----------------------------------------------------------------- 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] _______________________________________________ Gmat-buildtest mailing list Gmat-buildtest@lists.sourceforge.net https://lists.sourceforge.net/lists/listinfo/gmat-buildtest