-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Windows 10/MATLAB R2017a/VS 2013
Tested build: 2021-09-13
Regression build: 2021-09-10
Total number of scripts: 15869 (+98 deferred)
Percent Passed: 99.23%
New issues: 9
Output changes: 3
New truth failures: 0
New crashes: 0
New script errors: 6
New comparator errors: 0
Fixed issues: 276
Total issues: 126
Test system warnings: 47
New deferred issues: 9
Fixed deferred issues: 1
Total deferred issues: 75
Run Time: 00 hours, 24 minutes, 32 seconds
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
None
Output changes (but still pass):
BatchEstimator_Propagator_SPK_GN
KalmanFilter_Propagator_SPK_TDRS
RunEstimator_SolveMode_RunInitialGuess
Output changes (but still fail):
None
New crashes/hangs/etc.:
None
New script errors:
MatlabFunction_Custom_DegToRad_Assignment
MatlabFunction_Custom_DegToRad
MatlabFunction_Custom
Optimize_fmincon_ExitMode_SaveAndContinue_3
Optimize_fmincon_cvg_status
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2
New comparator errors:
None
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
BatchEstimator_AbsoluteTol_GpsPosVec
BatchEstimator_MaxConsecutiveDivergences_GpsPosVec
BatchEstimator_MaximumIterations_GpsPosVec
EKF_EphemerisFile_STK_IncludeEventBoundaries_False
EKF_ErrorModel_NoiseSigma_GpsPosVec
EKF_SpacecraftNavigation_OrbitErrorCovariance_NonPosDef_GpsPosVec
EKF_TrackingFileSet_AddTrackingConfig_All
EKF_TrackingFileSet_FileName3_GpsPosVec
ErrorModel_NoiseSigma_GpsPosVec
ErrorModel_NoiseSigma_GpsPosVec2
EstimatedParameter_DisallowForBLS
EstimatedParameter_FOGM_AtmosDensityScaleFactor_HalfLife_3600sec
EstimatedParameter_FOGM_Cd_HalfLife_3600sec
KalmanFilter_AddPredictToMatlabFile_ADSF_GpsPosVec
KalmanFilter_AddPredictToMatlabFile_Cd_Cr_GpsPosVec
KalmanFilter_AddPredictToMatlabFile_GpsPosVec
KalmanFilter_InputWarmStartFile_GpsPosVec_Keplerian
KalmanFilter_InputWarmStartFile_NoMeasurementsToProcess
KalmanFilter_MatlabFile_GpsPosVec
KalmanFilter_MeasDeweightingSigmaThreshold_FogmCd_FogmADSF_GpsPosVec
KalmanFilter_MeasurementUpdate_GpsPosVec
KalmanFilter_PredictTimeSpan_2days
KalmanFilter_PredictTimeSpan_STK
KalmanFilter_TimeUpdate_GpsPosVec [GMT-6801]
KalmanFilter_WarmStartEpoch_TooEarly
KalmanFilter_WarmStartEpoch_TooLate
Matlab_NoInputsOutputs
ProcessNoiseModel_AccelNoiseSigma_GpsPosVec
ProcessNoiseModel_Type_StateNoiseCompensation
Smoother_MeasDeweightingSigmaThreshold_FogmCd_FogmADSF_GpsPosVec
Smoother_RunEstimator_Command_Error
SpacecraftNavigation_SolveFors_CartesianState_Cd_ADSF_GpsPosVec
StopCond_GMAT_MoonPM_FirstStepAlgorithm_MultiProps
TrkFile_Est_DSN_DS_Range
Fixed crashes/hangs/etc.:
None
Fixed script errors:
AcceptFilter_DataTypes_GpsPosVec
AcceptFilter_Level2_DataTypes_GpsPosVec
AcceptFilter_ThinningTime_300_GpsPosVec
AcceptFilter_TimeSpanThinningTime_GpsPosVec
BatchEstimator_ILSEMaximumIterations_GpsPosVec
BatchEstimator_ILSEMultiplicativeConstant_GpsPosVec
BatchEstimator_InversionAlgorithm_Cholesky_GpsPosVec
BatchEstimator_InversionAlgorithm_Internal_GpsPosVec
BatchEstimator_InversionAlgorithm_Schur_GpsPosVec
BatchEstimator_MatlabFile_GpsPosVec
BatchEstimator_MatlabFile_ThrustAngles
BatchEstimator_OLSEAdditiveConstant_GpsPosVec
BatchEstimator_OLSEInitialRMSSigma_GpsPosVec
BatchEstimator_OLSEMultiplicativeConstant_GpsPosVec
BatchEstimator_OLSEUseRMSP_False_GpsPosVec
BatchEstimator_RelativeTol_GpsPosVec
BatchEstimator_ReportFile_GpsPosVec_Editing
BatchEstimator_ReportFile_GpsPosVec
BatchEstimator_ReportFile_MeasurementStatistics_UserEdit_TimeSpan_GpsPosVec
BatchEstimator_UseInnerLoopEditing_GpsPosVec
EKFS_EphemerisFile_STK_PredDv [GMT-7483]
EKFS_Plate_AreaCoefficientSigma_GpsPosVec
EKFS_Plate_DiffuseFractionSigma_GpsPosVec
EKFS_Plate_SolveFors_AreaCoefficient_GpsPosVec_GOES17
EKFS_Plate_SolveFors_AreaCoefficient_Multiple
EKFS_Plate_SpecularFractionSigma_GpsPosVec
EKFS_SpacecraftNavigation_AtmosDensityScaleFactorSigma_RandomConstant_GpsPosVec
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_LargeMeasurementGap
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_SmoEph
[GMT-7483]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv
[GMT-7483]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart
[GMT-7398]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_ADSF_RandomConstant_GpsPosVec
EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_FOGM_GpsPosVec
EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_RandomConstant_GpsPosVec
EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cr_RandomConstant_GpsPosVec
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCdConstr_FogmADSF_GpsPosVec
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSFConstr_GpsPosVec
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_GpsPosVec
EKFS_SpacecraftNavigation_SolveFors_CartesianState_GpsPosVec
EKFS_SpacecraftNavigation_SolveFors_CartesianState_RandomConstCdConstr_RandomConstADSF_GpsPosVec
EKFS_SpacecraftNavigation_SolveFors_CartesianState_RandomConstCd_RandomConstADSFConstr_GpsPosVec
EKFS_ThrustSegment_SolveFors_ThrustAngle1_Constant_GpsPosVec
EKFS_ThrustSegment_SolveFors_ThrustAngle1_Linear_GpsPosVec
EKFS_ThrustSegment_SolveFors_ThrustAngle1_Quadratic_GpsPosVec
EKFS_ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_GpsPosVec
[GMT-7483]
EKFS_ThrustSegment_SolveFors_ThrustAngles_ThrustScaleFactor_Cr_GpsPosVec
EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_Long_LowThrust
EKFS_ThrustSegment_ThrustScaleFactorSigma_GpsPosVec
EKF_AcceptFilter_DataTypes_GpsPosVec
EKF_AcceptFilter_Level2_DataTypes_GpsPosVec
EKF_AcceptFilter_Level2_EpochFormat_TAIModJulian
EKF_AcceptFilter_Level2_FinalEpoch_GpsPosVec
EKF_AcceptFilter_Level2_InitialEpoch_GpsPosVec
EKF_AcceptFilter_Level2_RecordNumbers_GpsPosVec
EKF_AcceptFilter_Level2_TimeSpan_GpsPosVec
EKF_AcceptFilter_Level2_TimeSpan_RecordNumbers_GpsPosVec
EKF_AcceptFilter_ThinningFrequency_10_GpsPosVec
EKF_AcceptFilter_ThinningTime_300_GpsPosVec
EKF_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_GpsPosVec
EKF_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Meters_GpsPosVec
EKF_EphemerisFile_STK_IncludeCovariance_Position_GpsPosVec
EKF_EphemerisFile_STK_IncludeCovariance_Position_Meters_GpsPosVec
EKF_ErrorModel_Type_GpsPosVec
EKF_RejectFilter_Level2_DataTypes_GpsPosVec
EKF_RejectFilter_Level2_EpochFormat_TAIModJulian
EKF_RejectFilter_Level2_FinalEpoch_GpsPosVec
EKF_RejectFilter_Level2_InitialEpoch_GpsPosVec
EKF_RejectFilter_Level2_Multiple_GpsPosVec
EKF_RejectFilter_Level2_RecordNumbers_GpsPosVec
EKF_RejectFilter_Level2_TimeSpan_GpsPosVec
EKF_RejectFilter_Level2_TimeSpan_RecordNumbers_GpsPosVec
EKF_RunEstimator_GpsPosVec
EKF_RunEstimator_SolveMode_RunInitialGuess
EKF_SpacecraftNavigation_CdSigma_RandomConstant_GpsPosVec
EKF_SpacecraftNavigation_CrSigma_RandomConstant_GpsPosVec
EKF_SpacecraftNavigation_LEO_GpsPosVec_Fermi_Drag_RandomConstant
EKF_SpacecraftNavigation_OrbitErrorCovariance_GpsPosVec
EKF_SpacecraftNavigation_ProcessNoiseModel_GpsPosVec
EKF_SpacecraftNavigation_SolveFors_CartesianState_Drag_Negative_GpsPosVec
ErrorModel_Bias_GpsPosVec2
ErrorModel_Type_GpsPosVec
EstimatedParameter_FOGM_AtmosDensityScaleFactor_SteadyStateSigma
EstimatedParameter_FOGM_AtmosDensityScaleFactor_SteadyStateValue
EstimatedParameter_FOGM_AtmosDensityScaleFactor_TimeUpdateInitial
EstimatedParameter_FOGM_Cd_SteadyStateSigma
EstimatedParameter_FOGM_Cd_SteadyStateValue
EstimatedParameter_FOGM_Cd_TimeUpdateInitial
EstimatedParameter_FOGM_LeapSecond_MeasurementUpdate
EstimatedParameter_FOGM_LeapSecond_TimeUpdate
EstimatedParameter_FOGM_SolveFor_AtmosDensityScaleFactor
EstimatedParameter_FOGM_SolveFor_Cd_AtmosDensityScaleFactor
EstimatedParameter_FOGM_SolveFor_Cd
KalmanFilter_DataFilters_GpsPosVec
KalmanFilter_DelayRectifyTimeSpan_SuppressWarmStartRecords
KalmanFilter_InputWarmStartFile_GpsPosVec_ADSF
KalmanFilter_InputWarmStartFile_GpsPosVec_AddCd
KalmanFilter_InputWarmStartFile_GpsPosVec_AddFogmCd
KalmanFilter_InputWarmStartFile_GpsPosVec_Cd
KalmanFilter_InputWarmStartFile_GpsPosVec_DropCd
KalmanFilter_InputWarmStartFile_GpsPosVec_EarthFixed
KalmanFilter_InputWarmStartFile_GpsPosVec_FogmADSF_ChangeHalfLife
KalmanFilter_InputWarmStartFile_GpsPosVec_FogmADSF_ChangeSigma
KalmanFilter_InputWarmStartFile_GpsPosVec_FogmADSF_ChangeValue
KalmanFilter_InputWarmStartFile_GpsPosVec_FogmADSF
KalmanFilter_InputWarmStartFile_GpsPosVec_FogmCd_ChangeHalfLife
KalmanFilter_InputWarmStartFile_GpsPosVec_FogmCd_ChangeSigma
KalmanFilter_InputWarmStartFile_GpsPosVec_FogmCd_ChangeValue
KalmanFilter_InputWarmStartFile_GpsPosVec_FogmCd_FogmADSF
KalmanFilter_InputWarmStartFile_GpsPosVec_FogmCd
KalmanFilter_InputWarmStartFile_GpsPosVec_NPlateSRP_AreaCoefficient_Multiple
KalmanFilter_InputWarmStartFile_GpsPosVec_NPlateSRP_EquateAreaCoefficients
KalmanFilter_InputWarmStartFile_GpsPosVec_ThrustScaleFactor
KalmanFilter_InputWarmStartFile_GpsPosVec
KalmanFilter_InputWarmStartFile_ThrustAngles_ThrustScaleFactor_GpsPosVec
KalmanFilter_LeapSecond_GpsPosVec
KalmanFilter_MeasDeweightingCoefficient_FogmCd_FogmADSF_GpsPosVec
KalmanFilter_MeasDeweightingCoefficient_GpsPosVec
KalmanFilter_Measurements_GpsPosVec
KalmanFilter_OutputWarmStartFile_GpsPosVec_Cd
KalmanFilter_OutputWarmStartFile_GpsPosVec_FogmCd_FogmADSF
KalmanFilter_OutputWarmStartFile_GpsPosVec_FogmCd_RandomConstantADSF
KalmanFilter_OutputWarmStartFile_GpsPosVec_FogmCd
KalmanFilter_OutputWarmStartFile_GpsPosVec
KalmanFilter_PredictUsingEndState_GpsPosVec
KalmanFilter_ProcessNoiseTimeStep_0sec_Backfilter
KalmanFilter_ProcessNoiseTimeStep_0sec
KalmanFilter_Propagator_EarthFullModeling_GpsPosVec
KalmanFilter_ReportFile_DuringEstimation_AllSolverIterations
KalmanFilter_ReportFile_DuringEstimation_OrbitErrorCovariance
KalmanFilter_ReportFile_DuringEstimation
KalmanFilter_ReportFile_GpsPosVec
KalmanFilter_ReportStyle_Verbose
KalmanFilter_ScaledResidualThreshold_GpsPosVec
KalmanFilter_Smoother_PredictTimeSpan_Both_OEM [GMT-6949]
KalmanFilter_StartAfterFirstMeasurement_GpsPosVec
KalmanFilter_TimeUpdate_GpsPosVec_FogmCd_FogmADSF
KalmanFilter_WarmStartEpochFormat_TAIModJulian
KalmanFilter_WarmStartEpoch_Default
KalmanFilter_WarmStartEpoch_FirstMeasurement
KalmanFilter_WarmStartEpoch_LastWarmStartRecord
KalmanFilter_WarmStartEpoch
MatlabFunction_Custom_magic
Optimize_fmincon_ExitMode_Stop
Plate_SolveFors_AreaCoefficient_GpsPosVec_GOES17
ProcessNoiseModel_AccelNoiseSigma_FOGM_Cd_ADSF_GpsPosVec
ProcessNoiseModel_AccelNoiseSigma_GpsPosVec_BackFilter
ProcessNoiseModel_CoordinateSystem_EarthVNB_GpsPosVec_BackFilter
ProcessNoiseModel_CoordinateSystem_EarthVNB_GpsPosVec
RejectFilter_DataTypes_GpsPosVec
RejectFilter_Level2_DataTypes_GpsPosVec
RejectFilter_Level2_TimeSpan_Inclusive_GpsPosVec
RejectFilter_TimeSpan_Inclusive_GpsPosVec
RunSmoother_GpsPosVec
Smoother_AddPredictToMatlabFile_ADSF_GpsPosVec
Smoother_AddPredictToMatlabFile_Cd_Cr_GpsPosVec
Smoother_AddPredictToMatlabFile_GpsPosVec
Smoother_CheckMeasurementEditing
Smoother_Filter_EndStatesMatch_GpsPosVec
Smoother_Filter_EphemerisPredictionsMatch_GpsPosVec
Smoother_Filter_FogmCd_FogmADSF_GpsPosVec
Smoother_Filter_FogmCd_GpsPosVec
Smoother_Filter_GpsPosVec_EarthFixed
Smoother_Filter_GpsPosVec
Smoother_Filter_MeasDeweighting_FogmCd_FogmADSF_GpsPosVec
Smoother_Filter_RandomConstCd_GpsPosVec
Smoother_Filter_SPADDrag_GpsPosVec
Smoother_MatlabFile_FogmCd_FogmADSF_GpsPosVec
Smoother_MeasDeweightingCoefficient_Cd_ADSF_GpsPosVec
Smoother_MeasDeweightingCoefficient_FogmCd_FogmADSF_GpsPosVec
Smoother_MeasurementUpdate_GpsPosVec
Smoother_PredictTimeSpan_STK
Smoother_ReportFile_DuringEstimation_AllSolverIterations
Smoother_ReportFile_DuringEstimation_OrbitErrorCovariance
Smoother_ReportFile_FogmCd_FogmADSF_GpsPosVec
Smoother_ReportStyle_Normal
Smoother_ReportStyle_Verbose
Smoother_TimeUpdate_GpsPosVec
SpacecraftNavigation_AtmosDensityScaleFactorSigma_GpsPosVec
SpacecraftNavigation_CdSigma_GpsPosVec
SpacecraftNavigation_CrSigma_GpsPosVec
SpacecraftNavigation_LEO_GpsPosVec_Fermi_EstimatedState
SpacecraftNavigation_OrbitErrorCovariance_GpsPosVec
SpacecraftNavigation_OrbitErrorCovariance_Keplerian_GpsPosVec
SpacecraftNavigation_SPADDragScaleFactorSigma_GpsPosVec
SpacecraftNavigation_SPADDragScaleFactorSigma_SPADSRPScaleFactorSigma_GpsPosVec
SpacecraftNavigation_SPADSRPScaleFactorSigma_GpsPosVec
SpacecraftNavigation_SolveFors_CartesianState_ADSF_GpsPosVec
SpacecraftNavigation_SolveFors_CartesianState_Cd_Cr_GpsPosVec
SpacecraftNavigation_SolveFors_CartesianState_Cd_GpsPosVec
SpacecraftNavigation_SolveFors_CartesianState_Cr_GpsPosVec
SpacecraftNavigation_SolveFors_CartesianState_GpsPosVec
SpacecraftNavigation_SolveFors_CartesianState_LeapSec_GpsPosVec
SpacecraftNavigation_SolveFors_CartesianState_SPADDragScaleFactor_GpsPosVec
SpacecraftNavigation_SolveFors_CartesianState_SPADSRPScaleFactor_GpsPosVec
SpacecraftNavigation_SolveFors_KeplerianState_Cd_Cr_GpsPosVec
SpacecraftNavigation_SolveFors_KeplerianState_Cd_GpsPosVec
SpacecraftNavigation_SolveFors_KeplerianState_Cr_GpsPosVec
SpacecraftNavigation_SolveFors_KeplerianState_GpsPosVec
SpacecraftNavigation_SolveFors_KeplerianState_LeapSec_GpsPosVec
SpacecraftNavigation_SolveFors_KeplerianState_SPADDragScaleFactor_GpsPosVec
SpacecraftNavigation_SolveFors_KeplerianState_SPADSRPScaleFactor_GpsPosVec
ThrustSegment_SolveFors_ThrustAngle1_Constant_GpsPosVec
ThrustSegment_SolveFors_ThrustAngle1_Linear_GpsPosVec
ThrustSegment_SolveFors_ThrustAngle1_Quadratic_GpsPosVec
ThrustSegment_SolveFors_ThrustAngle2_Constant_GpsPosVec
ThrustSegment_SolveFors_ThrustAngle2_Linear_GpsPosVec
ThrustSegment_SolveFors_ThrustAngle2_Quadratic_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_ConstantLinear_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_Constant_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_EpochAfterBurn_GpsPosVec
[GMT-7483]
ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_Constant_ThreeAxisKinematic_EpochAfterBurn_GpsPosVec
[GMT-7483]
ThrustSegment_SolveFors_ThrustAngles_Constant_ThrustMass_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_Constant_ThrustMass_Interpolate_Linear_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_Constant_ThrustMass_Interpolate_None_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_Constant_Thrust_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_EpochAfterBurn_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_EpochDuringBurn_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_GOES17
ThrustSegment_SolveFors_ThrustAngles_Linear_CoordinateSystemFixed_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_Linear_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_Linear_ThreeAxisKinematic_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_Quadratic_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_ThrustScaleFactor_Cr_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_ThrustScaleFactor_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_ThrustScaleFactor_LongLowThrust
ThrustSegment_ThrustAngle1Sigma_Constant
ThrustSegment_ThrustAngle1Sigma_Cubic
ThrustSegment_ThrustAngle1Sigma_Linear
ThrustSegment_ThrustAngle1Sigma_Quadratic
ThrustSegment_ThrustAngle2Sigma_Constant
ThrustSegment_ThrustAngle2Sigma_Cubic
ThrustSegment_ThrustAngle2Sigma_Linear
ThrustSegment_ThrustAngle2Sigma_Quadratic
ThrustSegment_ThrustAnglesSigma_Constant
ThrustSegment_ThrustAnglesSigma_Linear
ThrustSegment_ThrustAnglesSigma_Mixed
ThrustSegment_ThrustAnglesSigma_Quadratic
TrkFile_SimEst_GPS_PosVec
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
None
Script errors:
AcceptFilter_DataTypes_SpaceToSpace_Range:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AcceptFilter_DataTypes_SpaceToSpace_Range.txt
does not exist
AcceptFilter_Tracker_SpaceToSpace:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\AcceptFilter_Tracker_SpaceToSpace.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
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
EKF_RejectFilter_DataTypes_GpsPosVec:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\EKF_RejectFilter_DataTypes_GpsPosVec.txt
does not exist
EKF_TrackingFileSet_DataFilters_GpsPosVec:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\EKF_TrackingFileSet_DataFilters_GpsPosVec.txt
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_DegToRad:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\MatlabFunction_Custom_DegToRad.report
does not exist
MatlabFunction_Custom:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\MatlabFunction_Custom.report
does not exist
MatlabFunction_FunctionPath_Relative:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\MatlabFunction_FunctionPath_Relative.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_3:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_ExitMode_SaveAndContinue_3.report
does not exist
Optimize_fmincon_ExitMode_SaveAndContinue:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_ExitMode_SaveAndContinue.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_4:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_Minimize_Height_on_circle_4.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_RunInitialGuess:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_SolveMode_RunInitialGuess.report
does not exist
Optimize_fmincon_cvg_status:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_cvg_status_Report2.report
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
RejectFilter_DataTypes_SpaceToSpace_Range:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\RejectFilter_DataTypes_SpaceToSpace_Range.txt
does not exist
RejectFilter_Tracker_SpaceToSpace:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\RejectFilter_Tracker_SpaceToSpace.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
SpacecraftNavigation_MultiSat_SpaceToSpace_EphPropNRHO_DSN_Moon:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\SpacecraftNavigation_MultiSat_SpaceToSpace_EphPropNRHO_DSN_Moon.txt
does not exist
SpacecraftNavigation_MultiSat_SpaceToSpace_EphPropNRHO_GN_Moon:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\SpacecraftNavigation_MultiSat_SpaceToSpace_EphPropNRHO_GN_Moon.txt
does not exist
ThrustSegment_SolveFors_ThrustScaleFactor_EphProp_TDRS: [GMT-7289]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\ThrustSegment_SolveFors_ThrustScaleFactor_EphProp_TDRS.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
TrackingFileSet_DataFilters_SpaceToSpace:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\TrackingFileSet_DataFilters_SpaceToSpace.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:
EKF_EphemerisFile_STK_IncludeEventBoundaries_False: (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".
Plate_SolveFors_AreaCoefficient_EphProp_TDRS: (truth) [GMT-7289]
ERROR MESSAGE: Comparator BLSEstimatedStateComparator failed: Error
using fileread (line 23)
Could not open file
C:\Users\gsfc580gmattest\Documents\ScriptTest\input\Resources\FRR-71_Plate\truth\Plate_SolveFors_AreaCoefficient_EphProp_TDRS.truth.
No such file or directory.
Smoother_Filter_EphemerisPredictionsMatch_GpsPosVec: (reg)
ERROR MESSAGE: Array indices must be positive integers or logical
values.
Truth failures:
API_PD45PropagationE8x8SMPM (API) [pos err 0.000753381, tol 1e-07]
BatchEstimator_Propagator_Multiple_SunEarthMoon [Residual failed at 10
Jun
2010 01:30:00.000] [GMT-7421]
EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_STK/EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_STK_Smoother.e
[EphemerisTimePosVel failed position magnitude tolerance at row 216]
EKFS_EphemerisFile_STK_IncludeCovariance_None_Moon/EKFS_EphemerisFile_STK_IncludeCovariance_None_Moon_Smoother.e
[EphemerisTimePosVel failed velocity magnitude tolerance at row 1]
EKFS_EphemerisFile_STK_IncludeCovariance_None_Sun/EKFS_EphemerisFile_STK_IncludeCovariance_None_Sun_Smoother.e
[EphemerisTimePosVel failed velocity magnitude tolerance at row 1]
EKFS_EphemerisFile_STK_IncludeCovariance_Position_Moon/EKFS_EphemerisFile_STK_IncludeCovariance_Position_Moon_Smoother.e
[CovarianceTimePos failed tolerance at row 2]
EKFS_EphemerisFile_STK_IncludeCovariance_Position_Sun/EKFS_EphemerisFile_STK_IncludeCovariance_Position_Sun_Smoother.e
[EphemerisTimePosVel failed velocity magnitude tolerance at row 1]
EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Moon/EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Moon_Smoother.e
[CovarianceTimePosVel failed tolerance at row 2]
EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Sun/EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Sun_Smoother.e
[EphemerisTimePosVel failed velocity magnitude tolerance at row 1]
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_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_ColdStart/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_ColdStart_Smoother.e
[CovarianceTimePos failed tolerance at row 2] [GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LargeMeasurementGap/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LargeMeasurementGap_Smoother.txt
[Sigma-B failed at 16 Mar 2019 00:00:00.000]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_Smoother.e
[CovarianceTimePos failed tolerance at row 2] [GMT-7398]
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_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_ProcessNoiseModel_RandomConstantADSF_GN/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantADSF_GN_FPS.mat
[Covariance comparison failed tolerance at 11 of 12 significant digits at
index (7,6,172)]
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantBias_DSN/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantBias_DSN_FPS.mat
[Covariance comparison failed tolerance at 7 of 14 significant digits at index
(8,8,581)]
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantCd_GN/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantCd_GN_FPS.mat
[Covariance comparison failed tolerance at 12 of 14 significant digits at
index (7,6,172)]
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantCr_DSN_Sun/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantCr_DSN_Sun_FPS.mat
[Covariance comparison failed tolerance at 12 of 14 significant digits at
index (7,3,312)]
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantNPlate_DSN_Sun/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantNPlate_DSN_Sun_FPS.mat
[Covariance comparison failed tolerance at 13 of 14 significant digits at
index (7,3,312)]
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantSPADDrag_GN/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantSPADDrag_GN_FPS.mat
[Covariance comparison failed tolerance at 12 of 14 significant digits at
index (7,6,172)]
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantSPADSRP_DSN_Sun/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantSPADSRP_DSN_Sun_FPS.mat
[Covariance comparison failed tolerance at 13 of 14 significant digits at
index (7,3,312)]
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantTSF_DSN/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantTSF_DSN_FPS.mat
[Covariance comparison failed tolerance at 13 of 14 significant digits at
index (6,5,607)]
EKFS_ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_GpsPosVec/EKFS_ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_GpsPosVec_Smoother_backfilter.txt
[Parameter EstSat.EarthMJ2000Eq.X error 0.006062 exceeds tolerance 0.005000]
[GMT-7483]
EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_CCSDS [#11 failed]
EphemStressTests_Default_Prop_CCSDS_Forward_and_BackwardDirect []
[GMT-6840]
ErrorModel_SolveFors_PassBiases_AzimuthElevation [Parameter
EstCAN.EstSat_Azimuth.PassBiases.1 error 0.100000 exceeds tolerance
0.010000] [GMT-7565]
ErrorModel_SolveFors_PassBiases_SpaceToSpace_DSN [0 truth states are
present but 8 tolerances were provided] [GMT-7565]
ErrorModel_SolveFors_PassBiases_XEastYNorth [Parameter
EstCAN.EstSat_XEast.PassBiases.1 error 0.100000 exceeds tolerance 0.010000]
[GMT-7565]
fmincon_Report [#1 failed]
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_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_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_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]
Simulator_Propagator_SPK_TDRS_Multiple [Residual failed at 01 Mar 2005
01:00:00.000] [GMT-7289]
Smoother_AddPredictToMatlabFile_ADSF_GpsPosVec [Variable
Smoother.State(7,:) error 0.097486 failed tolerance 1e-06 at linear index
1]
Smoother_AddPredictToMatlabFile_Bias_RangeSkinAzimuthElevation [Variable
Smoother.State(7,:) error 0.0939565 failed tolerance 1e-06 at linear index
1]
Smoother_AddPredictToMatlabFile_Cd_Cr_GpsPosVec [Variable
Smoother.State(7,:) error 0.0492116 failed tolerance 0.0001 at linear index
1]
Smoother_AddPredictToMatlabFile_NPlateCoefs_DSN [Variable
Smoother.State(9,:) error 3.96489 failed tolerance 1e-06 at linear index 1]
Smoother_AddPredictToMatlabFile_SPADDragScaleFactor_GN [Variable
Smoother.State(7,:) error 0.0129433 failed tolerance 1e-06 at linear index
1]
Smoother_AddPredictToMatlabFile_SPADSRP_XSouthYEast [Variable
Smoother.State(7,:) error 0.194622 failed tolerance 1e-06 at linear index
1]
Smoother_AddPredictToMatlabFile_TSF_Lunar_DSN [Variable
Smoother.State(7,:) error 4.55868e-05 failed tolerance 1e-06 at linear
index 1]
Smoother_Filter_FogmCd_FogmADSF_GpsPosVec [Covariance comparison failed
tolerance at 1 of 8 significant digits at index (8,8,361)]
Smoother_Filter_FogmCd_GpsPosVec [Covariance comparison failed tolerance
at 4 of 8 significant digits at index (7,7,361)]
Smoother_MatlabFile_BackfilterMatfileCorruption [Found extra field
BackwardComputed] [GMT-6949]
Smoother_MeasurementUpdate_GpsPosVec [EstSat.AtmosDensityScaleFactor
error
1.41843e-07 failed tolerance 1e-09 at index 1]
Smoother_PredictTimeSpan_STK_SN [Test ScenarioEpoch does not match truth
ScenarioEpoch] [GMT-7376]
Smoother_ReportFile_DuringEstimation_AllSolverIterations [Output field
576.799862 failed tolerance in record 435]
Smoother_ReportFile_FogmCd_FogmADSF_GpsPosVec [#515 failed]
Smoother_TimeUpdate_GpsPosVec [Variable Smoother.State(1:214) error
0.0888471 failed tolerance 1e-08 at linear index 1]
Spacecraft_Validation_AddPlates [#1 failed] [GMT-7022]
SpacecraftNavigation_Moon_DsnTcp_RangeRate_LRO_EarthInitialState_MoonFM_KeplerianState
[The test run failed to converge] [GMT-7515]
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]
ThrustSegment_SolveFors_ThrustAngles_Linear_ThreeAxisKinematic_GpsPosVec
[Parameter FM.Est_Thruster1_SetPoint1.ThrustAngle2.C1 error 0.000215
exceeds tolerance 0.000200]
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]
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):
TrkFile_SimEst_TDRS_range_Solve_Cr [] [GMT-5416]
Output changes (but still pass) (deferred):
Ephem_GMAT_Code500_StepSize [GMT-4112]
Ephem_GMAT_Code500_StepSize [GMT-4112]
Ephem_GMAT_Code500_StepSize [GMT-4112]
Output changes (but still fail) (deferred):
Ephem_GMAT_Code500_InterpolationOrder [pos err 0.0173914, 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]
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):
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond
[GMT-7291, GMT-7398]
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_NormalMatrixReduction_UseInitialCovariance [#1 failed]
[GMT-7274]
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
[CovarianceTimePos failed tolerance at row 2] [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_ErrorModel_SolveFors_Bias_RandomConstant_GN [GMT-7434-Linux]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_EarthFixed
[GMT-7398]
EKFS_SpacecraftNavigation_Moon_DsnTcp_RangeRate_LRO_EarthInitialState_MoonFM
[GMT-6801]
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]
ScriptLanguage_LineContinuation_BeginningOfLine [GMT-3756]
ScriptLanguage_Validation_DataTypes_ReferenceArray_Formation_5
[GMT-6064]
Simulator_Propagator_EarthPointMass_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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