INPUT NAMELIST FROM FILE OINML : $INPUT SC_NAME = 'JA2 ' ! Spacecraft Initial Conditions IC(1) = 0.5413332561165851E+04 IC(2) = -0.2971293786892220E+02 IC(3) = 0.5498143491249568E+04 IC(4) = -0.4152361292470300E+01 IC(5) = 0.4186640973179191E+01 IC(6) = 0.4107226192421614E+01 PARTLS = 'DRAG', DRAG_COEFF = 0.1828602554546782E+02 START = '16-JUL-2010 00:00:00.0000 UTC ' STOP = '17-JUL-2010 00:00:00.0000 UTC ' ! $Id$ ! customer sc_model for OSTM, including altimeter and AMR antenna dish, but no p DEBUG=0 ! Extra partials ! PARTLS(1)='CONST_H','CONST_C','CONST_L','CONST_X','CONST_Y', ! PARTLS(6)='ONCE_PER_REV','TWICE_PER_REV' ITERATE_SMOOTH_TIME=0.0D0 ! Spacecraft model MASS=501.862 SC_MODEL = 'CUSTOM' SC_ATTITUDE = 'TOPEX' READ_ATTITUDE_FILE_ON_OFF='ON' ! CUSTOM Macro model COMPONENT_NAME(1) ='X+', 'X-', 'Y+', 'Y-', 'Z+', 'Z-', 'S+', 'S-', 'AD', 'MR COMPONENT_AREA =0.912,0.912,2.147,2.147,1.165,2.147,9.536,9.536,1.131,0.7 COMPONENT_SPECULAR=0.425,0.408,0.334,0.274,0.236,0.298,0.344,0.004,0.408,0.4 COMPONENT_DIFFUSE =0.178,0.186,0.342,0.369,0.382,0.336,0.006,0.298,0.186,0.1 COMPONENT_ORIENTATION(1,1) = 'ALONG SC_X' ! +X side COMPONENT_ORIENTATION(1,2) = '- SC_X' ! -X side COMPONENT_ORIENTATION(1,3) = 'ALONG SC_Y' ! +Y side COMPONENT_ORIENTATION(1,4) = '- SC_Y' ! -Y side COMPONENT_ORIENTATION(1,5) = 'ALONG SC_Z' ! +Z side COMPONENT_ORIENTATION(1,6) = '- SC_Z' ! -Z side COMPONENT_ORIENTATION(1,7) = 'A = TOWARD SUN' ! Sun direction COMPONENT_ORIENTATION(2,7) = 'b = A DOT Y+' ! cosine of sun-sc-Y angle COMPONENT_ORIENTATION(3,7) = 'C = b * Y+' ! sun vector projected on Y COMPONENT_ORIENTATION(4,7) = 'A - C' ! +S solar panel side COMPONENT_ORIENTATION(1,8) = '- S+' ! -S solar panel side COMPONENT_ORIENTATION(1,9) = 'ALONG SC_Z' ! altimeter dish pointing d COMPONENT_ORIENTATION(1,10) = 'D1 = 0.5 * SC_X' ! AMR dish back tilt about COMPONENT_ORIENTATION(2,10) = 'E1 = 0.866 * SC_Z'! and up COMPONENT_ORIENTATION(3,10) = 'D1 - E1' ! AMR dish back COMPONENT_ORIENTATION(1,11) = '- MR+' ! AMR dish face down ! Integration control STATE_TOL=1.0D-10 VARY_TOL=1.0D-7 ! Gravity model OBLATENESS_ON_OFF='ON' GRAVITY_FILE='/GIPSY_source/goa-var/etc/gravity_fields/GGM02C.200x200' ! jem01_rl03b_180-J34_rate.nml was used in release07b.nml ! Tide models SOLID_TIDE_ON_OFF='ON' POLE_TIDE_ON_OFF='ON' OCEAN_TIDE_ON_OFF='ON' ! TIDES_FILE = '/GIPSY_source/goa-var/etc/gravity_fields/tides.csr4.0+teg4.335 TIDES_FILE = '/GIPSY_source/goa-var/etc/gravity_fields/fes04S1convdelta+opol ! Relativity model RELATIVITY_ON_OFF='ON' ! Custom force model CONSTANT_ACC_HCL_ON_OFF='ON' HALF_PER_REV_ACC_HCL_ON_OFF='OFF' ONCE_PER_REV_ACC_HCL_ON_OFF='ON' TWICE_PER_REV_ACC_HCL_ON_OFF='ON' ! Atmospheric drag model ATMOS_ON_OFF='ON' DRAG_COEFF=2.04 ATMOS_DENSITY_MODEL='DTM2000' ATMOS_FILE='/GIPSY_source/goa-var/etc/atmos_flux.nml' ! ATMOS_FILE='/orms2/projects/sacc/atmos_flux.nml' ! Earth radiation model EARTH_RAD_ON_OFF='ON' EC=102050600D0 ! Solar pressure model SOLAR_PRESSURE_ON_OFF='ON' SC=102050600D0 ! CONSTANT_ACC_XYZ_ON_OFF='ON' ! CONSTANT_ACC_X = 1.8401145E-01 ! 0.09 micro Newton ! CONSTANT_ACC_Y = 3.6802290E-01 ! 0.18 micro Newton ! Solar Array Ramp Biases !Stop Solar Array Ramp to Bias Position -50.5 1996-326T08:07:41P 154 080 !Start Solar Array Ramp to Bias Position 1996-334T09:17:00P 155 032 !Stop Solar Array Ramp to Bias Position +50.5 1996-334T09:27:10P 155 032 ! SOLAR_ARRAY_BIAS = -50.5, 50.5 ! ARRAY_BIAS_TIMES = -97468980.0, -97468370.0 ! TOPEX Solar, Drag, Albedo Coefficients, and Empirical Forces : ! Start Auto Update ! End Auto Update $tpnml IT( 1)= 090101, TP( 1)= 284040000., 34.000000, 0.0000E+00, IT( 4)= 800101, TP( 4)= 2524564800., 0.000000, 0.0000E+00, IT( 7)= 800101, TP( 7)= 2524564800., 0.000000, 0.0000E+00, IT( 10)= 800101, TP( 10)= 2524564800., 0.000000, 0.0000E+00, IT( 13)= 800101, TP( 13)= 2524564800., 0.000000, 0.0000E+00, IT( 16)= 800101, TP( 16)= 2524564800., 0.000000, 0.0000E+00, IT( 19)= 800101, TP( 19)= 2524564800., 0.000000, 0.0000E+00, IT( 22)= 800101, TP( 22)= 2524564800., 0.000000, 0.0000E+00, IT( 25)= 800101, TP( 25)= 2524564800., 0.000000, 0.0000E+00, IT( 28)= 800101, TP( 28)= 2524564800., 0.000000, 0.0000E+00, IT( 31)= 800101, TP( 31)= 2524564800., 0.000000, 0.0000E+00, IT( 34)= 800101, TP( 34)= 2524564800., 0.000000, 0.0000E+00, IT( 37)= 800101, TP( 37)= 2524564800., 0.000000, 0.0000E+00, IT( 40)= 100712, TP( 40)= 332164800., 34.053674, -0.3421E-08, IT( 43)= 100713, TP( 43)= 332251200., 34.053493, -0.6765E-09, IT( 46)= 100714, TP( 46)= 332337600., 34.053549, 0.1795E-08, IT( 49)= 100715, TP( 49)= 332424000., 34.053777, 0.3362E-08, IT( 52)= 100716, TP( 52)= 332510400., 34.054102, 0.3972E-08, IT( 55)= 100717, TP( 55)= 332596800., 34.054423, 0.3192E-08, IT( 58)= 100718, TP( 58)= 332683200., 34.054640, 0.1931E-08, IT( 61)= 100719, TP( 61)= 332769600., 34.054659, -0.1552E-08, IT( 64)= 100720, TP( 64)= 332856000., 34.054380, -0.4907E-08, IT( 67)= 100721, TP( 67)= 332942400., 34.053831, -0.7519E-08, IT( 70)= 800101, TP( 70)= 2524564800., 0.000000, 0.0000E+00, IT( 73)= 800101, TP( 73)= 2524564800., 0.000000, 0.0000E+00, IT( 76)= 800101, TP( 76)= 2524564800., 0.000000, 0.0000E+00, IT( 79)= 800101, TP( 79)= 2524564800., 0.000000, 0.0000E+00, IT( 82)= 800101, TP( 82)= 2524564800., 0.000000, 0.0000E+00, IT( 85)= 800101, TP( 85)= 2524564800., 0.000000, 0.0000E+00, IT( 88)= 800101, TP( 88)= 2524564800., 0.000000, 0.0000E+00, IT( 91)= 800101, TP( 91)= 2524564800., 0.000000, 0.0000E+00, IT( 94)= 800101, TP( 94)= 2524564800., 0.000000, 0.0000E+00, IT( 97)= 800101, TP( 97)= 2524564800., 0.000000, 0.0000E+00, IT(100)= 800101, TP(100)= 2524564800., 0.000000, 0.0000E+00, IT(103)= 800101, TP(103)= 2524564800., 0.000000, 0.0000E+00, IT(106)= 800101, TP(106)= 2524564800., 0.000000, 0.0000E+00, IT(109)= 800101, TP(109)= 2524564800., 0.000000, 0.0000E+00, IT(112)= 800101, TP(112)= 2524564800., 0.000000, 0.0000E+00, IT(115)= 800101, TP(115)= 2524564800., 0.000000, 0.0000E+00, IT(118)= 800101, TP(118)= 2524564800., 0.000000, 0.0000E+00, IT(121)= 800101, TP(121)= 2524564800., 0.000000, 0.0000E+00, IT(124)= 800101, TP(124)= 2524564800., 0.000000, 0.0000E+00, IT(127)= 800101, TP(127)= 2524564800., 0.000000, 0.0000E+00, IT(130)= 800101, TP(130)= 2524564800., 0.000000, 0.0000E+00, IT(133)= 800101, TP(133)= 2524564800., 0.000000, 0.0000E+00, IT(136)= 800101, TP(136)= 2524564800., 0.000000, 0.0000E+00, IT(139)= 800101, TP(139)= 2524564800., 0.000000, 0.0000E+00, IT(142)= 800101, TP(142)= 2524564800., 0.000000, 0.0000E+00, IT(145)= 800101, TP(145)= 2524564800., 0.000000, 0.0000E+00, IT(148)= 800101, TP(148)= 2524564800., 0.000000, 0.0000E+00, IT(151)= 100712, TP(151)= 332164800., 0.09307, 0.27336E-07, 0.48456, -0.22 IT(156)= 100713, TP(156)= 332251200., 0.09546, 0.28834E-07, 0.48439, -0.17 IT(161)= 100714, TP(161)= 332337600., 0.09806, 0.28342E-07, 0.48426, -0.18 IT(166)= 100715, TP(166)= 332424000., 0.10036, 0.24702E-07, 0.48406, -0.40 IT(171)= 100716, TP(171)= 332510400., 0.10233, 0.22573E-07, 0.48355, -0.75 IT(176)= 100717, TP(176)= 332596800., 0.10426, 0.24801E-07, 0.48277, -0.11 IT(181)= 100718, TP(181)= 332683200., 0.10661, 0.29893E-07, 0.48158, -0.14 IT(186)= 100719, TP(186)= 332769600., 0.10943, 0.31479E-07, 0.48026, -0.12 IT(191)= 100720, TP(191)= 332856000., 0.11205, 0.31149E-07, 0.47942, -0.96 IT(196)= 100721, TP(196)= 332942400., 0.11481, 0.30877E-07, 0.47859, -0.88 IT(201)= 800101, TP(201)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(206)= 800101, TP(206)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(211)= 800101, TP(211)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(216)= 800101, TP(216)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(221)= 800101, TP(221)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(226)= 800101, TP(226)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(231)= 800101, TP(231)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(236)= 800101, TP(236)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(241)= 800101, TP(241)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(246)= 800101, TP(246)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(251)= 800101, TP(251)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(256)= 800101, TP(256)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(261)= 800101, TP(261)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(266)= 800101, TP(266)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(271)= 800101, TP(271)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(276)= 800101, TP(276)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(281)= 800101, TP(281)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(286)= 800101, TP(286)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(291)= 800101, TP(291)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(296)= 800101, TP(296)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(301)= 800101, TP(301)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(306)= 800101, TP(306)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(311)= 800101, TP(311)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(316)= 800101, TP(316)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(321)= 800101, TP(321)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(326)= 800101, TP(326)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 IT(331)= 800101, TP(331)= 2524564800., 0.00000, 0.00000E+00, 0.00000, 0.00 TPTYPE = 'UT1 ' $end TP array has been read from input namelist. Initialize the TP array: The TP type = UT1 Zonal tide model to use = IERS03 There is no Extended_EO_Model Parameter Input No ocean tides EO model will be used. Reading attitude modes from file /GIPSY_source/daily_builds/goa-ops.2008.05.28a/topex_daily/data/attitude Message from subroutine topex_yaw! Topex starts its orbit at beta angle (deg) -21.8352006 Yaw steering mode as computed by the internal model is: Sinusoidal Steering ************************************************ ****** INTEGRATION SUMMARY AND STATISTICS ****** Integrations start time = 332510466.1840000 Integrations stop time = 332596866.1840000 Maximum integration step size = 43.7197 Minimum integration step size = 0.0068 Number of integration steps = 4190 The participating force models were: NEWTONIAN POINT MASS RELATIVITY OBLATENESS SOLAR PRESSURE CUSTOM TIDES(SOLID,OCEAN,POLE) EARTH RADIATION ATMOSPHERE DRAG CUSTOM FORCE