-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Windows 10/MATLAB R2017a/VS 2013
Tested build: 2021-08-19
Regression build: 2021-08-18
Total number of scripts: 15828 (+97 deferred)
Percent Passed: 99.23%
New issues: 87
Output changes: 41
New truth failures: 5
New crashes: 0
New script errors: 39
New comparator errors: 2
Fixed issues: 27
Total issues: 130
Test system warnings: 59
New deferred issues: 7
Fixed deferred issues: 0
Total deferred issues: 74
Run Time: 23 hours, 32 minutes, 53 seconds
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
BatchEstimator_ReportStyle_Verbose_MultiSat_SpaceToSpace [#1143 failed]
[GMT-7421]
EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_CCSDS [#13 failed]
EphemStressTests_Default_Prop_CCSDS_Forward_and_BackwardDirect []
[GMT-6840]
Matlab_NoInputsOutputs []
Smoother_Filter_RandomConstCd_GpsPosVec [Parameter EstSat.Cd error
0.001223 exceeds tolerance 0.001000]
Output changes (but still pass):
BatchEstimator_Propagator_EphProp_Numerical_TDRS
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantADSF_GN
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantBias_DSN
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantCd_GN
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantCr_DSN_Sun
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantNPlate_DSN_Sun
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantSPADDrag_GN
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantSPADSRP_DSN_Sun
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantTSF_DSN
Ephem_GMAT_CCSDS_OEM_60sec
Ephem_GMAT_CCSDS_OEM_60sec_backward
Ephem_GMAT_CCSDS_OEM_60sec_for_loop
Ephem_GMAT_CCSDS_OEM_60sec_if_loop
Ephem_GMAT_CCSDS_OEM_60sec_ifelse1_loop
Ephem_GMAT_CCSDS_OEM_60sec_ifelse2_loop
Ephem_GMAT_CCSDS_OEM_60sec_IterativeProcess_Optimizer
Ephem_GMAT_CCSDS_OEM_60sec_target
Ephem_GMAT_CCSDS_OEM_60sec_while_loop
Ephem_GMAT_CCSDS_OEM_60sec_with_1DV_IB
Ephem_GMAT_CCSDS_OEM_60sec_with_600secFB
Ephem_GMAT_CCSDS_OEM_3600sec
Ephem_GMAT_CCSDS_OEM_86400sec_IterativeProcess_Target_and_DynamicsChange
Ephem_GMAT_CCSDS_OEM_DefaultIntegrationStep_with_1DV_IB
Ephem_GMAT_CCSDS_OEM_ForwardProp_BackrProp_Monotonic_time
Ephem_GMAT_InitialEpoch_FinalEpoch_StepSize
EphemStressTests_Default_and_ABM_Integrator_CCSDS_60Sec_MultipleSCs_ForwardDirection
EphemStressTests_Default_Prop_CCSDS_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection
EphemStressTests_Default_Prop_CCSDS_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect
EphemStressTests_Default_Prop_CCSDS_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
EphemStressTests_PD78_ABM_Prop_CCSDS_60Sec_Step_ForwardDirection
EphemStressTests_PD78_ABM_Prop_CCSDS_60Sec_Step_ForwardDirection_New
EphemStressTests_SPK_Integrator_CCSDS_60Sec_ForwardDirection
GMAT_ToggleEphemeris_MiddleOff
GMAT_ToggleEphemeris_StartOffToggleOn
GMAT_ToggleEphemeris_TwoEphemeris
GMATFunction_Global_EphemerisFile
GMATFunction_Global_EphemerisFile_With_Toggle
GMATFunction_Global_EphemerisFile_With_Toggle_2
GMATFunction_Hohmann_Targeter_Inside
Function_PassLocal_SC_In_Receive_LocalSC_Out_EphemerisFile
Output changes (but still fail):
BatchEstimator_Propagator_SPK_GN [#1 failed] [GMT-7289]
KalmanFilter_Propagator_SPK_TDRS [The test run failed to converge]
[GMT-7289]
New crashes/hangs/etc.:
None
New script errors:
AttitudeProp_CCSDS_EulerAngle_121
AttitudeProp_CCSDS_EulerAngle_123
AttitudeProp_CCSDS_EulerAngle_131
AttitudeProp_CCSDS_EulerAngle_132
AttitudeProp_CCSDS_EulerAngle_212
AttitudeProp_CCSDS_EulerAngle_213
AttitudeProp_CCSDS_EulerAngle_231
AttitudeProp_CCSDS_EulerAngle_232
AttitudeProp_CCSDS_EulerAngle_312
AttitudeProp_CCSDS_EulerAngle_313
AttitudeProp_CCSDS_EulerAngle_323
AttitudeProp_CCSDS_EulerAngle_FrameAndAttitudeDir
AttitudeProp_CCSDS_EulerAngle_OutputDCM
AttitudeProp_CCSDS_EulerAngle_OutputMRP
AttitudeProp_CCSDS_EulerAngle_OutputQuat
AttitudeProp_CCSDS_EulerAngle_ZeroInterpolationDegree
AttitudeProp_CCSDS_EulerAngle
AttitudeProp_CCSDS_MixedAttitudeSegment
AttitudeProp_CCSDS_Quaternion_FrameAndAttitudeDir
AttitudeProp_CCSDS_Quaternion_OutputDCM
AttitudeProp_CCSDS_Quaternion_OutputEuler
AttitudeProp_CCSDS_Quaternion_OutputMRP
AttitudeProp_CCSDS_Quaternion_QuatType_First
AttitudeProp_CCSDS_Quaternion
AttitudeProp_EulerFile_DOYFormat_EndOfYearLeap
AttitudeProp_EulerFile_DOYFormat
CCSDS_EdgeCornerStress_ChangeFileInCommand
CCSDS_EdgeCornerStress_InterpolateCloseToBeginningAndEnd
CCSDS_EdgeCornerStress_LargeFile
JWST_SPAD_CCSDSAttitude_EarthSPAD
MatlabFunction_Custom_DegToRad_Assignment
MatlabFunction_Custom_magic
MatlabFunction_Custom
Optimize_fmincon_ExitMode_DiscardAndContinue_2
Optimize_fmincon_SolveMode_Defaultscript
Optimize_fmincon_SolveMode_Solve
Plate_Prop_AreaCoefficient_AEM
Plate_SolveFors_AreaCoefficient_UseAEM
scriptEvent_optimizer_fmincon__InitialValue_Variable
New comparator errors:
CCSDS_EdgeCornerStress_ChangeModeInCommand (truth)
CCSDS_EdgeCornerStress_ChangeModeInCommand (reg)
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
BatchEstimator_FreezeMeasurementEditing_MultiSat_SpaceToSpace
BatchEstimator_Propagator_Code500_TDRS [GMT-7289]
BatchEstimator_ReportFile_MultiSat_SpaceToSpace
fmincon_Report
fmincon_ShowProgress
Optimize_fmincon_cvg_status
Optimize_fmincon_cvg_status
SpacecraftNavigation_MultiSat_SpaceToSpace_MoonSun
Vary_optimizer_fmincon_Additive_and_Multiplicative_ScaleFactor_RealNumber
Vary_optimizer_fmincon_AdditiveScaleFactor_ArrayElement
Vary_optimizer_fmincon_MultiplicativeScaleFactor_ArrayElement
Vary_optimizer_fmincon_MultiplicativeScaleFactor_Variable
Write_Spacecraft_NavigationHardware
Fixed crashes/hangs/etc.:
None
Fixed script errors:
Optimize_fmincon_ExitMode_DiscardAndContinue_3
Optimize_fmincon_Minimize_Height_on_circle_4
Optimize_fmincon_SolveMode_RunInitialGuess
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable
Vary_optimizer_fmincon_Perturbation_ArrayElement
Vary_optimizer_fmincon_Perturbation_RealNumber
Vary_optimizer_fmincon_Perturbation_Variable
Vary_optimizer_fmincon_UpperBound_Variable
Vary_optimizer_fmincon__InitialValue_Array
Vary_optimizer_fmincon__InitialValue_Variable
Vary_optimizer_fmincon__LowerBound_RealNumber
completed_steps_1_thru_10_of_FRC_1_using_fmincon_Optimizer
fmincon_ConstraintTolerance
scriptEvent_optimizer_fmincon__InitialValue_RealNumber
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
None
Script errors:
AttitudeProp_CCSDS_EulerAngle_121:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_121.report
does not exist
AttitudeProp_CCSDS_EulerAngle_123:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_123.report
does not exist
AttitudeProp_CCSDS_EulerAngle_131:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_131.report
does not exist
AttitudeProp_CCSDS_EulerAngle_132:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_132.report
does not exist
AttitudeProp_CCSDS_EulerAngle_212:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_212.report
does not exist
AttitudeProp_CCSDS_EulerAngle_213:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_213.report
does not exist
AttitudeProp_CCSDS_EulerAngle_231:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_231.report
does not exist
AttitudeProp_CCSDS_EulerAngle_232:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_232.report
does not exist
AttitudeProp_CCSDS_EulerAngle_312:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_312.report
does not exist
AttitudeProp_CCSDS_EulerAngle_313:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_313.report
does not exist
AttitudeProp_CCSDS_EulerAngle_323:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_323.report
does not exist
AttitudeProp_CCSDS_EulerAngle_FrameAndAttitudeDir:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_FrameAndAttitudeDir.report
does not exist
AttitudeProp_CCSDS_EulerAngle_OutputDCM:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_OutputDCM.report
does not exist
AttitudeProp_CCSDS_EulerAngle_OutputMRP:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_OutputMRP.report
does not exist
AttitudeProp_CCSDS_EulerAngle_OutputQuat:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_OutputQuat.report
does not exist
AttitudeProp_CCSDS_EulerAngle_ZeroInterpolationDegree:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle_ZeroInterpolationDegree.report
does not exist
AttitudeProp_CCSDS_EulerAngle:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_EulerAngle.report
does not exist
AttitudeProp_CCSDS_MixedAttitudeSegment:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_MixedAttitudeSegment.report
does not exist
AttitudeProp_CCSDS_Quaternion_FrameAndAttitudeDir:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_Quaternion_FrameAndAttitudeDir.report
does not exist
AttitudeProp_CCSDS_Quaternion_OutputDCM:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_Quaternion_OutputDCM.report
does not exist
AttitudeProp_CCSDS_Quaternion_OutputEuler:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_Quaternion_OutputEuler.report
does not exist
AttitudeProp_CCSDS_Quaternion_OutputMRP:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_Quaternion_OutputMRP.report
does not exist
AttitudeProp_CCSDS_Quaternion_QuatType_First:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_Quaternion_QuatType_First.report
does not exist
AttitudeProp_CCSDS_Quaternion:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_CCSDS_Quaternion.report
does not exist
AttitudeProp_EulerFile_DOYFormat_EndOfYearLeap:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_EulerFile_DOYFormat_EndOfYearLeap.report
does not exist
AttitudeProp_EulerFile_DOYFormat:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AttitudeProp_EulerFile_DOYFormat.report
does not exist
BatchEstimator_Propagator_SPK_EGAPMultiple_TDRS: [GMT-7050]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\BatchEstimator_Propagator_SPK_EGAPMultiple_TDRS.txt
does not exist
BatchEstimator_Propagator_STK_TDRS: [GMT-7289]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\BatchEstimator_Propagator_STK_TDRS.txt
does not exist
CCSDS_EdgeCornerStress_ChangeFileInCommand:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\CCSDS_EdgeCornerStress_ChangeFileInCommand.report
does not exist
CCSDS_EdgeCornerStress_InterpolateCloseToBeginningAndEnd:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\CCSDS_EdgeCornerStress_InterpolateCloseToBeginningAndEnd.report
does not exist
CCSDS_EdgeCornerStress_LargeFile:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\CCSDS_EdgeCornerStress_LargeFile.report
does not exist
EKFS_SpacecraftNavigation_LEO_TDRS_Aqua_FogmCd: [GMT-7376]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\EKFS_SpacecraftNavigation_LEO_TDRS_Aqua_FogmCd.txt
does not exist
JWST_SPAD_CCSDSAttitude_EarthSPAD:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\JWST_SPAD_CCSDSAttitude_EarthSPAD.report
does not exist
MatlabFunction_Custom_DegToRad_Assignment:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\MatlabFunction_Custom_DegToRad_Assignment.report
does not exist
MatlabFunction_Custom_magic:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\MatlabFunction_Custom_magic.report
does not exist
MatlabFunction_Custom:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\MatlabFunction_Custom.report
does not exist
Optimize_fmincon_ExitMode_DiscardAndContinue_2:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_ExitMode_DiscardAndContinue_2.report
does not exist
Optimize_fmincon_ExitMode_SaveAndContinue_2:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_ExitMode_SaveAndContinue_2.report
does not exist
Optimize_fmincon_ExitMode_Stop:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_ExitMode_Stop.report
does not exist
Optimize_fmincon_Minimize_Height_on_circle_2:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_Minimize_Height_on_circle_2.report
does not exist
Optimize_fmincon_Minimize_Height_on_circle:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_Minimize_Height_on_circle.report
does not exist
Optimize_fmincon_SolveMode_Defaultscript:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_SolveMode_Defaultscript.report
does not exist
Optimize_fmincon_SolveMode_Solve:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_SolveMode_Solve.report
does not exist
Plate_Prop_AreaCoefficient_AEM:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Plate_Prop_AreaCoefficient_AEM.txt
does not exist
Plate_SolveFors_AreaCoefficient_SN: [GMT-7376]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Plate_SolveFors_AreaCoefficient_SN.txt
does not exist
Plate_SolveFors_AreaCoefficient_UseAEM:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Plate_SolveFors_AreaCoefficient_UseAEM.txt
does not exist
Smoother_Filter_ProcessNoiseTimeStep_0sec_SN: [GMT-7376]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Smoother_Filter_ProcessNoiseTimeStep_0sec_SN.txt
does not exist
ThrustSegment_SolveFors_ThrustScaleFactor_SN: [GMT-7376]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\ThrustSegment_SolveFors_ThrustScaleFactor_SN.txt
does not exist
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2.report
does not exist
Vary_optimizer_fmincon_UpperBound_ArrayElement:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_UpperBound_ArrayElement.report
does not exist
Vary_optimizer_fmincon__InitialValue_RealNumber:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__InitialValue_RealNumber.report
does not exist
Vary_optimizer_fmincon__LowerBound_Array:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__LowerBound_Array.report
does not exist
Vary_optimizer_fmincon__LowerBound_Variable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__LowerBound_Variable.report
does not exist
scriptEvent_optimizer_fmincon__InitialValue_Variable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\scriptEvent_optimizer_fmincon__InitialValue_Variable.report
does not exist
Comparator errors:
CCSDS_EdgeCornerStress_ChangeModeInCommand: (truth)
ERROR MESSAGE: Comparator PercentDiffComparator failed: Error using
textscan
First input can not be empty. Expected a non-empty character vector or a
valid file-id.
CCSDS_EdgeCornerStress_ChangeModeInCommand: (reg)
ERROR MESSAGE: Array indices must be positive integers or logical
values.
EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_CCSDS: (truth)
[GMT-7483]
ERROR MESSAGE: Comparator STKEphemerisComparator failed: Output
argument "ephStruct" (and maybe others) not assigned during call to
"comparator.STKEphemerisComparator.Compare>read_stk_eph".
Truth failures:
API_PD45PropagationE8x8SMPM (API) [pos err 0.000753381, tol 1e-07]
BatchEstimator_NormalMatrixReduction_UseInitialCovariance [#1 failed]
[GMT-7274]
BatchEstimator_Propagator_Code500_TDRS [ptrn 1 failed] [GMT-7289]
BatchEstimator_Propagator_Multiple_SunEarthMoon [Residual failed at 10
Jun
2010 01:30:00.000] [GMT-7421]
BatchEstimator_Propagator_SPK_EndEarly_TDRS/BatchEstimator_Propagator_SPK_EndEarly_TDRS.log
[ptrn 1 failed] [GMT-7289]
BatchEstimator_Propagator_SPK_GN [#1 failed] [GMT-7289]
BatchEstimator_Propagator_SPK_HasGap_TDRS/BatchEstimator_Propagator_SPK_HasGap_TDRS.log
[ptrn 1 failed] [GMT-7289]
BatchEstimator_Propagator_SPK_StartLate_TDRS/BatchEstimator_Propagator_SPK_StartLate_TDRS.txt
[Parameter EstSat.EarthMJ2000Eq.X error 4688.570003 exceeds tolerance
0.005000] [GMT-7289]
BatchEstimator_Propagator_SPK_StartLate_TDRS/BatchEstimator_Propagator_SPK_StartLate_TDRS.txt
[#29 failed] [GMT-7289]
BatchEstimator_Propagator_SPK_StartLate_TDRS/BatchEstimator_Propagator_SPK_StartLate_TDRS.log
[ptrn 1 failed] [GMT-7289]
BatchEstimator_ReportStyle_Verbose_MultiSat_SpaceToSpace [#1143 failed]
[GMT-7421]
EKFS_EphemerisFile_STK_PredDv/EKFS_EphemerisFile_STK_PredDv_Filter.e
[Test
NumberOfCovariancePoints does not equal truth NumberOfCovariancePoints]
[GMT-7483]
EKFS_EphemerisFile_STK_PredDv/EKFS_EphemerisFile_STK_PredDv_Smoother.e
[Test NumberOfCovariancePoints does not equal truth
NumberOfCovariancePoints] [GMT-7483]
EKFS_EphemerisFile_STK_PredDv/EKFS_EphemerisFile_STK_PredDv_Filter.report
[Found 4466 output records and 4465 truth records] [GMT-7483]
EKFS_EphemerisFile_STK_PredDv/EKFS_EphemerisFile_STK_PredDv_Smooth.report
[Found 4466 output records and 4465 truth records] [GMT-7483]
EKFS_SpacecraftNavigation_GEO_Range_SDO_NPlateAreaCoefficient/EKFS_SpacecraftNavigation_GEO_Range_SDO_NPlateAreaCoefficient_Smoother.txt
[The test run failed to complete] [GMT-6801]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_Filter.e
[Test NumberOfCovariancePoints does not equal truth NumberOfCovariancePoints]
[GMT-7483]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_Smoother.e
[Test NumberOfCovariancePoints does not equal truth NumberOfCovariancePoints]
[GMT-7483]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_SmoEph/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_SmoEph_Smoother.e
[Test NumberOfCovariancePoints does not equal truth NumberOfCovariancePoints]
[GMT-7483]
EKFS_SpacecraftNavigation_Moon_DsnTcp_RangeRate_LRO_EarthInitialState_MoonFM/EKFS_SpacecraftNavigation_Moon_DsnTcp_RangeRate_LRO_EarthInitialState_MoonFM_Smoother.txt
[The test run failed to complete] [GMT-6801]
EKFS_SpacecraftNavigation_MultiSat_TdrsAndUser_DifferentProcessNoise [0
truth states are present but 12 tolerances were provided] [GMT-7421]
EKFS_SpacecraftNavigation_OrbitErrorCovariance_GN_Moon [Failed to find a
covariance record at 10 Sep 2005 00:00:00.000] [GMT-6801]
EKFS_SpacecraftNavigation_Sun_DSN_STEREOA_EarthInitialState_SunFM/EKFS_SpacecraftNavigation_Sun_DSN_STEREOA_EarthInitialState_SunFM_Smoother.txt
[The test run failed to complete] [GMT-6801]
EKFS_SpacecraftNavigation_Sun_DSN_STEREOA_SunInitialState_EarthFM/EKFS_SpacecraftNavigation_Sun_DSN_STEREOA_SunInitialState_EarthFM_Smoother.txt
[The test run failed to complete] [GMT-6801]
EKFS_ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_GpsPosVec/EKFS_ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_GpsPosVec_Smoother_backfilter.txt
[Parameter FM.Est_Thruster1_SetPoint1.ThrustAngle1.C0 error 14.750623 exceeds
tolerance 0.005000] [GMT-7483]
EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_CCSDS [#13 failed]
EphemStressTests_Default_Prop_CCSDS_Forward_and_BackwardDirect []
[GMT-6840]
GroundStation_Iono_Range_DeepSpace [Found 13688 output records and 13695
truth records] [GMD-7061]
KalmanFilter_InputWarmStartFile_SN [Output field -4638.173817 failed
tolerance in record 1] [GMT-7376]
KalmanFilter_MatlabFile_GN_Moon [Variable EstimationConfig.StateNames
did
not match at index 1] [GMT-6801]
KalmanFilter_Propagator_Multiple_MixedCentralBody [Observed measurement
failed at 10 Jun 2010 00:40:00.000] [GMT-7421]
KalmanFilter_Propagator_Multiple_SunEarthMoon [Observed measurement
failed
at 10 Jun 2010 00:00:00.000] [GMT-7421]
KalmanFilter_Propagator_SPK_TDRS [The test run failed to converge]
[GMT-7289]
KalmanFilter_Propagator_SPK_TDRS [ptrn 1,2 failed] [GMT-7289]
KalmanFilter_Smoother_PredictTimeSpan_Both_OEM/KalmanFilter_Smoother_PredictTimeSpan_Both_OEM_filter.oem
[#1 failed] [GMT-6949]
KalmanFilter_WarmStartEpoch_SN [Output field -4638.173817 failed
tolerance
in record 1] [GMT-7376]
MatAPI_Epoch_LeapSecond_In (MatAPI) [#7 failed] [2561]
MatAPI_Epoch_LeapSecond_Out (MatAPI) [#7 failed] [2561]
MatAPI_PD45PropagationE8x8SMPM (MatAPI) [pos err 0.000753381, tol
1e-07]
Matlab_NoInputsOutputs []
Matlab_NoOutputs []
Optimize_fmincon_CostFunction_and_ConvergedStatus_Display_2 [ptrn 1,2,3
failed]
Plate_Validation_PlateNormalHistoryFile [#1 failed] [GMT-7022]
RotationMatrixTest_MercuryMJ2000Ec [max diff 1.09735e-09 > tol 1e-12]
[GMT-7223]
Simulator_Propagator_SPK_GN [Residual failed at 01 Mar 2005
01:00:00.000]
[GMT-7289]
Simulator_Propagator_SPK_MoonOccultation [#66 failed] [GMT-7289]
Simulator_Propagator_SPK_MultipleOccultation [#1 failed] [GMT-7289]
Simulator_Propagator_SPK_TDRS [Residual failed at 01 Mar 2005
01:00:00.000] [GMT-7289]
Smoother_Filter_RandomConstCd_GpsPosVec [Parameter EstSat.Cd error
0.001223 exceeds tolerance 0.001000]
Smoother_MatlabFile_BackfilterMatfileCorruption [Found extra field
BackwardComputed] [GMT-6949]
Smoother_PredictTimeSpan_STK_SN [Unable to read STK ephemeris
C:\Users\gsfc580gmattest\Documents\ScriptTest\output\2021-08-19\Resources\FRR-70_Smoother\script\Smoother_PredictTimeSpan_STK_SN_Smoother.e]
[GMT-7376]
Spacecraft_Validation_AddPlates [#1 failed] [GMT-7022]
SpacecraftNavigation_L1_DsnSeqRange_SOHO_PassBiases [The test run failed
to converge] [GMT-7565]
SpacecraftNavigation_Moon_DsnTcp_RangeRate_LRO_EarthInitialState_MoonFM_KeplerianState
[The test run failed to converge] [GMT-7515]
SpacecraftNavigation_MultiSat_DifferentInitialEpochs [#1 failed]
SpacecraftNavigation_MultiSat_SpaceToSpace_SharedBias_Angles [The test
run
failed to converge] [GMT-7421]
SpacecraftNavigation_TDRS_SecondGen_MA2_Landsat7 [Residual failed at 28
Aug 2015 19:41:22.000] [GMT-7376]
SpacecraftNavigation_TDRS_SecondGen_MA4_Landsat7 [Failed to find a
SN_Range residual record at 28 Aug 2015 19:41:12.000] [GMT-7376]
ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_EpochAfterBurn_GpsPosVec
[The test run failed to converge] [GMT-7483]
ThrustSegment_SolveFors_ThrustAngles_Constant_ThreeAxisKinematic_EpochAfterBurn_GpsPosVec
[The test run failed to converge] [GMT-7483]
TrackingFileSet_AddTrackingConfig_DsnSeqRange [#1 failed] [GMR-7061]
TrackingFileSet_AddTrackingConfig_DsnTcp [#1 failed] [GMR-7061]
TrackingFileSet_AddTrackingConfig_Range [#1 failed] [GMR-7061]
TrackingFileSet_AddTrackingConfig_RangeRate [#1 failed] [GMR-7061]
TrackingFileSet_FileName2 [#2 failed] [GMR-7061]
TrackingFileSet_Validation_TimeGapForPassBreak [#2 failed] [GMT-7565]
Transponder_HardwareDelay_Sim_Range [GMAT: 617 lines, Truth: 619 lines]
[GMR-7061]
Transponder_HardwareDelay_Sim_Range_RangeSkin [GMAT: 65 lines, Truth: 66
lines] [GMR-7061]
Transponder_HardwareDelay_Sim_RangeSkin [GMAT: 65 lines, Truth: 66
lines]
[GMR-7061]
Tut_MultipleShootingTutorial_Step3 [] [GMT-7280]
Vary_optimizer_fmincon__AdditiveScaleFactor_Variable [ptrn 1,2 failed]
Vary_optimizer_fmincon_AdditiveScaleFactor_RealNumber [ptrn 1,2 failed]
Vary_optimizer_fmincon_MultiplicativeScaleFactor_RealNumber [ptrn 1,2
failed]
-----------------------------------------------------------------
New Issues (Deferred)
-----------------------------------------------------------------
New truth failures (deferred):
None
Output changes (but still pass) (deferred):
None
Output changes (but still fail) (deferred):
Ephem_GMAT_Code500_InterpolationOrder [pos err 0.0173914, tol 0.002]
[GMT-4075, GMT-4112]
Ephem_GMAT_Code500_InterpolationOrder [pos err 0.0463976, tol 0.002]
[GMT-4075, GMT-4112]
EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection
[pos err 15.2508, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection
[pos err 9.57601, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect
[pos err 14.3834, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
[pos err 0.000217107, tol 1e-12] [GMT-4112]
EphemStressTests_PD78_ABM_Prop_Code500_60Sec_Step_ForwardDirection [pos
err 21.5632, tol 1e-12] [GMT-4112]
New crashes/hangs/etc. (deferred):
None
New script errors (deferred):
None
New comparator errors (deferred):
None
-----------------------------------------------------------------
Fixed Issues (Deferred)
-----------------------------------------------------------------
Fixed truth failures (deferred):
None
Fixed crashes/hangs/etc. (deferred):
None
Fixed script errors (deferred):
None
Fixed comparator errors (deferred):
None
-----------------------------------------------------------------
All Known Issues (Deferred)
-----------------------------------------------------------------
Crashes/hangs/etc. (deferred):
GMAT_LunarTransfer_AllPlanets_DE421_BS
GMAT_MarsTransfer_4_BS
Script errors (deferred):
BatchEstimator_EstimationEpoch [GMT-5708]
EKF_SpacecraftNavigation_OrbitErrorCovariance_Keplerian_GpsPosVec
EKF_SpacecraftNavigation_SolveFors_KeplerianState_Cd_RandomConstant_GN
EKF_SpacecraftNavigation_SolveFors_KeplerianState_Cr_RandomConstant_DSN
EKF_SpacecraftNavigation_SolveFors_KeplerianState_GN
EKF_SpacecraftNavigation_SolveFors_KeplerianState_GpsPosVec
KalmanFilter_InputWarmStartFile_GN_Moon_Keplerian [GMT-6801]
KalmanFilter_InputWarmStartFile_GpsPosVec_KeplerianToCartesian
[GMT-6801]
KalmanFilter_OutputWarmStartFile_GpsPosVec_Keplerian [GMT-6801]
Math_Shadowed_Builtins [GMT-3043]
OCPropTest_SPAD_Drag_1deg_Bicubic_LEO [GMT-7147]
OCPropTest_SPAD_Drag_SRP_1deg_Bicubic_LEO [GMT-7147]
Python_IO_String [5317]
ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522]
THF_Sim_Accel_ConfigD_None_NA_2 [GMT-6451]
THF_Sim_Accel_ConfigD_None_NA_3 [GMT-6451]
THF_Sim_Accel_ConfigD_None_NA_4 [GMT-6451]
THF_Sim_Accel_ConfigD_None_NA [GMT-6451]
THF_Sim_Thrust_CSF2_None_NA_ZeroTSF [GMT-6451]
ThrustHistoryFile_EstimateTSF_EpochBeforeBurn_RSSStep_Aqua [GMT-6451]
ThrustSegment_SolveFors_ThrustScaleFactor_Multiple_RSSStep [GMT-6451]
ThrustSegment_SolveFors_ThrustScaleFactor_RSSStep [GMT-6451]
TrkFile_SimEst_DSN_DS_Range_Solve_Bias_apriori [GMT-5709]
Comparator errors (deferred):
GroundStation_Iono_Range_Kband (truth) [GMT-5644]
GroundStation_Iono_RangeRate_Kband (truth) [GMT-5644]
GroundStation_TropoIono_Range_Kband (truth) [GMT-5644]
Truth failures (deferred):
AcceptFilter_Validation_RecordNumbers [#5 failed] [GMT-6034]
Achieve_Validation_LHS_Field [ptrn 1 failed] [GMT-3687]
Achieve_Validation_RHS_Field [no error or exception] [GMT-3687]
BatchEstimator_ReportFile_InitialState [#1 failed]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond_Filter.e
[EphemerisTimePosVel failed epoch tolerance at row 988] [GMT-7291, GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond_Smoother.e
[EphemerisTimePosVel failed epoch tolerance at row 988] [GMT-7291, GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond_Filter.mat
[Found extra field CartesianStateNames] [GMT-7291, GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond_Smoother.mat
[Found extra field CartesianStateNames] [GMT-7291, GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond.tab
[Output field 0.001068 failed tolerance in record 979] [GMT-7291, GMT-7398]
Ephem_GMAT_Code500_InterpolationOrder/Ephem_GMAT_Code500_InterpolationOrder_1.eph
[pos err 0.0173914, tol 0.002] [GMT-4075, GMT-4112]
Ephem_GMAT_Code500_InterpolationOrder/Ephem_GMAT_Code500_InterpolationOrder_3.eph
[pos err 0.0463976, tol 0.002] [GMT-4075, GMT-4112]
Ephem_GMAT_Code500_StepSize/Ephem_GMAT_Code500_StepSize_1.eph [pos err
305.165, tol 0.002] [GMT-4112]
EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection
[pos err 15.2508, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection
[pos err 9.57601, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect
[pos err 14.3834, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
[pos err 0.000217107, tol 1e-12] [GMT-4112]
EphemStressTests_PD78_ABM_Prop_Code500_60Sec_Step_ForwardDirection [pos
err 21.5632, tol 1e-12] [GMT-4112]
EphemStressTests_SPK_Integrator_Code500_60Sec_ForwardDirection [pos err
0.000427977, tol 1e-12] [GMT-4112]
Epoch_LeapSecond_G2MJD [max mjd diff 1.000259s > tol 0.001000s] [2561]
Epoch_LeapSecond_In [max greg. diff 1.000005s > tol 0.001000s] [2561]
Epoch_LeapSecond_Out [max mjd diff 1.000146s > tol 0.001000s] [2561]
Formation_Validation_MissingComma [no error or exception] [GMT-3672]
GMAT_ISS_Earth_JGM2_0_0_NutationUpdateInterval [pos err 0.00081496, tol
1e-06] [GMT-2567]
GMAT_LEO_PropSynchronization_BS []
GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS [pos err 0.0756285, tol 0.002]
GroundStation_Tropo_TRK223_DsnTcp_OREX/GroundStation_Tropo_TRK223_DsnTcp_OREX.txt
[Residual failed at 02 Feb 2021 09:25:00.000] [GMT-7455]
Math_Inf [GMAT: 53 lines, Truth: 69 lines] [GMT-3195]
Minimize_Validation_Field [no warn or err] [GMT-3687]
Nonlinear_Validation_LHS_Field [no warn or err] [GMT-3687]
Nonlinear_Validation_RHS_Field [ptrn 1 failed] [GMT-3687]
Optimize_Yukon_Minimize_Height_on_circle_2 [diff 497, tol 0.001]
Optimize_Yukon_Minimize_Height_on_circle_4 [diff 497, tol 0.001]
RejectFilter_Validation_RecordNumbers [#5 failed] [GMT-6034]
ScriptLanguage_Comments_AfterControlFlow [] [GMT-3332]
ScriptLanguage_LiteralArrays_String [] [GMT-3680]
ScriptLanguage_ReferenceArrays_ForceModel_7 [] [GMT-3541]
ScriptLanguage_Validation_Semicolons_1 [no error or exception]
[GMT-3545]
SpacecraftNavigation_Validation_Mode [#1 failed] [GMT-5841]
String_AssignNumericParam [] [GMT-2888]
ThrustSegment_ThrustAngle1_Cubic [diff. num. lines] [GMT-7483]
TrackingFileSet_InconsistentSpacecraftState [Output field
-1254560.770370
failed tolerance in record 1] [GMT-7553]
TrkFile_SimEst_TDRS_range_Solve_Cr [] [GMT-5416]
Vary_Validation_RHS_Field [no error or exception] [GMT-3687]
Write_Multiple_ReportFile_Concise_2 [#24 failed] [GMT-5801]
Write_Multiple_ReportFile_Verbose [#24 failed]
Write_Multiple_ReportFile_Verbose_2 [#24 failed] [GMT-5801]
-----------------------------------------------------------------
Test System Warnings
-----------------------------------------------------------------
Passing tests tagged with bugs:
(To fix, remove bug ID from Bugs key in .tc file)
Comet_Validation_OrientationEpoch_3 [GMT-3252]
CoordSysTest_Luna_MJ2000Eq_To_ICRF [GMT-3227]
CoordinateSystem_Validation_Axes_4 [GMT-3155]
EKFS_EphemerisFile_STK_IncludeCovariance_None_Moon [GMT-7398]
EKFS_EphemerisFile_STK_IncludeCovariance_None_Sun [GMT-7398]
EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Moon
[GMT-7398]
EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Sun
[GMT-7398]
EKFS_EphemerisFile_STK_IncludeCovariance_Position_Moon [GMT-7398]
EKFS_EphemerisFile_STK_IncludeCovariance_Position_Sun [GMT-7398]
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_GN [GMT-7434-Linux]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_ColdStart
[GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_EarthFixed
[GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart
[GMT-7398]
EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr [GMT-7278-Linux]
EphemPropagator_Code500_CentralBody_Jupiter [GMT-5795]
EphemPropagator_Code500_CentralBody_Saturn [GMT-5795]
EphemPropagator_Code500_ForwardProp_Interp [GMT-5760]
EphemPropagator_SatAssigmentToNewSatThenProp [GMT-3434]
EphemStressTests_Default_Prop_STK_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection
[GMT-6090]
EphemStressTests_Default_Prop_STK_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect
[GMT-6090]
Ephem_GMAT_SPK_60sec_backward [GMT-5286]
Ephem_GMAT_SPK_DefaultIntegrationStep_User_Defined_LagrangeOrder
[GMT-5286]
Ephem_GMAT_STK_60sec_IterativeProcess_Optimizer [GMT-6090]
Ephem_GMAT_STK_60sec_IterativeProcess_Optimizer_NoBoundaries [GMT-6090]
Events_ContactLocator_Ephemeris_DE405AllPlanets [GMT-5377]
Events_ContactLocator_Ephemeris_DE424AllPlanets [GMT-5377]
Events_ContactLocator_Heo2 [GMT-5302]
Events_ContactLocator_UseEntireInterval_False_MissionSequence [GMT-5292]
Ex_GmatFunction [GMT-3604]
FMParams_GMAT_UserAsteroid(OSIRIS)_HarmonicGravity_SRP_PointMasses
[GMT-6955]
ForceModel_SPAD_Drag_1deg_Bicubic_Mars [Linux, Mac]
ForceModel_SPAD_Drag_1deg_Bilinear_Mars [Linux, Mac]
Formation_Validation_PropFormSatInTwoProps [GMT-3581]
GMAT_GEO_EarthSunMoon_0_0_0_Relativity [3405]
GMAT_GEO_EarthSun_0_0_0_Relativity [3405]
GMAT_ISS_EarthSunMoon_0_0_0_Relativity [3405]
GMAT_ISS_EarthSunMoon_0_0_0_Relativity_Cmd [3405]
GMAT_ISS_EarthSun_0_0_0_Relativity [3405]
IntegratedFlyby_MarsFlyby [GMT-7169]
KalmanFilter_TimeUpdate_GpsPosVec [GMT-6801]
Math_Validation_Cross_WrongDim2 [GMT-5676]
Phase_EpochFormat_TAIGregorian [GMT-7168]
Phase_Type_Radau [GMT-7168]
Plate_Type_File [GMT-7022]
Plate_Type_File_CoordinateSystem_EarthMJ2000Ec [GMT-7022]
Plate_Type_File_CoordinateSystem_FixedInBody [GMT-7022]
Plate_Type_File_StartEpoch [GMT-7022]
ScriptLanguage_LineContinuation_BeginningOfLine [GMT-3756]
ScriptLanguage_Validation_DataTypes_ReferenceArray_Formation_5
[GMT-6064]
Simulator_Propagator_EarthPointMass_Drag [GMT-5417]
Simulator_Propagator_EarthPointMass_SRP_Drag [GMT-5417]
SpacePointParams_CelestialBody_EpochOutput [3939]
SpacecraftNavigation_CdSigma_Range_MSISE86 [GMT-6829 Linux only]
SpacecraftNavigation_SPADDragScaleFactorSigma_ConstrainInc [GMT-7078,
Ubuntu only]
SpacecraftNavigation_SPADDragScaleFactorSigma_GN_MSISE86 [GMT-6829 Linux
only]
SpacecraftNavigation_SPADSRPScaleFactorSigma_ConstrainInc [GMT-7078,
Linux
only]
SpacecraftNavigation_SolveFors_CartesianState_SPADDragScaleFactor_GN_MSISE86
[GMT-6829 Linux only]
ThrustSegment_SolveFors_ThrustAngles_ThrustScaleFactor_Cr_DSN_Keplerian
[GMT-7483]
Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
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