1,28) = 4.337957247815D-10, 3.832707393818D-13, -4.728817059330D-10, 4.445068713337D-10, 3.772975372915D-13, -4.665364304798D-10, 4.264699341510D-10, 3.579649614789D-13, -4.815747746264D-10, 4.445068718535D-10, 3.772975376310D-13, -4.665364308146D-10, 6.445068669496D-10, 3.772975366501D-13, -4.665364318051D-10, 6.445068669496D-10, 3.772975366501D-13, -4.665364318051D-10, 5.445068687249D-10, 3.772975368764D-13, -4.665364312254D-10, 6.445068669496D-10, 3.772975366501D-13, -4.665364318051D-10, 6.445068669496D-10, 3.772975366501D-13, -4.665364318051D-10, 7.587567077566D-09, APQ4(1,29) = 3.368946970747D-13, 1.353779458249D-13, -4.446253892287D-13, 3.772975376594D-13, 1.352349882452D-13, -4.266233876238D-13, 3.377689703449D-13, 1.350789986542D-13, -4.705519327830D-13, 3.772975380774D-13, 1.352349883669D-13, -4.266233879520D-13, 3.772975366501D-13, 1.594766043431D-13, -4.266233871602D-13, 3.772975366501D-13, 1.594766043431D-13, -4.266233871602D-13, 3.772975368764D-13, 1.473557962573D-13, -4.266233874162D-13, 3.772975366501D-13, 1.594766043431D-13, -4.266233871602D-13, 3.772975366501D-13, 1.594766043431D-13, -4.266233871602D-13, 3.772975366501D-13, 2.685638780747D-13, APQ4(1,30) = -4.699127499886D-10, -4.121271875226D-13, 8.219851248434D-10, -4.665364302868D-10, -4.266233878855D-13, 8.231339637044D-10, -4.766954777317D-10, -4.463312802912D-13, 8.137279874585D-10, -4.665364305803D-10, -4.266233882695D-13, 8.231339645350D-10, -4.665364318051D-10, -4.266233871602D-13, 1.023133960011D-09, -4.665364318051D-10, -4.266233871602D-13, 1.023133960011D-09, -4.665364312254D-10, -4.266233874162D-13, 9.231339614163D-10, -4.665364318051D-10, -4.266233871602D-13, 1.023133960011D-09, -4.665364318051D-10, -4.266233871602D-13, 1.023133960011D-09, 3.831517849570D-09, -4.266233871602D-13, 4.980073648585D-09, APQ4(1,31) = 4.337957249117D-10, 3.832707394968D-13, -4.728817060748D-10, 4.445068714671D-10, 3.772975374046D-13, -4.665364306198D-10, 4.264699342790D-10, 3.579649615863D-13, -4.815747747709D-10, 4.445068719869D-10, 3.772975377442D-13, -4.665364309545D-10, 5.445068685616D-10, 3.772975367632D-13, -4.665364310855D-10, 5.445068685616D-10, 3.772975367632D-13, -4.665364310855D-10, 5.445068688883D-10, 3.772975369896D-13, -4.665364313654D-10, 5.445068685616D-10, 3.772975367632D-13, -4.665364310855D-10, 5.445068685616D-10, 3.772975367632D-13, -4.665364310855D-10, 5.445068685616D-10, 3.772975367632D-13, -4.665364310855D-10, 7.587567077922D-09, APQ4(1,32) = 3.368946971757D-13, 1.353779458655D-13, -4.446253893621D-13, 3.772975377725D-13, 1.352349882858D-13, -4.266233877518D-13, 3.377689704462D-13, 1.350789986947D-13, -4.705519329242D-13, 3.772975381906D-13, 1.352349884075D-13, -4.266233880800D-13, 3.772975367632D-13, 1.473557962131D-13, -4.266233872882D-13, 3.772975367632D-13, 1.473557962131D-13, -4.266233872882D-13, 3.772975369896D-13, 1.473557963015D-13, -4.266233875442D-13, 3.772975367632D-13, 1.473557962131D-13, -4.266233872882D-13, 3.772975367632D-13, 1.473557962131D-13, -4.266233872882D-13, 3.772975367632D-13, 1.473557962131D-13, -4.266233872882D-13, 3.772975368764D-13, 2.685638781667D-13, APQ4(1,33) = -4.699127501296D-10, -4.121271876463D-13, 8.219851250900D-10, -4.665364304267D-10, -4.266233880135D-13, 8.231339639513D-10, -4.766954778747D-10, -4.463312804251D-13, 8.137279877026D-10, -4.665364307203D-10, -4.266233883974D-13, 8.231339647820D-10, -4.665364310855D-10, -4.266233872882D-13, 9.231339611394D-10, -4.665364310855D-10, -4.266233872882D-13, 9.231339611394D-10, -4.665364313654D-10, -4.266233875442D-13, 9.231339616932D-10, -4.665364310855D-10, -4.266233872882D-13, 9.231339611394D-10, -4.665364310855D-10, -4.266233872882D-13, 9.231339611394D-10, -4.665364310855D-10, -4.266233872882D-13, 9.231339611394D-10, 3.831517849290D-09, -4.266233874162D-13, 4.980073649169D-09, APQ4(1,34) = 4.337957249117D-10, 3.832707394968D-13, -4.728817060748D-10, 4.445068714671D-10, 3.772975374046D-13, -4.665364306198D-10, 4.264699342790D-10, 3.579649615863D-13, -4.815747747709D-10, 4.445068719869D-10, 3.772975377442D-13, -4.665364309545D-10, 5.445068685616D-10, 3.772975367632D-13, -4.665364310855D-10, 5.445068685616D-10, 3.772975367632D-13, -4.665364310855D-10, 5.445068688883D-10, 3.772975369896D-13, -4.665364313654D-10, 5.445068685616D-10, 3.772975367632D-13, -4.665364310855D-10, 5.445068685616D-10, 3.772975367632D-13, -4.665364310855D-10, 5.445068685616D-10, 3.772975367632D-13, -4.665364310855D-10, 6.445068673063D-10, 3.772975368764D-13, -4.665364320850D-10, 7.587567077922D-09, APQ4(1,35) = 3.368946971757D-13, 1.353779458655D-13, -4.446253893621D-13, 3.772975377725D-13, 1.352349882858D-13, -4.266233877518D-13, 3.377689704462D-13, 1.350789986947D-13, -4.705519329242D-13, 3.772975381906D-13, 1.352349884075D-13, -4.266233880800D-13, 3.772975367632D-13, 1.473557962131D-13, -4.266233872882D-13, 3.772975367632D-13, 1.473557962131D-13, -4.266233872882D-13, 3.772975369896D-13, 1.473557963015D-13, -4.266233875442D-13, 3.772975367632D-13, 1.473557962131D-13, -4.266233872882D-13, 3.772975367632D-13, 1.473557962131D-13, -4.266233872882D-13, 3.772975367632D-13, 1.473557962131D-13, -4.266233872882D-13, 3.772975368764D-13, 1.594766044352D-13, -4.266233874162D-13, 3.772975368764D-13, 2.685638781667D-13, APQ4(1,36) = -4.699127501296D-10, -4.121271876463D-13, 8.219851250900D-10, -4.665364304267D-10, -4.266233880135D-13, 8.231339639513D-10, -4.766954778747D-10, -4.463312804251D-13, 8.137279877026D-10, -4.665364307203D-10, -4.266233883974D-13, 8.231339647820D-10, -4.665364310855D-10, -4.266233872882D-13, 9.231339611394D-10, -4.665364310855D-10, -4.266233872882D-13, 9.231339611394D-10, -4.665364313654D-10, -4.266233875442D-13, 9.231339616932D-10, -4.665364310855D-10, -4.266233872882D-13, 9.231339611394D-10, -4.665364310855D-10, -4.266233872882D-13, 9.231339611394D-10, -4.665364310855D-10, -4.266233872882D-13, 9.231339611394D-10, -4.665364320850D-10, -4.266233874162D-13, 1.023133960595D-09, 3.831517849290D-09, -4.266233874162D-13, 4.980073649169D-09, APQ4(1,37) = -1.340671981463D-11, 3.761646769692D-12, -4.882517868276D-11, -3.052363044987D-11, 3.766526881291D-12, -5.908496903096D-11, -8.480975227135D-12, 3.787933645294D-12, -4.160345559616D-11, -3.052363055443D-11, 3.766526884681D-12, -5.908496913896D-11, -3.052363003666D-11, 3.766526874888D-12, -5.908496867353D-11, -3.052363003666D-11, 3.766526874888D-12, -5.908496867353D-11, -3.052363005497D-11, 3.766526877148D-12, -5.908496870898D-11, -3.052363003666D-11, 3.766526874888D-12, -5.908496867353D-11, -3.052363003666D-11, 3.766526874888D-12, -5.908496867353D-11, -3.052363003666D-11, 3.766526874888D-12, -5.908496867353D-11, -3.052363004582D-11, 3.766526876018D-12, -5.908496869125D-11, -3.052363004582D-11, 3.766526876018D-12, -5.908496869125D-11, 7.691288862063D-09, APQ4(1,38) = -3.985290805550D-12, 8.234059229314D-14, 5.410040483586D-12, -4.124940430015D-12, 8.233321636333D-14, 5.322610720858D-12, -3.919288524333D-12, 8.262683542309D-14, 5.498362722389D-12, -4.124940434088D-12, 8.233321643743D-14, 5.322610725392D-12, -4.124940421313D-12, 8.233321622337D-14, 5.322610713011D-12, -4.124940421313D-12, 8.233321622337D-14, 5.322610713011D-12, -4.124940423788D-12, 8.233321627277D-14, 5.322610716205D-12, -4.124940421313D-12, 8.233321622337D-14, 5.322610713011D-12, -4.124940421313D-12, 8.233321622337D-14, 5.322610713011D-12, -4.124940421313D-12, 8.233321622337D-14, 5.322610713011D-12, -4.124940422550D-12, 8.233321624807D-14, 5.322610714608D-12, -4.124940422550D-12, 8.233321624807D-14, 5.322610714608D-12, 1.142494346900D-12, 2.635116861455D-13, APQ4(1,39) = 6.719354433292D-11, 5.382005930526D-12, -6.510666582219D-11, 7.577209575936D-11, 5.406907717006D-12, -5.831055444075D-11, 6.583766077994D-11, 5.402167329998D-12, -6.565227020088D-11, 7.577209586399D-11, 5.406907721872D-12, -5.831055446731D-11, 7.577209545971D-11, 5.406907707814D-12, -5.831055446312D-11, 7.577209545971D-11, 5.406907707814D-12, -5.831055446312D-11, 7.577209550518D-11, 5.406907711059D-12, -5.831055449811D-11, 7.577209545971D-11, 5.406907707814D-12, -5.831055446312D-11, 7.577209545971D-11, 5.406907707814D-12, -5.831055446312D-11, 7.577209545971D-11, 5.406907707814D-12, -5.831055446312D-11, 7.577209548245D-11, 5.406907709437D-12, -5.831055448061D-11, 7.577209548245D-11, 5.406907709437D-12, -5.831055448061D-11, -3.896216864708D-09, -7.367662529443D-13, 4.886232456000D-09, APQ4(1,40) = -1.340671981329D-11, 3.761646769316D-12, -4.882517867788D-11, -3.052363044682D-11, 3.766526880914D-12, -5.908496902505D-11, -8.480975226287D-12, 3.787933644915D-12, -4.160345559200D-11, -3.052363055138D-11, 3.766526884304D-12, -5.908496913305D-11, -3.052363003361D-11, 3.766526874511D-12, -5.908496866762D-11, -3.052363003361D-11, 3.766526874511D-12, -5.908496866762D-11, -3.052363005192D-11, 3.766526876771D-12, -5.908496870307D-11, -3.052363003361D-11, 3.766526874511D-12, -5.908496866762D-11, -3.052363003361D-11, 3.766526874511D-12, -5.908496866762D-11, -3.052363003361D-11, 3.766526874511D-12, -5.908496866762D-11, -3.052363004276D-11, 3.766526875641D-12, -5.908496868534D-11, -3.052363004276D-11, 3.766526875641D-12, -5.908496868534D-11, 7.691288861294D-09, 1.142494346785D-12, -3.896216864318D-09, 7.791288860515D-09, APQ4(1,41) = -3.985290805151D-12, 8.234059228490D-14, 5.410040483045D-12, -4.124940429603D-12, 8.233321635510D-14, 5.322610720325D-12, -3.919288523941D-12, 8.262683541483D-14, 5.498362721839D-12, -4.124940433676D-12, 8.233321642920D-14, 5.322610724859D-12, -4.124940420900D-12, 8.233321621513D-14, 5.322610712479D-12, -4.124940420900D-12, 8.233321621513D-14, 5.322610712479D-12, -4.124940423375D-12, 8.233321626453D-14, 5.322610715672D-12, -4.124940420900D-12, 8.233321621513D-14, 5.322610712479D-12, -4.124940420900D-12, 8.233321621513D-14, 5.322610712479D-12, -4.124940420900D-12, 8.233321621513D-14, 5.322610712479D-12, -4.124940422138D-12, 8.233321623983D-14, 5.322610714076D-12, -4.124940422138D-12, 8.233321623983D-14, 5.322610714076D-12, 1.142494346785D-12, 2.635116861191D-13, -7.367662528706D-13, 1.142494346671D-12, 2.756266348265D-13, APQ4(1,42) = 6.719354432620D-11, 5.382005929988D-12, -6.510666581568D-11, 7.577209575178D-11, 5.406907716466D-12, -5.831055443492D-11, 6.583766077336D-11, 5.402167329457D-12, -6.565227019431D-11, 7.577209585642D-11, 5.406907721332D-12, -5.831055446147D-11, 7.577209545214D-11, 5.406907707274D-12, -5.831055445729D-11, 7.577209545214D-11, 5.406907707274D-12, -5.831055445729D-11, 7.577209549760D-11, 5.406907710518D-12, -5.831055449227D-11, 7.577209545214D-11, 5.406907707274D-12, -5.831055445729D-11, 7.577209545214D-11, 5.406907707274D-12, -5.831055445729D-11, 7.577209545214D-11, 5.406907707274D-12, -5.831055445729D-11, 7.577209547487D-11, 5.406907708896D-12, -5.831055447478D-11, 7.577209547487D-11, 5.406907708896D-12, -5.831055447478D-11, -3.896216864318D-09, -7.367662528706D-13, 4.886232455512D-09, -3.896216863929D-09, -7.367662527969D-13, 4.986232455013D-09, APQ4(1,43) = -3.012454970427D-11, 3.710969041047D-12, -6.910217233911D-11, -1.794575413620D-11, 3.739261929652D-12, -5.934492707307D-11, -5.305860164996D-11, 3.471874868450D-12, -1.082190750340D-10, -1.794575421626D-11, 3.739261933018D-12, -5.934492717194D-11, -1.794575380609D-11, 3.739261923296D-12, -5.934492675910D-11, -1.794575380609D-11, 3.739261923296D-12, -5.934492675910D-11, -1.794575381685D-11, 3.739261925539D-12, -5.934492679470D-11, -1.794575380609D-11, 3.739261923296D-12, -5.934492675910D-11, -1.794575380609D-11, 3.739261923296D-12, -5.934492675910D-11, -1.794575380609D-11, 3.739261923296D-12, -5.934492675910D-11, -1.794575381147D-11, 3.739261924417D-12, -5.934492677690D-11, -1.794575381147D-11, 3.739261924417D-12, -5.934492677690D-11, 6.082184235915D-10, 9.495461049568D-13, 4.221419574641D-10, 6.082184235307D-10, 9.495461048618D-13, 4.221419574219D-10, 1.683101270714D-09, APQ4(1,44) = -3.935526479174D-12, 8.240727569862D-14, 5.440125804280D-12, -4.093707380083D-12, 8.243995933972D-14, 5.343155961293D-12, -3.826540661348D-12, 8.297955785910D-14, 5.584013352759D-12, -4.093707384079D-12, 8.243995941391D-14, 5.343155965880D-12, -4.093707371662D-12, 8.243995919957D-14, 5.343155953249D-12, -4.093707371662D-12, 8.243995919957D-14, 5.343155953249D-12, -4.093707374118D-12, 8.243995924903D-14, 5.343155956455D-12, -4.093707371662D-12, 8.243995919957D-14, 5.343155953249D-12, -4.093707371662D-12, 8.243995919957D-14, 5.343155953249D-12, -4.093707371662D-12, 8.243995919957D-14, 5.343155953249D-12, -4.093707372890D-12, 8.243995922430D-14, 5.343155954852D-12, -4.093707372890D-12, 8.243995922430D-14, 5.343155954852D-12, 1.102384028620D-12, 1.419660420047D-13, -7.197107468543D-13, 1.102384028510D-12, 1.419660419905D-13, -7.197107467823D-13, 1.377025947996D-12, 1.839926793822D-13, APQ4(1,45) = 8.101554365544D-11, 5.420167648836D-12, -4.936299124974D-11, 6.771078555578D-11, 5.430298311598D-12, -5.736095031448D-11, 1.016164581363D-10, 5.644800039365D-12, -1.402753780909D-11, 6.771078564531D-11, 5.430298316485D-12, -5.736095034577D-11, 6.771078530662D-11, 5.430298302366D-12, -5.736095031230D-11, 6.771078530662D-11, 5.430298302366D-12, -5.736095031230D-11, 6.771078534725D-11, 5.430298305625D-12, -5.736095034672D-11, 6.771078530662D-11, 5.430298302366D-12, -5.736095031230D-11, 6.771078530662D-11, 5.430298302366D-12, -5.736095031230D-11, 6.771078530662D-11, 5.430298302366D-12, -5.736095031230D-11, 6.771078532694D-11, 5.430298303996D-12, -5.736095032951D-11, 6.771078532694D-11, 5.430298303996D-12, -5.736095032951D-11, 4.257284913693D-10, -6.105684831122D-13, 8.177598539547D-10, 4.257284913268D-10, -6.105684830511D-13, 8.177598538729D-10, -5.684026217033D-11, -9.642423338831D-13, 1.492556304339D-09, APQ4(1,46) = -3.473746585959D-11, 3.672624892062D-12, -7.417037550867D-11, -1.893897718030D-11, 3.735506688658D-12, -6.014895779732D-11, -5.201987060120D-11, 3.481260208379D-12, -1.063867856004D-10, -1.893897726292D-11, 3.735506692020D-12, -6.014895789810D-11, -1.893897684070D-11, 3.735506682308D-12, -6.014895747644D-11, -1.893897684070D-11, 3.735506682308D-12, -6.014895747644D-11, -1.893897685207D-11, 3.735506684549D-12, -6.014895751253D-11, -1.893897684070D-11, 3.735506682308D-12, -6.014895747644D-11, -1.893897684070D-11, 3.735506682308D-12, -6.014895747644D-11, -1.893897684070D-11, 3.735506682308D-12, -6.014895747644D-11, -1.893897684639D-11, 3.735506683428D-12, -6.014895749449D-11, -1.893897684639D-11, 3.735506683428D-12, -6.014895749449D-11, 6.086382920314D-10, 9.587071442687D-13, 4.221576955884D-10, 6.086382919706D-10, 9.587071441728D-13, 4.221576955462D-10, 8.397591980831D-10, 1.233244199350D-12, 3.483926443135D-10, 8.443443640505D-10, APQ4(1,47) = -3.924289073003D-12, 8.248391629831D-14, 5.452704803589D-12, -4.094879675261D-12, 8.243879205174D-14, 5.343423467963D-12, -3.831433205322D-12, 8.295628848891D-14, 5.579742831378D-12, -4.094879679259D-12, 8.243879212593D-14, 5.343423472550D-12, -4.094879666833D-12, 8.243879191159D-14, 5.343423459922D-12, -4.094879666833D-12, 8.243879191159D-14, 5.343423459922D-12, -4.094879669290D-12, 8.243879196106D-14, 5.343423463128D-12, -4.094879666833D-12, 8.243879191159D-14, 5.343423459922D-12, -4.094879666833D-12, 8.243879191159D-14, 5.343423459922D-12, -4.094879666833D-12, 8.243879191159D-14, 5.343423459922D-12, -4.094879668062D-12, 8.243879193632D-14, 5.343423461525D-12, -4.094879668062D-12, 8.243879193632D-14, 5.343423461525D-12, 1.106369076233D-12, 1.419877620300D-13, -7.220018507293D-13, 1.106369076122D-12, 1.419877620158D-13, -7.220018506571D-13, 1.225141788786D-12, 1.533247481263D-13, -8.375561529511D-13, 1.230677604831D-12, 1.533562393641D-13, APQ4(1,48) = 8.486472579732D-11, 5.451577459099D-12, -4.514118385096D-11, 6.841370532358D-11, 5.433127519585D-12, -5.676158453723D-11, 1.006713386265D-10, 5.637042733084D-12, -1.555587067010D-11, 6.841370541495D-11, 5.433127524474D-12, -5.676158456712D-11, 6.841370506761D-11, 5.433127510348D-12, -5.676158454007D-11, 6.841370506761D-11, 5.433127510348D-12, -5.676158454007D-11, 6.841370510866D-11, 5.433127513608D-12, -5.676158457413D-11, 6.841370506761D-11, 5.433127510348D-12, -5.676158454007D-11, 6.841370506761D-11, 5.433127510348D-12, -5.676158454007D-11, 6.841370506761D-11, 5.433127510348D-12, -5.676158454007D-11, 6.841370508813D-11, 5.433127511978D-12, -5.676158455710D-11, 6.841370508813D-11, 5.433127511978D-12, -5.676158455710D-11, 4.255631543803D-10, -6.166065997965D-13, 8.176677328525D-10, 4.255631543377D-10, -6.166065997348D-13, 8.176677327707D-10, 3.480349491016D-10, -8.433714784460D-13, 9.580110768376D-10, 3.448881851102D-10, -8.405399502554D-13, 9.604595838362D-10, APQ4(1,49) = -1.340672058235D-11, 3.761646776831D-12, -4.882517881624D-11, -3.052363153426D-11, 3.766526888284D-12, -5.908496936846D-11, -8.480975913294D-12, 3.787933652632D-12, -4.160345562245D-11, -3.052363163881D-11, 3.766526891674D-12, -5.908496947646D-11, -3.052363112105D-11, 3.766526881881D-12, -5.908496901102D-11, -3.052363112105D-11, 3.766526881881D-12, -5.908496901102D-11, -3.052363113936D-11, 3.766526884141D-12, -5.908496904648D-11, -3.052363112105D-11, 3.766526881881D-12, -5.908496901102D-11, -3.052363112105D-11, 3.766526881881D-12, -5.908496901102D-11, -3.052363112105D-11, 3.766526881881D-12, -5.908496901102D-11, -3.052363113020D-11, 3.766526883011D-12, -5.908496902875D-11, -3.052363113020D-11, 3.766526883011D-12, -5.908496902875D-11, 6.447192189297D-10, 1.142494369447D-12, 4.006166258969D-10, 6.447192188652D-10, 1.142494369332D-12, 4.006166258568D-10, 6.082184285963D-10, 1.102384050451D-12, 4.257284903842D-10, 6.086382970420D-10, 1.106369098140D-12, 4.255631533936D-10, 6.447192246375D-10, APQ4(1,50) = -3.985290813919D-12, 8.234059246605D-14, 5.410040494947D-12, -4.124940438678D-12, 8.233321653623D-14, 5.322610732035D-12, -3.919288532563D-12, 8.262683559661D-14, 5.498362733936D-12, -4.124940442750D-12, 8.233321661033D-14, 5.322610736569D-12, -4.124940429975D-12, 8.233321639627D-14, 5.322610724189D-12, -4.124940429975D-12, 8.233321639627D-14, 5.322610724189D-12, -4.124940432450D-12, 8.233321644567D-14, 5.322610727382D-12, -4.124940429975D-12, 8.233321639627D-14, 5.322610724189D-12, -4.124940429975D-12, 8.233321639627D-14, 5.322610724189D-12, -4.124940429975D-12, 8.233321639627D-14, 5.322610724189D-12, -4.124940431213D-12, 8.233321642097D-14, 5.322610725785D-12, -4.124940431213D-12, 8.233321642097D-14, 5.322610725785D-12, 1.142494349299D-12, 1.423621993383D-13, -7.367662544915D-13, 1.142494349185D-12, 1.423621993241D-13, -7.367662544178D-13, 9.495461069508D-13, 1.419660423028D-13, -6.105684843944D-13, 9.587071462820D-13, 1.419877623282D-13, -6.166066010914D-13, 1.142494371846D-12, 1.423621996373D-13, APQ5(1,1) = 6.719354499958D-11, 5.382005942369D-12, -6.510666593692D-11, 7.577209664352D-11, 5.406907729012D-12, -5.831055441154D-11, 6.583766139315D-11, 5.402167341780D-12, -6.565227038215D-11, 7.577209674816D-11, 5.406907733878D-12, -5.831055443810D-11, 7.577209634387D-11, 5.406907719820D-12, -5.831055443391D-11, 7.577209634387D-11, 5.406907719820D-12, -5.831055443391D-11, 7.577209638934D-11, 5.406907723064D-12, -5.831055446890D-11, 7.577209634387D-11, 5.406907719820D-12, -5.831055443391D-11, 7.577209634387D-11, 5.406907719820D-12, -5.831055443391D-11, 7.577209634387D-11, 5.406907719820D-12, -5.831055443391D-11, 7.577209636661D-11, 5.406907721442D-12, -5.831055445140D-11, 7.577209636661D-11, 5.406907721442D-12, -5.831055445140D-11, 4.006166251150D-10, -7.367662688090D-13, 8.328023142734D-10, 4.006166250750D-10, -7.367662687354D-13, 8.328023141901D-10, 4.221419557018D-10, -7.197107622344D-13, 8.177598570074D-10, 4.221576938226D-10, -7.220018661624D-13, 8.176677359058D-10, 4.006166236442D-10, -7.367662703562D-13, 8.328023176653D-10, APQ5(1,2) = -1.340672057699D-11, 3.761646775326D-12, -4.882517879671D-11, -3.052363152205D-11, 3.766526886778D-12, -5.908496934482D-11, -8.480975909901D-12, 3.787933651117D-12, -4.160345560581D-11, -3.052363162660D-11, 3.766526890168D-12, -5.908496945282D-11, -3.052363110884D-11, 3.766526880375D-12, -5.908496898739D-11, -3.052363110884D-11, 3.766526880375D-12, -5.908496898739D-11, -3.052363112715D-11, 3.766526882635D-12, -5.908496902284D-11, -3.052363110884D-11, 3.766526880375D-12, -5.908496898739D-11, -3.052363110884D-11, 3.766526880375D-12, -5.908496898739D-11, -3.052363110884D-11, 3.766526880375D-12, -5.908496898739D-11, -3.052363111799D-11, 3.766526881505D-12, -5.908496900512D-11, -3.052363111799D-11, 3.766526881505D-12, -5.908496900512D-11, 6.447192186718D-10, 1.142494368990D-12, 4.006166257367D-10, 6.447192186073D-10, 1.142494368875D-12, 4.006166256966D-10, 6.082184283530D-10, 1.102384050011D-12, 4.257284902139D-10, 6.086382967986D-10, 1.106369097698D-12, 4.255631532234D-10, 6.447192243796D-10, 1.142494371389D-12, 4.006166234840D-10, 1.044719223962D-09, APQ5(1,3) = -3.985290812325D-12, 8.234059243312D-14, 5.410040492783D-12, -4.124940437028D-12, 8.233321650330D-14, 5.322610729906D-12, -3.919288530995D-12, 8.262683556356D-14, 5.498362731736D-12, -4.124940441101D-12, 8.233321657740D-14, 5.322610734440D-12, -4.124940428325D-12, 8.233321636333D-14, 5.322610722060D-12, -4.124940428325D-12, 8.233321636333D-14, 5.322610722060D-12, -4.124940430800D-12, 8.233321641273D-14, 5.322610725253D-12, -4.124940428325D-12, 8.233321636333D-14, 5.322610722060D-12, -4.124940428325D-12, 8.233321636333D-14, 5.322610722060D-12, -4.124940428325D-12, 8.233321636333D-14, 5.322610722060D-12, -4.124940429563D-12, 8.233321638803D-14, 5.322610723656D-12, -4.124940429563D-12, 8.233321638803D-14, 5.322610723656D-12, 1.142494348842D-12, 1.423621992814D-13, -7.367662541968D-13, 1.142494348728D-12, 1.423621992672D-13, -7.367662541231D-13, 9.495461065710D-13, 1.419660422460D-13, -6.105684841502D-13, 9.587071458985D-13, 1.419877622714D-13, -6.166066008447D-13, 1.142494371389D-12, 1.423621995804D-13, -7.367662700615D-13, 1.142494370932D-12, 1.908219944439D-13, APQ5(1,4) = 6.719354497270D-11, 5.382005940216D-12, -6.510666591088D-11, 7.577209661321D-11, 5.406907726849D-12, -5.831055438821D-11, 6.583766136681D-11, 5.402167339619D-12, -6.565227035589D-11, 7.577209671785D-11, 5.406907731715D-12, -5.831055441477D-11, 7.577209631357D-11, 5.406907717657D-12, -5.831055441058D-11, 7.577209631357D-11, 5.406907717657D-12, -5.831055441059D-11, 7.577209635903D-11, 5.406907720901D-12, -5.831055444557D-11, 7.577209631357D-11, 5.406907717657D-12, -5.831055441058D-11, 7.577209631357D-11, 5.406907717657D-12, -5.831055441058D-11, 7.577209631357D-11, 5.406907717657D-12, -5.831055441058D-11, 7.577209633630D-11, 5.406907719279D-12, -5.831055442808D-11, 7.577209633630D-11, 5.406907719279D-12, -5.831055442808D-11, 4.006166249548D-10, -7.367662685143D-13, 8.328023139403D-10, 4.006166249147D-10, -7.367662684407D-13, 8.328023138570D-10, 4.221419555329D-10, -7.197107619465D-13, 8.177598566803D-10, 4.221576936537D-10, -7.220018658736D-13, 8.176677355787D-10, 4.006166234840D-10, -7.367662700615D-13, 8.328023173322D-10, 4.006166233237D-10, -7.367662697668D-13, 1.232802316839D-09, APQ5(1,5) = -2.170107119976D-10, 3.688872881717D-12, 2.277283443896D-10, -2.340567254887D-10, 3.710207277317D-12, 2.183768578055D-10, -2.130808185811D-10, 3.743474491470D-12, 2.363305746613D-10, -2.340567257830D-10, 3.710207280657D-12, 2.183768579425D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567248391D-10, 3.710207273236D-12, 2.183768578442D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567247689D-10, 3.710207272123D-12, 2.183768577787D-10, -2.340567247689D-10, 3.710207272123D-12, 2.183768577787D-10, 4.736287283149D-10, 2.811991013403D-12, 3.839914700296D-10, 4.736287282675D-10, 2.811991013121D-12, 3.839914699912D-10, 4.474230800089D-10, 2.769747768033D-12, 4.015525082460D-10, 4.481107749350D-10, 2.773023807285D-12, 4.011588961491D-10, 4.736287317373D-10, 2.811991019308D-12, 3.839914691108D-10, 4.736287315478D-10, 2.811991018183D-12, 3.839914689572D-10, 6.895379712800D-09, APQ5(1,6) = -3.794585034802D-12, 6.882512381853D-14, 5.276076219786D-12, -3.667174466219D-12, 6.867768489099D-14, 5.345300365634D-12, -3.856943696639D-12, 6.850892079200D-14, 5.194017324709D-12, -3.667174469376D-12, 6.867768495280D-14, 5.345300370546D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174462855D-12, 6.867768481544D-14, 5.345300359277D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174461755D-12, 6.867768479484D-14, 5.345300357674D-12, -3.667174461755D-12, 6.867768479484D-14, 5.345300357674D-12, -3.065221377261D-12, 1.151666400038D-13, -2.002035548670D-12, -3.065221376954D-12, 1.151666399923D-13, -2.002035548470D-12, -2.814390094951D-12, 1.154962774091D-13, -2.172700677043D-12, -2.820470366295D-12, 1.154717356208D-13, -2.169095102862D-12, -3.065221403561D-12, 1.151666402456D-13, -2.002035538759D-12, -3.065221402335D-12, 1.151666401996D-13, -2.002035537958D-12, -1.495016379847D-12, 3.029794676981D-13, APQ5(1,7) = 1.391413955241D-10, -4.089642398621D-12, -2.765408990132D-10, 1.190651250341D-10, -4.101198638754D-12, -2.896537726278D-10, 1.471750215677D-10, -4.068124159116D-12, -2.665809586489D-10, 1.190651250488D-10, -4.101198642445D-12, -2.896537729542D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651253361D-10, -4.101198634242D-12, -2.896537720012D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651253004D-10, -4.101198633012D-12, -2.896537719143D-10, 1.190651253004D-10, -4.101198633012D-12, -2.896537719143D-10, -1.920927570609D-10, -1.145084438640D-12, -6.581631581012D-10, -1.920927570417D-10, -1.145084438526D-12, -6.581631580354D-10, -2.298317612351D-10, -1.197945486829D-12, -6.326185696352D-10, -2.290179567953D-10, -1.193864925316D-12, -6.330746429283D-10, -1.920927541312D-10, -1.145084441045D-12, -6.581631618519D-10, -1.920927540544D-10, -1.145084440587D-12, -6.581631615886D-10, 4.135042944937D-09, -1.020823102462D-12, 5.789384493763D-09, APQ5(1,8) = -2.170107119976D-10, 3.688872881717D-12, 2.277283443896D-10, -2.340567254887D-10, 3.710207277317D-12, 2.183768578055D-10, -2.130808185811D-10, 3.743474491470D-12, 2.363305746613D-10, -2.340567257830D-10, 3.710207280657D-12, 2.183768579425D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567248391D-10, 3.710207273236D-12, 2.183768578442D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567247689D-10, 3.710207272123D-12, 2.183768577787D-10, -2.340567247689D-10, 3.710207272123D-12, 2.183768577787D-10, 4.736287283149D-10, 2.811991013403D-12, 3.839914700296D-10, 4.736287282675D-10, 2.811991013121D-12, 3.839914699912D-10, 4.474230800089D-10, 2.769747768033D-12, 4.015525082460D-10, 4.481107749350D-10, 2.773023807285D-12, 4.011588961491D-10, 4.736287317373D-10, 2.811991019308D-12, 3.839914691108D-10, 4.736287315478D-10, 2.811991018183D-12, 3.839914689572D-10, 7.221852346133D-10, -1.495016379847D-12, -3.571156923444D-10, 6.895379712800D-09, APQ5(1,9) = -3.794585034802D-12, 6.882512381853D-14, 5.276076219786D-12, -3.667174466219D-12, 6.867768489099D-14, 5.345300365634D-12, -3.856943696639D-12, 6.850892079200D-14, 5.194017324709D-12, -3.667174469376D-12, 6.867768495280D-14, 5.345300370546D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174462855D-12, 6.867768481544D-14, 5.345300359277D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174461755D-12, 6.867768479484D-14, 5.345300357674D-12, -3.667174461755D-12, 6.867768479484D-14, 5.345300357674D-12, -3.065221377261D-12, 1.151666400038D-13, -2.002035548670D-12, -3.065221376954D-12, 1.151666399923D-13, -2.002035548470D-12, -2.814390094951D-12, 1.154962774091D-13, -2.172700677043D-12, -2.820470366295D-12, 1.154717356208D-13, -2.169095102862D-12, -3.065221403561D-12, 1.151666402456D-13, -2.002035538759D-12, -3.065221402335D-12, 1.151666401996D-13, -2.002035537958D-12, -1.495016379847D-12, 1.780314342502D-13, -1.020823102462D-12, -1.495016379847D-12, 3.029794676981D-13, APQ5(1,10) = 1.391413955241D-10, -4.089642398621D-12, -2.765408990132D-10, 1.190651250341D-10, -4.101198638754D-12, -2.896537726278D-10, 1.471750215677D-10, -4.068124159116D-12, -2.665809586489D-10, 1.190651250488D-10, -4.101198642445D-12, -2.896537729542D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651253361D-10, -4.101198634242D-12, -2.896537720012D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651253004D-10, -4.101198633012D-12, -2.896537719143D-10, 1.190651253004D-10, -4.101198633012D-12, -2.896537719143D-10, -1.920927570609D-10, -1.145084438640D-12, -6.581631581012D-10, -1.920927570417D-10, -1.145084438526D-12, -6.581631580354D-10, -2.298317612351D-10, -1.197945486829D-12, -6.326185696352D-10, -2.290179567953D-10, -1.193864925316D-12, -6.330746429283D-10, -1.920927541312D-10, -1.145084441045D-12, -6.581631618519D-10, -1.920927540544D-10, -1.145084440587D-12, -6.581631615886D-10, -3.571156923444D-10, -1.020823102462D-12, 1.062579072760D-09, 4.135042944937D-09, -1.020823102462D-12, 5.789384493763D-09, APQ5(1,11) = -2.426163060438D-10, 3.821146992880D-12, 2.144377865165D-10, -2.188288810352D-10, 3.754903690131D-12, 2.258623674916D-10, -2.594916533426D-10, 4.200172601219D-12, 2.159318155760D-10, -2.188288812940D-10, 3.754903693510D-12, 2.258623676509D-10, -2.188288803734D-10, 3.754903683747D-12, 2.258623673138D-10, -2.188288803734D-10, 3.754903683747D-12, 2.258623673138D-10, -2.188288805047D-10, 3.754903686000D-12, 2.258623674493D-10, -2.188288803734D-10, 3.754903683747D-12, 2.258623673138D-10, -2.188288803734D-10, 3.754903683747D-12, 2.258623673138D-10, -2.188288803734D-10, 3.754903683747D-12, 2.258623673138D-10, -2.188288804391D-10, 3.754903684874D-12, 2.258623673815D-10, -2.188288804391D-10, 3.754903684874D-12, 2.258623673815D-10, 4.418730120457D-10, 2.572171538771D-12, 3.999229101909D-10, 4.418730120015D-10, 2.572171538514D-12, 3.999229101509D-10, 4.325893394650D-10, 2.497921066058D-12, 4.040382991981D-10, 4.346978147125D-10, 2.510678531406D-12, 4.029323486789D-10, 4.418730148805D-10, 2.572171544173D-12, 3.999229096757D-10, 4.418730147037D-10, 2.572171543144D-12, 3.999229095157D-10, 5.922557729236D-10, -1.272496314176D-12, -3.946293768461D-10, 5.922557729236D-10, -1.272496314176D-12, -3.946293768461D-10, 1.162531660052D-09, APQ5(1,12) = -3.968020331888D-12, 6.886646580855D-14, 5.195269263674D-12, -3.724767900314D-12, 6.862671864055D-14, 5.326196203625D-12, -4.195170463473D-12, 6.692661183585D-14, 5.194776122727D-12, -3.724767903599D-12, 6.862671870232D-14, 5.326196208467D-12, -3.724767894298D-12, 6.862671852389D-14, 5.326196194346D-12, -3.724767894298D-12, 6.862671852389D-14, 5.326196194346D-12, -3.724767896533D-12, 6.862671856506D-14, 5.326196197542D-12, -3.724767894298D-12, 6.862671852389D-14, 5.326196194346D-12, -3.724767894298D-12, 6.862671852389D-14, 5.326196194346D-12, -3.724767894298D-12, 6.862671852389D-14, 5.326196194346D-12, -3.724767895416D-12, 6.862671854447D-14, 5.326196195944D-12, -3.724767895416D-12, 6.862671854447D-14, 5.326196195944D-12, -2.950010781944D-12, 1.159552422437D-13, -2.063645399649D-12, -2.950010781649D-12, 1.159552422321D-13, -2.063645399443D-12, -2.584351579033D-12, 1.161548564507D-13, -2.322663162506D-12, -2.597260641566D-12, 1.161248610847D-13, -2.314172925299D-12, -2.950010806080D-12, 1.159552424872D-13, -2.063645391234D-12, -2.950010804900D-12, 1.159552424408D-13, -2.063645390408D-12, -1.399241585951D-12, 1.632988546787D-13, -8.907716857863D-13, -1.399241585951D-12, 1.632988546787D-13, -8.907716857863D-13, -1.650275859035D-12, 1.868167321169D-13, APQ5(1,13) = 1.320218305686D-10, -3.993564470741D-12, -2.802932664857D-10, 1.368853813624D-10, -4.057140542127D-12, -2.812928551438D-10, 1.196322386128D-10, -3.919470553775D-12, -2.536363587233D-10, 1.368853814185D-10, -4.057140545778D-12, -2.812928554447D-10, 1.368853814444D-10, -4.057140535230D-12, -2.812928544418D-10, 1.368853814444D-10, -4.057140535230D-12, -2.812928544418D-10, 1.368853815266D-10, -4.057140537664D-12, -2.812928546106D-10, 1.368853814444D-10, -4.057140535230D-12, -2.812928544418D-10, 1.368853814444D-10, -4.057140535230D-12, -2.812928544418D-10, 1.368853814444D-10, -4.057140535230D-12, -2.812928544418D-10, 1.368853814855D-10, -4.057140536447D-12, -2.812928545262D-10, 1.368853814855D-10, -4.057140536447D-12, -2.812928545262D-10, -2.270038980416D-10, -1.408952809839D-12, -6.405589062848D-10, -2.270038980189D-10, -1.408952809698D-12, -6.405589062207D-10, -2.572965873909D-10, -1.479925158377D-12, -6.210620752480D-10, -2.549368630107D-10, -1.467597043676D-12, -6.223685708457D-10, -2.270038957587D-10, -1.408952812798D-12, -6.405589095909D-10, -2.270038956679D-10, -1.408952812234D-12, -6.405589093347D-10, -3.893176834992D-10, -7.693372246272D-13, 9.214277122851D-10, -3.893176834992D-10, -7.693372246272D-13, 9.214277122851D-10, -1.554657694947D-11, -1.144897308828D-12, 1.446594990785D-09, APQ5(1,14) = -2.543362028354D-10, 3.873081710215D-12, 2.102433120571D-10, -2.198449095981D-10, 3.755770947253D-12, 2.254166673542D-10, -2.565440930932D-10, 4.184274554984D-12, 2.166038902508D-10, -2.198449098592D-10, 3.755770950633D-12, 2.254166675121D-10, -2.198449089280D-10, 3.755770940868D-12, 2.254166671819D-10, -2.198449089280D-10, 3.755770940868D-12, 2.254166671819D-10, -2.198449090599D-10, 3.755770943122D-12, 2.254166673171D-10, -2.198449089280D-10, 3.755770940868D-12, 2.254166671819D-10, -2.198449089280D-10, 3.755770940868D-12, 2.254166671819D-10, -2.198449089280D-10, 3.755770940868D-12, 2.254166671819D-10, -2.198449089939D-10, 3.755770941995D-12, 2.254166672495D-10, -2.198449089939D-10, 3.755770941995D-12, 2.254166672495D-10, 4.421447359333D-10, 2.576983590803D-12, 3.998729404636D-10, 4.421447358891D-10, 2.576983590545D-12, 3.998729404236D-10, 4.337743948383D-10, 2.514161285596D-12, 4.037091744436D-10, 4.340446513978D-10, 2.517862113365D-12, 4.036417737134D-10, 4.421447387724D-10, 2.576983596214D-12, 3.998729399456D-10, 4.421447385955D-10, 2.576983595184D-12, 3.998729397857D-10, 5.923006563898D-10, -1.279181979305D-12, -3.942448772949D-10, 5.923006563898D-10, -1.279181979305D-12, -3.942448772949D-10, 7.001265085145D-10, -1.521751499388D-12, -3.341211718177D-10, 7.016050415884D-10, APQ5(1,15) = -3.985223189832D-12, 6.893105396125D-14, 5.188721795218D-12, -3.725228858842D-12, 6.862666780193D-14, 5.326403129167D-12, -4.189364104110D-12, 6.690403797832D-14, 5.197100545253D-12, -3.725228862128D-12, 6.862666786370D-14, 5.326403134009D-12, -3.725228852823D-12, 6.862666768527D-14, 5.326403119889D-12, -3.725228852823D-12, 6.862666768527D-14, 5.326403119889D-12, -3.725228855059D-12, 6.862666772644D-14, 5.326403123085D-12, -3.725228852823D-12, 6.862666768527D-14, 5.326403119889D-12, -3.725228852823D-12, 6.862666768527D-14, 5.326403119889D-12, -3.725228852823D-12, 6.862666768527D-14, 5.326403119889D-12, -3.725228853941D-12, 6.862666770586D-14, 5.326403121487D-12, -3.725228853941D-12, 6.862666770586D-14, 5.326403121487D-12, -2.952062041318D-12, 1.159445379440D-13, -2.062740922375D-12, -2.952062041022D-12, 1.159445379325D-13, -2.062740922169D-12, -2.592095624422D-12, 1.161275656832D-13, -2.318158774126D-12, -2.601342673846D-12, 1.161149804200D-13, -2.311760511522D-12, -2.952062065490D-12, 1.159445381875D-13, -2.062740913935D-12, -2.952062064309D-12, 1.159445381412D-13, -2.062740913110D-12, -1.401297446492D-12, 1.633067896324D-13, -8.928843688886D-13, -1.401297446492D-12, 1.633067896324D-13, -8.928843688886D-13, -1.517490368802D-12, 1.731214697779D-13, -1.049238930536D-12, -1.522218917314D-12, 1.731300275274D-13, APQ5(1,16) = 1.237082161888D-10, -3.956081833731D-12, -2.832275122864D-10, 1.360736591010D-10, -4.056592504507D-12, -2.816658174431D-10, 1.215939482225D-10, -3.930930603930D-12, -2.532536273241D-10, 1.360736591552D-10, -4.056592508158D-12, -2.816658177452D-10, 1.360736591898D-10, -4.056592497611D-12, -2.816658167367D-10, 1.360736591898D-10, -4.056592497611D-12, -2.816658167367D-10, 1.360736592714D-10, -4.056592500045D-12, -2.816658169057D-10, 1.360736591898D-10, -4.056592497611D-12, -2.816658167367D-10, 1.360736591898D-10, -4.056592497611D-12, -2.816658167367D-10, 1.360736591898D-10, -4.056592497611D-12, -2.816658167367D-10, 1.360736592306D-10, -4.056592498828D-12, -2.816658168212D-10, 1.360736592306D-10, -4.056592498828D-12, -2.816658168212D-10, -2.266442819445D-10, -1.404241991895D-12, -6.406698947801D-10, -2.266442819218D-10, -1.404241991755D-12, -6.406698947160D-10, -2.557695814030D-10, -1.464626073833D-12, -6.216666241476D-10, -2.551840639307D-10, -1.461009919682D-12, -6.219696678453D-10, -2.266442796556D-10, -1.404241994844D-12, -6.406698980903D-10, -2.266442795649D-10, -1.404241994282D-12, -6.406698978340D-10, -3.891381910091D-10, -7.753516385574D-13, 9.218945212805D-10, -3.891381910091D-10, -7.753516385574D-13, 9.218945212805D-10, -3.344487080255D-10, -1.053046635014D-12, 1.068687167784D-09, -3.329031632189D-10, -1.053687823213D-12, 1.069982475783D-09, APQ5(1,17) = -2.170107127990D-10, 3.688872887593D-12, 2.277283446443D-10, -2.340567264923D-10, 3.710207283282D-12, 2.183768579397D-10, -2.130808193206D-10, 3.743474497802D-12, 2.363305750172D-10, -2.340567267867D-10, 3.710207286621D-12, 2.183768580768D-10, -2.340567257023D-10, 3.710207276975D-12, 2.183768578474D-10, -2.340567257023D-10, 3.710207276975D-12, 2.183768578474D-10, -2.340567258427D-10, 3.710207279201D-12, 2.183768579784D-10, -2.340567257023D-10, 3.710207276975D-12, 2.183768578474D-10, -2.340567257023D-10, 3.710207276975D-12, 2.183768578474D-10, -2.340567257023D-10, 3.710207276975D-12, 2.183768578474D-10, -2.340567257725D-10, 3.710207278088D-12, 2.183768579129D-10, -2.340567257725D-10, 3.710207278088D-12, 2.183768579129D-10, 4.736287305652D-10, 2.811991026743D-12, 3.839914695971D-10, 4.736287305179D-10, 2.811991026461D-12, 3.839914695587D-10, 4.474230819174D-10, 2.769747780858D-12, 4.015525080437D-10, 4.481107768517D-10, 2.773023820150D-12, 4.011588959422D-10, 4.736287339876D-10, 2.811991032648D-12, 3.839914686783D-10, 4.736287337982D-10, 2.811991031523D-12, 3.839914685247D-10, 6.221852383735D-10, -1.495016394259D-12, -3.571156894693D-10, 6.221852383735D-10, -1.495016394259D-12, -3.571156894693D-10, 5.922557750438D-10, -1.399241599150D-12, -3.893176819191D-10, 5.923006585121D-10, -1.401297459714D-12, -3.891381894257D-10, 6.221852408590D-10, APQ5(1,18) = -3.794585039735D-12, 6.882512390800D-14, 5.276076226645D-12, -3.667174470986D-12, 6.867768498027D-14, 5.345300372583D-12, -3.856943701653D-12, 6.850892088106D-14, 5.194017331461D-12, -3.667174474144D-12, 6.867768504208D-14, 5.345300377495D-12, -3.667174465422D-12, 6.867768486351D-14, 5.345300363019D-12, -3.667174465422D-12, 6.867768486351D-14, 5.345300363019D-12, -3.667174467623D-12, 6.867768490472D-14, 5.345300366226D-12, -3.667174465422D-12, 6.867768486351D-14, 5.345300363019D-12, -3.667174465422D-12, 6.867768486351D-14, 5.345300363019D-12, -3.667174465422D-12, 6.867768486351D-14, 5.345300363019D-12, -3.667174466523D-12, 6.867768488412D-14, 5.345300364623D-12, -3.667174466523D-12, 6.867768488412D-14, 5.345300364623D-12, -3.065221381245D-12, 1.151666401535D-13, -2.002035551272D-12, -3.065221380939D-12, 1.151666401420D-13, -2.002035551072D-12, -2.814390098609D-12, 1.154962775592D-13, -2.172700679867D-12, -2.820470369962D-12, 1.154717357709D-13, -2.169095105682D-12, -3.065221407546D-12, 1.151666403953D-13, -2.002035541361D-12, -3.065221406320D-12, 1.151666403493D-13, -2.002035540561D-12, -1.495016381790D-12, 1.641483196541D-13, -1.020823103790D-12, -1.495016381790D-12, 1.641483196541D-13, -1.020823103790D-12, -1.272496315830D-12, 1.632988548910D-13, -7.693372256273D-13, -1.279181980968D-12, 1.633067898447D-13, -7.753516395653D-13, -1.495016396203D-12, 1.641483198675D-13, APQ5(1,19) = 1.391413952626D-10, -4.089642403016D-12, -2.765408994080D-10, 1.190651245931D-10, -4.101198643113D-12, -2.896537731318D-10, 1.471750213651D-10, -4.068124163156D-12, -2.665809589540D-10, 1.190651246078D-10, -4.101198646804D-12, -2.896537734582D-10, 1.190651248237D-10, -4.101198636141D-12, -2.896537723314D-10, 1.190651248237D-10, -4.101198636141D-12, -2.896537723314D-10, 1.190651248951D-10, -4.101198638601D-12, -2.896537725052D-10, 1.190651248237D-10, -4.101198636141D-12, -2.896537723314D-10, 1.190651248237D-10, -4.101198636141D-12, -2.896537723314D-10, 1.190651248237D-10, -4.101198636141D-12, -2.896537723314D-10, 1.190651248594D-10, -4.101198637371D-12, -2.896537724183D-10, 1.190651248594D-10, -4.101198637371D-12, -2.896537724183D-10, -1.920927559181D-10, -1.145084431879D-12, -6.581631597506D-10, -1.920927558989D-10, -1.145084431765D-12, -6.581631596847D-10, -2.298317604036D-10, -1.197945480528D-12, -6.326185710746D-10, -2.290179559564D-10, -1.193864918980D-12, -6.330746443718D-10, -1.920927529884D-10, -1.145084434284D-12, -6.581631635012D-10, -1.920927529116D-10, -1.145084433826D-12, -6.581631632380D-10, -3.571156904819D-10, -1.020823114412D-12, 9.625790770762D-10, -3.571156904819D-10, -1.020823114412D-12, 9.625790770762D-10, -3.946293762087D-10, -8.907716966387D-13, 9.214277152602D-10, -3.942448766554D-10, -8.928843797611D-13, 9.218945242588D-10, -3.571156885052D-10, -1.020823115739D-12, 9.625790804070D-10, APQ5(1,20) = -2.170107119976D-10, 3.688872881717D-12, 2.277283443896D-10, -2.340567254887D-10, 3.710207277317D-12, 2.183768578055D-10, -2.130808185811D-10, 3.743474491470D-12, 2.363305746613D-10, -2.340567257830D-10, 3.710207280657D-12, 2.183768579425D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567248391D-10, 3.710207273236D-12, 2.183768578442D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567246986D-10, 3.710207271010D-12, 2.183768577131D-10, -2.340567247689D-10, 3.710207272123D-12, 2.183768577787D-10, -2.340567247689D-10, 3.710207272123D-12, 2.183768577787D-10, 4.736287283149D-10, 2.811991013403D-12, 3.839914700296D-10, 4.736287282675D-10, 2.811991013121D-12, 3.839914699912D-10, 4.474230800089D-10, 2.769747768033D-12, 4.015525082460D-10, 4.481107749350D-10, 2.773023807285D-12, 4.011588961491D-10, 4.736287317373D-10, 2.811991019308D-12, 3.839914691108D-10, 4.736287315478D-10, 2.811991018183D-12, 3.839914689572D-10, 7.221852346133D-10, -1.495016379847D-12, -3.571156923444D-10, 7.221852346133D-10, -1.495016379847D-12, -3.571156923444D-10, 5.922557729236D-10, -1.399241585951D-12, -3.893176834992D-10, 5.923006563898D-10, -1.401297446492D-12, -3.891381910091D-10, 6.221852383735D-10, -1.495016381790D-12, -3.571156904819D-10, 6.895379712800D-09, APQ5(1,21) = -3.794585034802D-12, 6.882512381853D-14, 5.276076219786D-12, -3.667174466219D-12, 6.867768489099D-14, 5.345300365634D-12, -3.856943696639D-12, 6.850892079200D-14, 5.194017324709D-12, -3.667174469376D-12, 6.867768495280D-14, 5.345300370546D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174462855D-12, 6.867768481544D-14, 5.345300359277D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174460655D-12, 6.867768477423D-14, 5.345300356070D-12, -3.667174461755D-12, 6.867768479484D-14, 5.345300357674D-12, -3.667174461755D-12, 6.867768479484D-14, 5.345300357674D-12, -3.065221377261D-12, 1.151666400038D-13, -2.002035548670D-12, -3.065221376954D-12, 1.151666399923D-13, -2.002035548470D-12, -2.814390094951D-12, 1.154962774091D-13, -2.172700677043D-12, -2.820470366295D-12, 1.154717356208D-13, -2.169095102862D-12, -3.065221403561D-12, 1.151666402456D-13, -2.002035538759D-12, -3.065221402335D-12, 1.151666401996D-13, -2.002035537958D-12, -1.495016379847D-12, 1.780314342502D-13, -1.020823102462D-12, -1.495016379847D-12, 1.780314342502D-13, -1.020823102462D-12, -1.272496314176D-12, 1.632988546787D-13, -7.693372246272D-13, -1.279181979305D-12, 1.633067896324D-13, -7.753516385574D-13, -1.495016394259D-12, 1.641483196541D-13, -1.020823114412D-12, -1.495016379847D-12, 3.029794676981D-13, APQ5(1,22) = 1.391413955241D-10, -4.089642398621D-12, -2.765408990132D-10, 1.190651250341D-10, -4.101198638754D-12, -2.896537726278D-10, 1.471750215677D-10, -4.068124159116D-12, -2.665809586489D-10, 1.190651250488D-10, -4.101198642445D-12, -2.896537729542D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651253361D-10, -4.101198634242D-12, -2.896537720012D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651252647D-10, -4.101198631782D-12, -2.896537718274D-10, 1.190651253004D-10, -4.101198633012D-12, -2.896537719143D-10, 1.190651253004D-10, -4.101198633012D-12, -2.896537719143D-10, -1.920927570609D-10, -1.145084438640D-12, -6.581631581012D-10, -1.920927570417D-10, -1.145084438526D-12, -6.581631580354D-10, -2.298317612351D-10, -1.197945486829D-12, -6.326185696352D-10, -2.290179567953D-10, -1.193864925316D-12, -6.330746429283D-10, -1.920927541312D-10, -1.145084441045D-12, -6.581631618519D-10, -1.920927540544D-10, -1.145084440587D-12, -6.581631615886D-10, -3.571156923444D-10, -1.020823102462D-12, 1.062579072760D-09, -3.571156923444D-10, -1.020823102462D-12, 1.062579072760D-09, -3.946293768461D-10, -8.907716857863D-13, 9.214277122851D-10, -3.942448772949D-10, -8.928843688886D-13, 9.218945212805D-10, -3.571156894693D-10, -1.020823103790D-12, 9.625790770762D-10, 4.135042944937D-09, -1.020823102462D-12, 5.789384493763D-09, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Earth/Moon Barycenter - Mars planetary ephemeris covariance consistent $ with DE403. $ $ 1) Mail message from Myles Standish dated October 13, 1995. $ $ 2) Standish, E. M., et. al., "JPL Planetary and Lunar Ephemerides, $ DE403/LE403", JPL IOM 314.10-127, May 22, 1995. $ $ 3) Standish, E. M., "Updated Covariance of Mars for DE234", $ JPL IOM 314.6-1452, September 4, 1992. $ $ The DE403 ephemeris is now based upon the (J2000) reference frame of the $ International Earth Rotation Service (IERS). $ $ Also, the modeling of the perturbations of asteroids upon the planetary $ orbits has been improved. $ $ Heliocentric position errors on 11-SEP-1997 in VIEW1 coordinates: $ $ Mars Earth-Moon $ $ radial 0.09280 km 0.00823 km $ down track 3.50069 km 2.35441 km $ cross track 4.46716 km 2.41721 km $ $ Note: this covariance is *NOT* the formal covariance originally generated $ by Myles Standish in his ephemeris solution. It has been increased by $ multiplying the formal sigmas by a factor of 3 (9x each covariance term). $ This was done by Myles Standish himself in order to get a "realistic" $ 1-sigma covariance for the MGS NAV Team. $ $ The Eros Set III covariance is from IOM 312.F-98-019 (Feb 12, 1998) $ APNAM5(23) = 'DMWB','DPB','DQB','EDWB','DAB','DEB', 'DMW4','DP4','DQ4','EDW4','DA4','DE4', APNAM5(35) = 'DMW9','DP9','DQ9','EDW9','DA9','DE9', $ SCAPQ5(23) = 12*1.0D0, $ Scale the formal covariance by 1. SCAPQ5(35) = 6*1.0D0, $ APQ5( 23, 23) = .2500619938607D-15, APQ5( 23, 24) = -.9840809907449D-16, .3012307203757D-15, APQ5( 23, 25) = -.6717466164725D-17, .7541612869500D-16, .3776553127620D-15, APQ5( 23, 26) = .4089233839056D-17, -.1642413344515D-17, -.1079032697502D-18, .6878386165598D-19, APQ5( 23, 27) = .4475725810474D-19, .3040308552871D-21, .7921580263731D-22, .2683325412564D-21, .2466195745570D-21, APQ5( 23, 28) = -.2772804565985D-19, .4122777712057D-20, .6754188665159D-20, -.4141840900251D-21, -.1449504322526D-21, .6449830592977D-21, APQ5( 23, 29) = .2526547011753D-15, -.1076259494468D-15, -.1604861006810D-16, .4129793504983D-17, .4471060435654D-19, -.2814441686566D-19, .2557662095781D-15, APQ5( 23, 30) = .5654626665896D-16, -.2374921888668D-15, -.3473195832252D-15, .9331081197412D-18, -.1114333165221D-20, .1201897480483D-20, .6945489596664D-16, .4189305687099D-15, APQ5( 23, 31) = -.7368457704872D-16, .1954231952373D-15, -.1655423108357D-15, -.1215023446591D-17, -.4720420756395D-20, .1934550630169D-20, -.7557637611684D-16, .1791365336996D-16, .2555002296624D-15, APQ5( 23, 32) = .2350198519801D-16, -.1003311983381D-16, -.1485599691033D-17, .3856764479765D-18, .3866037364955D-20, -.2696388560863D-20, .2377747506121D-16, .6453894706049D-17, -.7024295975793D-17, .2216646550056D-17, APQ5( 23, 33) = .7668707454546D-19, -.5831042764528D-21, -.2861548290076D-20, .5559161086068D-21, .4176215548227D-21, -.3369654932988D-21, .8038241575961D-19, .1174626010700D-20, -.8692160071761D-20, .6699776083859D-20, .1062979420069D-20, APQ5( 23, 34) = .1242932383509D-18, .2731396047934D-19, .4283939404765D-20, .8141006826895D-21, .1000976210837D-20, -.8798008951018D-21, .1105354074578D-18, -.1884309554330D-19, .4043864619091D-19, .1314747563459D-19, .1867091352772D-20, .1277903318814D-19, $ APQ5( 35, 35 ) = 3.411944855986297E-15, APQ5( 35, 36 ) = -9.993961098765528E-17, 3.513250664625000E-15, APQ5( 35, 37 ) = -2.437069027383009E-16, 2.807418003050796E-16, 1.409328231433322E-15, APQ5( 35, 38 ) = 1.947452562762970E-15,-4.082974889460758E-17, -1.407282547460761E-16, 1.369360714587576E-15, APQ5( 35, 39 ) = -3.183518148617593E-18,-5.172085285380212E-19, 5.576669917552228E-19, -1.517416422083525E-18, 2.670106258287285E-20, APQ5( 35, 40 ) = 9.869201300502101E-17, 2.187077101195288E-17, -6.115869173141696E-17, 1.383143587683706E-16,-8.976009702447546E-20, 1.253395849018215E-16, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ Extra print from SOLVE: SOLPRP( 1) = 20*0, $ 0=OFF, 1=SINGLE PRECISION, 2=DOUBLE PRECISION $ SOLPRP( 1) = 1, $ Information with a priori. $ SOLPRP( 2) = 1, $ A priori (APQ). $ SOLPRP( 4) = 2, $ Computed covariance (4 digits). $ SOLPRP( 5) = 1, $ Correlation matrix. SOLPRP( 6) = 1, $ Print 132 column SOLVE page. $ SOLPRP( 7) = 1, $ Sensitivity matrix. $ SOLPRP( 8) = 2, $ Perturbation matrix (4 digits). $ SOLPRP( 9) = 2, $ Consider covariance (4 digits). $ SOLPRP(10) = 1, $ Singular value analysis. $ 3, & 11-20 are not used. $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ TRANSLATE and EDIT $ $ "TRANSLATE" connects a name to a data type & translates the CSP commands. $ $ "EDIT" actually executes the "TRANSLATE" instructions. $ EDFLAG = .TRUE., $ TRUE ==> Data editing is on in REGRES. $ DANAMS( 1) = 100*' ', DANUMS( 1) = 100*0, $ DANAMS( 1) = 'ALL', DANUMS( 1) = 0, DANAMS( 2) = 'INS', DANUMS( 2) = 1, DANAMS( 3) = 'INQ', DANUMS( 3) = 3, DANAMS( 4) = 'IWS', DANUMS( 4) = 5, DANAMS( 5) = 'IWQ', DANUMS( 5) = 6, DANAMS( 6) = 'DDOD', DANUMS( 6) = 7, DANAMS( 7) = 'DDOR', DANUMS( 7) = 8, DANAMS( 8) = 'VLBI', DANUMS( 8) = 070008, DANAMS( 9) = 'DOPPLER', DANUMS( 9) = 110016, DANAMS(10) = 'F1', DANUMS(10) = 11, DANAMS(11) = 'F2', DANUMS(11) = 12, DANAMS(12) = 'F3', DANUMS(12) = 13, DANAMS(13) = 'F3C', DANUMS(13) = 14, DANAMS(14) = 'DF2', DANUMS(14) = 15, DANAMS(15) = 'F2MF3', DANUMS(15) = 16, DANAMS(16) = 'RANGE', DANUMS(16) = 310048, DANAMS(17) = 'ETR', DANUMS(17) = 31, DANAMS(18) = 'MARK1', DANUMS(18) = 32, DANAMS(19) = 'MARK1A', DANUMS(19) = 33, DANAMS(20) = 'TAU', DANUMS(20) = 34, DANAMS(21) = 'MU', DANUMS(21) = 35, DANAMS(22) = 'PLOP', DANUMS(22) = 36, DANAMS(23) = 'SRA', DANUMS(23) = 37, DANAMS(24) = 'MU2', DANUMS(24) = 38, DANAMS(25) = 'GSTDN', DANUMS(25) = 41, DANAMS(26) = 'DOPRNG', DANUMS(26) = 110048, DANAMS(27) = 'ANGLES', DANUMS(27) = 510058, DANAMS(28) = 'AZ', DANUMS(28) = 51, DANAMS(29) = 'EL', DANUMS(29) = 52, DANAMS(30) = 'HA', DANUMS(30) = 53, DANAMS(31) = 'DEC', DANUMS(31) = 54, DANAMS(32) = 'X30', DANUMS(32) = 55, DANAMS(33) = 'Y30', DANUMS(33) = 56, DANAMS(34) = 'X85', DANUMS(34) = 57, DANAMS(35) = 'Y85', DANUMS(35) = 58, DANAMS(36) = 'PLANPX', DANUMS(36) = 61, DANAMS(37) = 'PLANLN', DANUMS(37) = 62, DANAMS(38) = 'STARPX', DANUMS(38) = 145, DANAMS(39) = 'STARLN', DANUMS(39) = 146, DANAMS(40) = 'LDMKPX', DANUMS(40) = 143, DANAMS(41) = 'LDMKLN', DANUMS(41) = 144, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ MAPPING $ $ Input for the programs MAPGEN and MAPSEM. $ MAPGEN transforms from EME2000 to other coordinate systems. It creates $ the state vectors and mapping matrices. $ MAPSEM prints the mapped output. $ EQEPOC(1) = 99*0.0D0, $ Epoch for reference planes. DMAP(1) = 99*0.0, $ D.P. version of MAPIN(1,J) MAPIN(1,1) = 1188*' ', MAPSAT(1,1) = 792*' ', MAPSEN(1) = 99*0, $ Matrix print (0=OFF, 1=SENS, 2=PERT, 3=BOTH) $ MAPBUG( 1) = 30*0, $ MAPGEN & MAPSEM debug, covariance & planet $ mapping flags. MAPBUG(18) = 1, $ Mapped covariance print (1=OFF, 0=ON) MAPBUG(20) = 2, $ Planetary mapping is to VIEW1. $ MAPRP(1) = 0, $ Mapping matrix print (0=OFF, 1=ON) MAPRP(2) = 0, $ Mapped covariance print (0=OFF,1=S.P.,2=D.P.) MAPAP = 0, $ Mapped statistics: $ (0=FILTERED, 1=APRIORI, 2=SMOOTHED) $ CTOLR = 1.0D-5, CITLIM = 5, $ Parameters for closest approach determination $ $ EXAMPLE: $ $ B-Plane: Earth Mean Equator of Date $ $ MAPIN( 1,1) = ' ', $ Epoch to map. $ MAPIN( 2,1) = 'ET', $ Time scale. $ MAPIN( 3,1) = 'EQUATO', $ Name of the mapped to coordinate frame. $ MAPIN( 4,1) = 'EARTH', $ Body for the reference frame definition. $ MAPIN( 5,1) = 'SPACE', $ The reference plane X-axis orientation. $ MAPIN( 6,1) = 'EARTH', $ The body of the covariance center. $ MAPIN( 7,1) = 'MEAN', $ Reference plane definition. $ MAPIN( 8,1) = 'ASYMPT', $ Coordinate system $ MAPIN( 9,1) = 'EARTH', $ Target body of the event requested. $ MAPIN(10,1) = 'CLOSAP', $ Map to an event. $ MAPIN(11,1) = '01-MAY-1998 00:00:00', $ $ EME2000 Cartesian $ MAPIN(1,1)= ' ', MAPIN(2,1)= 'UTC', MAPIN(3,1)= 'EQUATO','EARTH','SPACE','PLUTO','MEAN','CARTES', 'PLUTO','CLOSAP','27-JAN-1998 00:00:00.0000','UTC', EQEPOC(1) = 2000.D0, $ $ VME2000 Cartesian $ MAPIN(1,2)= ' ', MAPIN(2,2)= 'UTC', MAPIN(3,2)= 'EQUATO','PLUTO','SPACE','PLUTO','MEAN','CARTES', 'PLUTO','CLOSAP','27-JAN-1998 00:00:00.0000','UTC', EQEPOC(2) = 2000.D0, $ $ View frame 1 $ MAPIN(1,3)= ' ', MAPIN(2,3)= 'UTC', MAPIN(3,3)= 'VIEW1',' ',' ','PLUTO',' ','CARTES', 'PLUTO','CLOSAP','27-JAN-1998 00:00:00.0000','UTC', EQEPOC(3) = 2000.D0, $ $ VME2000 classical $ MAPIN(1,4)= ' ', MAPIN(2,4)= 'UTC', MAPIN(3,4)= 'EQUATO','PLUTO','SPACE','PLUTO','MEAN','CLASSI', 'PLUTO','CLOSAP','27-JAN-1998 00:00:00.0000','UTC', EQEPOC(4) = 2000.D0, $ $ Plane-of-sky classical $ MAPIN(1,5)= ' ', MAPIN(2,5)= 'UTC', MAPIN(3,5)= 'SKYPLN','SCRAFT',' ','PLUTO',' ','CLASSI', 'PLUTO','CLOSAP','27-JAN-1998 00:00:00.0000','UTC', EQEPOC(5) = 2000.D0, $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ OUTPUT $ $ OUTPUT displays data residuals on a printed output. The program also $ generates plots and plotfiles of the data residuals. $ RSTA( 1) = 15*' ', RSTA( 1) = 'RESID','CRESID', $ Additional parameters on file. $ IPFLAG(1) = 4*0, $ $ The units of the data types in the ODP are as follows: $ $ F1, F2, F3, F2MF3: Hertz, for Doppler data types. $ SRA: Range Units, for range data. $ IWS, IWQ, DDOR: nanoseconds, for wide-band VLBI types. $ INS, INQ, DDOD: Hertz, for narrow-band VLBI types. $ X85, Y85: degrees, for angle data types. $ $ 1.0 mm/s = 0.02810 Hz for F1 and F2MF3, X-band. $ 1.0 mm/s = 0.05620 Hz for F2 and F3, X-band. $ 1.0 m = 7.01030 RU for SRA. $ 1.0 m = 3.33564 nanoseconds for IWS, IWQ, and DDOR. $ = 141.333 nanoradians. $ 1.0 mm/s = 0.02810 Hz for INS, INQ, and DDOD, X-band. $ PLDTYP( 1) = 'F1', PLTBND( 1) = 'X', PLSCAL( 1) = 1.4050, PLDTYP( 2) = 'F2', PLTBND( 2) = 'X', PLSCAL( 2) = 2.8100, PLDTYP( 3) = 'F3', PLTBND( 3) = 'X', PLSCAL( 3) = 2.8100, PLDTYP( 4) = 'F2MF3', PLTBND( 4) = 'X', PLSCAL( 4) = 1.4050, PLDTYP( 5) = 'SRA', PLTBND( 5) = 'X', PLSCAL( 5) = 35052.0, PLDTYP( 6) = 'IWS', PLTBND( 6) = 'X', PLSCAL( 6) = 50.00, PLDTYP( 7) = 'IWQ', PLTBND( 7) = 'X', PLSCAL( 7) = 50.00, PLDTYP( 8) = 'DDOR', PLTBND( 8) = 'X', PLSCAL( 8) = 50.00, PLDTYP( 9) = 'INS', PLTBND( 9) = 'X', PLSCAL( 9) = 1.4050, PLDTYP(10) = 'INQ', PLTBND(10) = 'X', PLSCAL(10) = 1.4050, PLDTYP(11) = 'DDOD', PLTBND(11) = 'X', PLSCAL(11) = 1.4050, PLDTYP(12) = 'X85', PLTBND(12) = ' ', PLSCAL(12) = 1.00, PLDTYP(13) = 'Y85', PLTBND(13) = ' ', PLSCAL(13) = 1.00, $ OUTBEG = '17-FEB-1996 00:00:00', $ Launch date. OUTEND = '01-JUL-2000 00:00:00', $ End-of-mission? $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $ $ TABWET and TABDRY from C. C. Chao 8/29/77. $ $ The elevation angle (in degrees) corresponding to each TAB value lies $ above it in the table. $ $ 1) Mottinger, N. A., "Reflections on Refraction -- A Historical Overview $ of the Tropospheric Refraction Model in the ODP," JPL IOM 314.10-385, $ January 18, 1984. $ $ 2) Chao, C. C., "Improved Tropospheric Mapping Tables Including Bending $ Effect for SATODP," JPL IOM 391.3-637, December 28, 1972. $ $ 3) Chao, C. C., "Improved Estimation of the Parameters and Mapping Tables $ of Tropospheric Calibration for MM71," JPL IOM 391.3-352, May 25, 1971. $ TABWET(1) = 261*0.0D0, $ TABWET(1) = $ .00 61.5790, $ .10 .20 .30 .40 .50 .60 .70 .80 .90 , 57.8413,54.3927,51.2432,48.3625,45.7235,43.3021,41.0769,39.0284,37.1397, $ 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 , 35.3955,33.7820,32.2870,30.8996,29.6100,28.4095,27.2901,26.2449,25.2675, $ 1.90 2.00 2.10 2.20 2.30 2.40 2.50 2.60 2.70 , 24.3521,23.4935,22.6873,21.9291,21.2152,20.5420,19.9066,19.3060,18.7377, $ 2.80 2.90 3.00 3.10 3.20 3.30 3.40 3.50 3.60 , 18.1994,17.6889,17.2042,16.7435,16.3053,15.8880,15.4903,15.1108,14.7484, $ 3.70 3.80 3.90 4.00 4.10 4.20 4.30 4.40 4.50 , 14.4021,14.0709,13.7538,13.4500,13.1587,12.8792,12.6109,12.3530,12.1051, $ 4.60 4.70 4.80 4.90 5.00 5.10 5.20 5.30 5.40 , 11.8666,11.6369,11.4157,11.2024,10.9967,10.7982,10.6065,10.4213,10.2423, $ 5.50 5.60 5.70 5.80 5.90 6.00 6.10 6.20 6.30 , 10.0692, 9.9017, 9.7395, 9.5824, 9.4302, 9.2827, 9.1396, 9.0008, 8.8660, $ 6.40 6.50 6.60 6.70 6.80 6.90 7.00 7.10 7.20 , 8.7352, 8.6081, 8.4845, 8.3645, 8.2477, 8.1341, 8.0235, 7.9159, 7.8111, $ 7.30 7.40 7.50 7.60 7.70 7.80 7.90 8.00 8.10 , 7.7090, 7.6094, 7.5125, 7.4179, 7.3256, 7.2356, 7.1478, 7.0621, 6.9784, $ 8.20 8.30 8.40 8.50 8.60 8.70 8.80 8.90 9.00 , 6.8966, 6.8167, 6.7387, 6.6624, 6.5878, 6.5148, 6.4435, 6.3737, 6.3054, $ 9.10 9.20 9.30 9.40 9.50 9.60 9.70 9.80 9.90 , 6.2385, 6.1730, 6.1089, 6.0462, 5.9847, 5.9244, 5.8653, 5.8075, 5.7507, $ 10.00 10.50 11.00 11.50 12.00 12.50 13.00 13.50 14.00 , 5.6951, 5.4323, 5.1929, 4.9739, 4.7728, 4.5876, 4.4164, 4.2578, 4.1104, $ 14.50 15.00 15.50 16.00 16.50 17.00 17.50 18.00 18.50 , 3.9731, 3.8449, 3.7250, 3.6125, 3.5069, 3.4075, 3.3138, 3.2253, 3.1417, $ 19.00 19.50 20.00 20.50 21.00 21.50 22.00 22.50 23.00 , 3.0625, 2.9874, 2.9160, 2.8483, 2.7838, 2.7223, 2.6637, 2.6078, 2.5543, $ 23.50 24.00 24.50 25.00 25.50 26.00 26.50 27.00 27.50 , 2.5032, 2.4542, 2.4073, 2.3624, 2.3192, 2.2778, 2.2380, 2.1997, 2.1629, $ 28.00 28.50 29.00 29.50 30.00 30.50 31.00 31.50 32.00 , 2.1274, 2.0932, 2.0603, 2.0285, 1.9979, 1.9683, 1.9397, 1.9121, 1.8854, $ 32.50 33.00 33.50 34.00 34.50 35.00 35.50 36.00 36.50 , 1.8595, 1.8345, 1.8103, 1.7869, 1.7642, 1.7422, 1.7209, 1.7002, 1.6801, $ 37.00 37.50 38.00 38.50 39.00 39.50 40.00 40.50 41.00 , 1.6606, 1.6417, 1.6233, 1.6055, 1.5882, 1.5713, 1.5549, 1.5390, 1.5235, $ 41.50 42.00 42.50 43.00 43.50 44.00 44.50 45.00 45.50 , 1.5085, 1.4938, 1.4796, 1.4657, 1.4522, 1.4390, 1.4262, 1.4137, 1.4016, $ 46.00 46.50 47.00 47.50 48.00 48.50 49.00 49.50 50.00 , 1.3897, 1.3782, 1.3669, 1.3559, 1.3452, 1.3348, 1.3247, 1.3147, 1.3051, $ 50.50 51.00 51.50 52.00 52.50 53.00 53.50 54.00 54.50 , 1.2957, 1.2865, 1.2775, 1.2687, 1.2602, 1.2519, 1.2438, 1.2358, 1.2281, $ 55.00 55.50 56.00 56.50 57.00 57.50 58.00 58.50 59.00 , 1.2206, 1.2132, 1.2060, 1.1990, 1.1922, 1.1855, 1.1790, 1.1727, 1.1665, $ 59.50 60.00 60.50 61.00 61.50 62.00 62.50 63.00 63.50 , 1.1604, 1.1546, 1.1488, 1.1432, 1.1378, 1.1325, 1.1273, 1.1222, 1.1173, $ 64.00 64.50 65.00 65.50 66.00 66.50 67.00 67.50 68.00 , 1.1125, 1.1078, 1.1033, 1.0989, 1.0946, 1.0904, 1.0863, 1.0823, 1.0785, $ 68.50 69.00 69.50 70.00 70.50 71.00 71.50 72.00 72.50 , 1.0747, 1.0711, 1.0676, 1.0641, 1.0608, 1.0576, 1.0545, 1.0514, 1.0485, $ 73.00 73.50 74.00 7 .50 75.00 75.50 76.00 76.50 77.00 , 1.0457, 1.0429, 1.0403, 1.0377, 1.0353, 1.0329, 1.0306, 1.0284, 1.0263, $ 77.50 78.00 78.50 79.00 79.50 80.00 80.50 81.00 81.50 , 1.0243, 1.0223, 1.0205, 1.0187, 1.0170, 1.0154, 1.0139, 1.0125, 1.0111, $ 82.00 82.50 83.00 83.50 84.00 84.50 85.00 85.50 86.00 , 1.0098, 1.0086, 1.0075, 1.0065, 1.0055, 1.0046, 1.0038, 1.0031, 1.0024, $ 86.50 87.00 87.50 88.00 88.50 89.00 89.50 90.00 , 1.0019, 1.0014, 1.0010, 1.0006, 1.0003, 1.0002, 1.0000, 1.0000, $ TABDRY(1) = 261*0.0D0, $ TABDRY(1) = $ .00 33.1457, $ .10 .20 .30 .40 .50 .60 .70 .80 .90 , 32.0301,30.9687,29.9582,28.9957,28.0787,27.2046,26.3712,25.5761,24.8173, $ 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 , 24.0929,23.4009,22.7396,22.1074,21.5028,20.9255,20.3703,19.8398,19.3314, $ 1.90 2.00 2.10 2.20 2.30 2.40 2.50 2.60 2.70 , 18.8441,18.3768,17.9283,17.4978,17.0843,16.6870,16.3051,15.9378,15.5844, $ 2.80 2.90 3.00 3.10 3.20 3.30 3.40 3.50 3.60 , 15.2443,14.9167,14.6011,14.2969,14.0036,13.7207,13.4476,13.1840,12.9294, $ 3.70 3.80 3.90 4.00 4.10 4.20 4.30 4.40 4.50 , 12.6834,12.4455,12.2156,11.9931,11.7778,11.5693,11.3675,11.1719,10.9823, $ 4.60 4.70 4.80 4.90 5.00 5.10 5.20 5.30 5.40 , 10.7985,10.6203,10.4473,10.2795,10.1165, 9.9523, 9.8046, 9.6552, 9.5099, $ 5.50 5.60 5.70 5.80 5.90 6.00 6.10 6.20 6.30 , 9.3687, 9.2313, 9.0976, 8.9675, 8.8408, 8.7175, 8.5973, 8.4802, 8.3661, $ 6.40 6.50 6.60 6.70 6.80 6.90 7.00 7.10 7.20 , 8.2548, 8.1463, 8.0405, 7.9373, 7.8365, 7.7382, 7.6421, 7.5484, 7.4567, $ 7.30 7.40 7.50 7.60 7.70 7.80 7.90 8.00 8.10 , 7.3672, 7.2798, 7.1943, 7.1107, 7.0289, 6.9490, 6.8707, 6.7942, 6.7193, $ 8.20 8.30 8.40 8.50 8.60 8.70 8.80 8.90 9.00 , 6.6459, 6.5741, 6.5038, 6.4349, 6.3675, 6.3014, 6.2366, 6.1731, 6.1108, $ 9.10 9.20 9.30 9.40 9.50 9.60 9.70 9.80 9.90 , 6.0529, 5.9930, 5.9342, 5.8735, 5.8170, 5.7615, 5.7071, 5.6537, 5.6012, $ 10.00 10.50 11.00 11.50 12.00 12.50 13.00 13.50 14.00 , 5.5497, 5.3055, 5.0773, 4.8761, 4.6863, 4.5106, 4.3477, 4.1963, 4.0551, $ 14.50 15.00 15.50 16.00 16.50 17.00 17.50 18.00 18.50 , 3.9232, 3.7998, 3.6840, 3.5753, 3.4729, 3.3764, 3.2853, 3.1992, 3.1176, $ 19.00 19.50 20.00 20.50 21.00 21.50 22.00 22.50 23.00 , 3.0403, 2.9668, 2.8971, 2.8307, 2.7674, 2.7071, 2.6496, 2.5946, 2.5420, $ 23.50 24.00 24.50 25.00 25.50 26.00 26.50 27.00 27.50 , 2.4917, 2.4434, 2.3972, 2.3529, 2.3103, 2.2694, 2.2301, 2.1923, 2.1559, $ 28.00 28.50 29.00 29.50 30.00 30.50 31.00 31.50 32.00 , 2.1208, 2.0870, 2.0544, 2.0230, 1.9926, 1.9633, 1.9350, 1.9076, 1.8811, $ 32.50 33.00 33.50 34.00 34.50 35.00 35.50 36.00 36.50 , 1.8555, 1.8307, 1.8067, 1.7834, 1.7609, 1.7391, 1.7179, 1.6973, 1.6774, $ 37.00 37.50 38.00 38.50 39.00 39.50 40.00 40.50 41.00 , 1.6580, 1.6392, 1.6210, 1.6033, 1.5860, 1.5693, 1.5530, 1.5372, 1.5218, $ 41.50 42.00 42.50 43.00 43.50 44.00 44.50 45.00 45.50 , 1.5068, 1.4922, 1.4780, 1.4642, 1.4507, 1.4376, 1.4249, 1.4125, 1.4004, $ 46.00 46.50 47.00 47.50 48.00 48.50 49.00 49.50 50.00 , 1.3886, 1.3771, 1.3659, 1.3549, 1.3443, 1.3339, 1.3238, 1.3139, 1.3043, $ 50.50 51.00 51.50 52.00 52.50 53.00 53.50 54.00 54.50 , 1.2949, 1.2857, 1.2768, 1.2681, 1.2596, 1.2513, 1.2432, 1.2353, 1.2276, $ 55.00 55.50 56.00 56.50 57.00 57.50 58.00 58.50 59.00 , 1.2200, 1.2127, 1.2055, 1.1986, 1.1917, 1.1851, 1.1786, 1.1723, 1.1661, $ 59.50 60.00 60.50 61.00 61.50 62.00 62.50 63.00 63.50 , 1.1601, 1.1542, 1.1485, 1.1429, 1.1375, 1.1322, 1.1270, 1.1220, 1.1171, $ 64.00 64.50 65.00 65.50 66.00 66.50 67.00 67.50 68.00 , 1.1123, 1.1076, 1.1031, 1.0987, 1.0944, 1.0902, 1.0861, 1.0822, 1.0783, $ 68.50 69.00 69.50 70.00 70.50 71.00 71.50 72.00 72.50 , 1.0746, 1.0709, 1.0674, 1.0640, 1.0607, 1.0575, 1.0543, 1.0513, 1.0484, $ 73.00 73.50 74.00 74.50 75.00 75.50 76.00 76.50 77.00 , 1.0456, 1.0428, 1.0402, 1.0377, 1.0352, 1.0328, 1.0305, 1.0283, 1.0262, $ 77.50 78.00 78.50 79.00 79.50 80.00 80.50 81.00 81.50 , 1.0242, 1.0223, 1.0204, 1.0187, 1.0170, 1.0154, 1.0139, 1.0124, 1.0111, $ 82.00 82.50 83.00 83.50 84.00 84.50 85.00 85.50 86.00 , 1.0098, 1.0086, 1.0075, 1.0065, 1.0055, 1.0046, 1.0038, 1.0031, 1.0024, $ 86.50 87.00 87.50 88.00 88.50 89.00 89.50 90.00 , 1.0019, 1.0014, 1.0010, 1.0006, 1.0003, 1.0002, 1.0000, 1.0000, $ $ End TAB table of 8/29/77 $ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$