-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Windows 10/MATLAB R2017a/VS 2013
Tested build: 2021-06-10
Regression build: 2021-06-09

Total number of scripts: 15702 (+97 deferred)
Percent Passed: 99.43%
New issues: 15
        Output changes: 3
        New truth failures: 3
        New crashes: 0
        New script errors: 9
        New comparator errors: 0
Fixed issues: 240
Total issues: 105

Test system warnings: 54
New deferred issues: 10
Fixed deferred issues: 1
Total deferred issues: 74

Run Time: 22 hours, 44 minutes, 16 seconds

-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
        StopCond_GMAT_MultiProp_StopGroupings_FirstStep []
        Vary_optimizer_fmincon__AdditiveScaleFactor_Variable [ptrn 1,2 failed]
        
Vary_optimizer_fmincon_Additive_and_Multiplicative_ScaleFactor_RealNumber
[ptrn 1,2 failed]

Output changes (but still pass):
        BatchEstimator_Propagator_Multiple_MixedCentralBody

Output changes (but still fail):
        BatchEstimator_Propagator_Multiple_SunEarthMoon [Residual failed at 10 
Jun
2010 01:30:00.000] [GMT-7421]
        KalmanFilter_Propagator_Multiple_SunEarthMoon [Observed measurement 
failed
at 10 Jun 2010 00:00:00.000] [GMT-7421]

New crashes/hangs/etc.:
        None

New script errors:
        MatlabFunction_Custom_DegToRad_Assignment
        MatlabFunction_Custom
        MatlabFunction_FunctionPath_Relative
        Optimize_fmincon_ExitMode_DiscardAndContinue_2
        Optimize_fmincon_ExitMode_SaveAndContinue_3
        Optimize_fmincon_ExitMode_SaveAndContinue
        Optimize_fmincon_SolveMode_RunInitialGuess
        Optimize_fmincon_cvg_status
        Vary_optimizer_fmincon__InitialValue_RealNumber

New comparator errors:
        None

-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
        EKFS_AcceptFilter_Level2_DataTypes_SnDoppler
        EKFS_AcceptFilter_Level2_DataTypes_SnRange
        EKFS_EphemerisFile_STK_IncludeCovariance_None_Moon [GMT-7398]
        EKFS_EphemerisFile_STK_IncludeCovariance_None_Moon [GMT-7398]
        EKFS_EphemerisFile_STK_IncludeCovariance_None_Sun [GMT-7398]
        EKFS_EphemerisFile_STK_IncludeCovariance_None_Sun [GMT-7398]
        EKFS_EphemerisFile_STK_IncludeCovariance_Position_Moon [GMT-7398]
        EKFS_EphemerisFile_STK_IncludeCovariance_Position_Moon [GMT-7398]
        EKFS_EphemerisFile_STK_IncludeCovariance_Position_Sun [GMT-7398]
        EKFS_EphemerisFile_STK_IncludeCovariance_Position_Sun [GMT-7398]
        EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Moon
[GMT-7398]
        EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Moon
[GMT-7398]
        EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Sun
[GMT-7398]
        EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Sun
[GMT-7398]
        EKFS_ErrorModel_BiasSigma_SnDoppler
        EKFS_ErrorModel_BiasSigma_SnRange
        EKFS_ErrorModel_NoiseSigma_SnDoppler
        EKFS_ErrorModel_NoiseSigma_SnRange
        EKFS_ErrorModel_SolveFors_Bias_SnDoppler
        EKFS_ErrorModel_SolveFors_Bias_SnRange
        EKFS_ErrorModel_SolveFors_Bias_SnRangeSnDoppler
        EKFS_GroundStation_Iono_L1_Est
        EKFS_GroundStation_Iono_Moon_Est
        EKFS_GroundStation_Iono_Sun_DsnSeqRange_Est
        EKFS_GroundStation_Iono_Sun_Est
        EKFS_GroundStation_Iono_TRK223_DsnSeqRange_ACE
        EKFS_GroundStation_Iono_TRK223_DsnTcp_ACE
        EKFS_GroundStation_Tropo_L1_Est
        EKFS_GroundStation_Tropo_Marini_L1_Est
        EKFS_GroundStation_Tropo_Marini_Moon_Est
        EKFS_GroundStation_Tropo_Marini_Sun_DsnSeqRange_Est
        EKFS_GroundStation_Tropo_Marini_Sun_Est
        EKFS_GroundStation_Tropo_Moon_Est
        EKFS_GroundStation_Tropo_Sun_DsnSeqRange_Est
        EKFS_GroundStation_Tropo_Sun_Est
        EKFS_GroundStation_Tropo_TRK223_DsnSeqRange_ACE
        EKFS_GroundStation_Tropo_TRK223_DsnTcp_ACE
        EKFS_GroundStation_TropoIono_TRK223_DSN_ACE
        EKFS_GroundStation_TropoSeasonal_TRK223_DsnSeqRange_ACE
        EKFS_GroundStation_TropoSeasonal_TRK223_DsnTcp_ACE
        EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_EarthFixed
[GMT-7398]
        EKFS_TrackingFileSet_AddTrackingConfig_SN
        EKFS_TrackingFileSet_UseRelativityCorrection_AzimuthElevation_Est
        KalmanFilter_Smoother_PredictTimeSpan_Both_OEM [GMT-6949]
        Matlab_NoInputsOutputs
        RunSmoother_GpsPosVec
        RunSmoother_GpsPosVec
        Smoother_AddPredictToMatlabFile_Cd_Cr_GpsPosVec
        Smoother_AddPredictToMatlabFile_GpsPosVec
        Smoother_DelayRectifyTimeSpan_DSN
        Smoother_DelayRectifyTimeSpan_DSN
        Smoother_Filter_EphemerisPredictionsMatch_GpsPosVec
        Smoother_Filter_FogmCd_FogmADSF_GpsPosVec
        Smoother_Filter_FogmCd_GpsPosVec
        Smoother_MatlabFile_FogmCd_FogmADSF_GpsPosVec
        Smoother_MeasDeweightingSigmaThreshold_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_ShowProgress_True
        Smoother_TimeUpdate_GpsPosVec
        ThrustSegment_SolveFors_ThrustAngles_Linear_ThreeAxisKinematic_GpsPosVec
        Vary_optimizer_fmincon_AdditiveScaleFactor_RealNumber
        Vary_optimizer_fmincon_MultiplicativeScaleFactor_Variable

Fixed crashes/hangs/etc.:
        None

Fixed script errors:
        EKFS_AcceptFilter_Level2_ObservedObjects_TDRS
        EKFS_EphemerisFile_STK_PredDv
        EKFS_ErrorModel_Bias_RangeSkin_Est
        EKFS_ErrorModel_Bias_SnDoppler_Est
        EKFS_ErrorModel_Bias_SnRange_Est
        EKFS_ErrorModel_Bias_XEastYNorth_Est
        EKFS_ErrorModel_Bias_XSouthYEast_Est
        EKFS_ErrorModel_SolveFors_Bias_RandomConstant_AzimuthElevation
        EKFS_ErrorModel_SolveFors_Bias_RandomConstant_DSN
        EKFS_ErrorModel_SolveFors_Bias_RandomConstant_GN [GMT-7434-Linux]
        EKFS_ErrorModel_SolveFors_Bias_RandomConstant_RangeSkin
        EKFS_ErrorModel_SolveFors_Bias_RandomConstant_XEastYNorth
        EKFS_ErrorModel_SolveFors_Bias_RandomConstant_XSouthYEast
        EKFS_Plate_AreaCoefficientSigma_DSN_Sun
        EKFS_Plate_AreaCoefficientSigma_GN_Moon
        EKFS_Plate_AreaCoefficientSigma_GpsPosVec
        EKFS_Plate_DiffuseFractionSigma_DSN_Sun
        EKFS_Plate_DiffuseFractionSigma_GN_Moon
        EKFS_Plate_DiffuseFractionSigma_GpsPosVec
        EKFS_Plate_DiffuseFractionSigma_RangeSkinAngles
        EKFS_Plate_Est_ApplyNPlateSRP
        EKFS_Plate_SolveFors_AreaCoefficient_Multiple_RangeSkinAngles
        EKFS_Plate_SolveFors_AreaCoefficient_Multiple
        EKFS_Plate_SolveFors_AreaCoefficient_RandomConstant
        EKFS_Plate_SolveFors_DiffuseFraction_Multiple_RandomConstant
        EKFS_Plate_SolveFors_DiffuseFraction_RandomConstant
        EKFS_Plate_SolveFors_SpecularFraction_Multiple_RandomConstant
        EKFS_Plate_SolveFors_SpecularFraction_RandomConstant
        EKFS_Plate_SpecularFractionSigma_DiffuseFractionSigma_DSN_Sun
        EKFS_Plate_SpecularFractionSigma_GN_Moon
        EKFS_Plate_SpecularFractionSigma_GpsPosVec
        EKFS_Plate_SpecularFractionSigma_RangeSkinAngles
        EKFS_SpacecraftNavigation_AtmosDensityScaleFactorSigma_DSN
        EKFS_SpacecraftNavigation_AtmosDensityScaleFactorSigma_GN
        
EKFS_SpacecraftNavigation_AtmosDensityScaleFactorSigma_RandomConstant_GpsPosVec
        EKFS_SpacecraftNavigation_AtmosDensityScaleFactorSigma_RangeSkinAngles
        EKFS_SpacecraftNavigation_CdSigma_RandomConstant_Angles
        EKFS_SpacecraftNavigation_CdSigma_RandomConstant_GN
        EKFS_SpacecraftNavigation_CrSigma_RandomConstant_DSN_Sun
        EKFS_SpacecraftNavigation_CrSigma_RandomConstant_DsnSeqRange_L1
        EKFS_SpacecraftNavigation_CrSigma_RandomConstant_GN_Moon
        EKFS_SpacecraftNavigation_CrSigma_RandomConstant_RangeSkinAngles
        EKFS_SpacecraftNavigation_GEO_Angles_GOES14_Bias
        EKFS_SpacecraftNavigation_GEO_Angles_GOES14
        EKFS_SpacecraftNavigation_GEO_Range_SDO_NPlateAreaCoefficient [GMT-6801]
        EKFS_SpacecraftNavigation_LEO_AnglesRangeSkin_ISS_FOGM_Cd
        EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_ColdStart
[GMT-7398]
        
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LargeMeasurementGap
        
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_SmoEph
        
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv
        EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart
[GMT-7398]
        EKFS_SpacecraftNavigation_LEO_RangeRate_SMAP
        EKFS_SpacecraftNavigation_LEO_RangeSkin_ISS_FOGM_Cd
        EKFS_SpacecraftNavigation_Moon_DsnTcpRangeRate_THEMISB_Cr
        
EKFS_SpacecraftNavigation_Moon_DsnTcp_RangeRate_LRO_EarthInitialState_MoonFM 
[GMT-6801]
        EKFS_SpacecraftNavigation_MultiSat_TdrsAndUser
        EKFS_SpacecraftNavigation_Multisat_AquaTD6_Cd
        EKFS_SpacecraftNavigation_OrbitErrorCovariance_DSN_L1
        EKFS_SpacecraftNavigation_OrbitErrorCovariance_DSN_Sun
        EKFS_SpacecraftNavigation_ProcessNoiseModel_DSN_Sun
        EKFS_SpacecraftNavigation_ProcessNoiseModel_DsnSeqRange_L1
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_ADSF_RandomConstant_GN
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_ADSF_RandomConstant_GpsPosVec
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_AzimuthElevation
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_FOGM_GN
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_FOGM_GpsPosVec
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_RandomConstant_AzimuthElevation
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_RandomConstant_GN
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_RandomConstant_GpsPosVec
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cr_RandomConstant_DSN
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cr_RandomConstant_GpsPosVec
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cr_RandomConstant_XEastYNorth
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cr_RandomConstant_XSouthYEast
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_DSN_Sun
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_DSN
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_DsnSeqRange_L1
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCdConstr_FogmADSF_GN
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCdConstr_FogmADSF_GpsPosVec
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSFConstr_GN
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSFConstr_GpsPosVec
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_GN
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_GpsPosVec
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_GN_Moon
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_GN_Sun
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_GN
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_GpsPosVec
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_RandomConstCdConstr_RandomConstADSF_GN
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_RandomConstCdConstr_RandomConstADSF_GpsPosVec
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_RandomConstCd_RandomConstADSFConstr_GN
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_RandomConstCd_RandomConstADSFConstr_GpsPosVec
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_RangeSkin
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_SN
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SPADDragScaleFactor_RandomConstant_GN
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SPADSRPScaleFactor_RandomConstant_DSN
        EKFS_SpacecraftNavigation_Sun_DSN_STEREOA_EarthInitialState_SunFM
[GMT-6801]
        EKFS_SpacecraftNavigation_Sun_DSN_STEREOA_SunInitialState_EarthFM
[GMT-6801]
        EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr [GMT-7278-Linux]
        EKFS_SpacecraftNavigation_TRK223_DSN_ACE
        EKFS_Spacecraft_NPlateSRPEquateAreaCoefficients
        EKFS_ThrustHistoryFile_EstimateTSF_ADSF_Aqua
        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_DSN
        EKFS_ThrustSegment_SolveFors_ThrustAngles_ThrustScaleFactor_Cr_GN
        EKFS_ThrustSegment_SolveFors_ThrustAngles_ThrustScaleFactor_Cr_GpsPosVec
        EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_DSN_Sun
        EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_GN_L1
        EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_GN_Moon
        EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_Long_LowThrust
        EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_Multiple
        EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_RangeSkinAngles
        EKFS_ThrustSegment_SolveFors_ThrustScaleFactor
        EKFS_ThrustSegment_ThrustScaleFactorSigma_GN_L1
        EKFS_ThrustSegment_ThrustScaleFactorSigma_GN_Moon
        EKFS_ThrustSegment_ThrustScaleFactorSigma_GpsPosVec
        EKFS_ThrustSegment_ThrustScaleFactorSigma_RangeSkinAngles
        EKFS_ThrustSegment_ThrustScaleFactorSigma
        
EKFS_TrackingFileSet_AberrationCorrection_AnnualAndDiurnal_XEastYNorth_Est
        
EKFS_TrackingFileSet_AberrationCorrection_AnnualAndDiurnal_XSouthYEast_Est
        EKFS_TrackingFileSet_AberrationCorrection_Annual_AzimuthElevation_Est
        EKFS_TrackingFileSet_AberrationCorrection_Annual_XEastYNorth_Est
        EKFS_TrackingFileSet_AberrationCorrection_Annual_XSouthYEast_Est
        EKFS_TrackingFileSet_AberrationCorrection_Diurnal_AzimuthElevation_Est
        EKFS_TrackingFileSet_AberrationCorrection_Diurnal_XEastYNorth_Est
        EKFS_TrackingFileSet_AberrationCorrection_Diurnal_XSouthYEast_Est
        EKFS_TrackingFileSet_AberrationCorrection_None_AzimuthElevation_Est
        EKFS_TrackingFileSet_AberrationCorrection_None_XEastYNorth_Est
        EKFS_TrackingFileSet_AberrationCorrection_None_XSouthYEast_Est
        EKFS_TrackingFileSet_UseETminusTAI_GN_L1_Est
        EKFS_TrackingFileSet_UseETminusTAI_GN_Moon_Est
        EKFS_TrackingFileSet_UseETminusTAI_RangeSkin_Est
        EKFS_TrackingFileSet_UseLightTime_DSN_Sun_Est
        EKFS_TrackingFileSet_UseLightTime_GN_L1_Est
        EKFS_TrackingFileSet_UseLightTime_GN_Moon_Est
        EKFS_TrackingFileSet_UseLightTime_RangeSkin_Est
        EKFS_TrackingFileSet_UseRelativityCorrection_GN_L1_Est
        EKFS_TrackingFileSet_UseRelativityCorrection_GN_Moon_Est
        EKFS_TrackingFileSet_UseRelativityCorrection_RangeSkin_Est
        EstimatedParameter_FOGM_SolveFor_Cd_AtmosDensityScaleFactor_DSN
        EstimatedParameter_FOGM_SolveFor_Cd_AtmosDensityScaleFactor_GN
        
EstimatedParameter_FOGM_SolveFor_Cd_AtmosDensityScaleFactor_RangeSkinAngles
        KalmanFilter_ProcessNoiseTimeStep_0sec_Backfilter
        KalmanFilter_ProcessNoiseTimeStep_240sec_Backfilter
        KalmanFilter_ProcessNoiseTimeStep_Angles_Backfilter
        KalmanFilter_ProcessNoiseTimeStep_DSN_Moon_Backfilter
        KalmanFilter_ProcessNoiseTimeStep_RangeSkin_Backfilter
        MatlabFunction_Custom_magic
        Optimize_fmincon_ExitMode_SaveAndContinue_2
        Optimize_fmincon_SolveMode_Defaultscript
        Optimize_fmincon_SolveMode_Solve
        ProcessNoiseModel_AccelNoiseSigma_GpsPosVec_BackFilter
        ProcessNoiseModel_CoordinateSystem_EarthVNB_GpsPosVec_BackFilter
        Smoother_CheckMeasurementEditing
        Smoother_DelayRectifyTimeSpan_GN
        Smoother_DelayRectifyTimeSpan_RangeSkinAzimuthElevation_Sun
        Smoother_DelayRectifyTimeSpan_XEastYNorth_Moon
        Smoother_DelayRectifyTimeSpan_XSouthYEast_L1
        Smoother_Filter_EndStatesMatch_GpsPosVec
        Smoother_Filter_GN_MoonFixed
        Smoother_Filter_GpsPosVec_EarthFixed
        Smoother_Filter_GpsPosVec
        Smoother_Filter_MeasDeweighting_FogmCd_FogmADSF_GpsPosVec
        Smoother_MeasDeweightingCoefficient_Angles
        Smoother_MeasDeweightingCoefficient_DSN_Sun
        Smoother_MeasDeweightingCoefficient_FogmCd_FogmADSF_GpsPosVec
        Smoother_MeasDeweightingCoefficient_GN_Moon
        Smoother_MeasDeweightingCoefficient_RangeSkin_L1
        Smoother_ReportStyle_Verbose
        Vary_optimizer_fmincon__InitialValue_Array
        Vary_optimizer_fmincon__InitialValue_Variable
        Write_Spacecraft_OrbitErrorCovariance_Smoother

Fixed comparator errors:
        None

-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
        None

Script errors:
        BatchEstimator_Propagator_EphProp_Numerical_TDRS: [GMT-7289]
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\BatchEstimator_Propagator_EphProp_Numerical_TDRS.txt
 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_SPK_StartLate_TDRS: [GMT-7289]
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\BatchEstimator_Propagator_SPK_StartLate_TDRS.txt
 does not exist
        BatchEstimator_Propagator_SPK_TDRS_Multiple: [GMT-7289]
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\BatchEstimator_Propagator_SPK_TDRS_Multiple.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
        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_3:
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_Minimize_Height_on_circle_3.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
        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_RealNumber:
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__LowerBound_RealNumber.report
 does not exist
        scriptEvent_optimizer_fmincon__InitialValue_RealNumber:
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\scriptEvent_optimizer_fmincon__InitialValue_RealNumber.report
 does not exist

Comparator errors:
        EKFS_EphemerisFile_STK_IncludeCovariance_None_Moon: (reg) [GMT-7398]
     ERROR MESSAGE: Array indices must be positive integers or logical
values. 
        EKFS_EphemerisFile_STK_IncludeCovariance_None_Moon: (reg) [GMT-7398]
     ERROR MESSAGE: Array indices must be positive integers or logical
values. 
        EKFS_EphemerisFile_STK_IncludeCovariance_None_Sun: (reg) [GMT-7398]
     ERROR MESSAGE: Array indices must be positive integers or logical
values. 
        EKFS_EphemerisFile_STK_IncludeCovariance_None_Sun: (reg) [GMT-7398]
     ERROR MESSAGE: Array indices must be positive integers or logical
values. 
        EKFS_EphemerisFile_STK_IncludeCovariance_Position_Moon: (reg) [GMT-7398]
     ERROR MESSAGE: Array indices must be positive integers or logical
values. 
        EKFS_EphemerisFile_STK_IncludeCovariance_Position_Moon: (reg) [GMT-7398]
     ERROR MESSAGE: Array indices must be positive integers or logical
values. 
        EKFS_EphemerisFile_STK_IncludeCovariance_Position_Sun: (reg) [GMT-7398]
     ERROR MESSAGE: Array indices must be positive integers or logical
values. 
        EKFS_EphemerisFile_STK_IncludeCovariance_Position_Sun: (reg) [GMT-7398]
     ERROR MESSAGE: Array indices must be positive integers or logical
values. 
        EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Moon: (reg)
[GMT-7398]
     ERROR MESSAGE: Array indices must be positive integers or logical
values. 
        EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Moon: (reg)
[GMT-7398]
     ERROR MESSAGE: Array indices must be positive integers or logical
values. 
        EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Sun: (reg)
[GMT-7398]
     ERROR MESSAGE: Array indices must be positive integers or logical
values. 
        EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Sun: (reg)
[GMT-7398]
     ERROR MESSAGE: Array indices must be positive integers or logical
values. 
        EKFS_EphemerisFile_STK_PredDv: (truth)
     ERROR MESSAGE: Comparator STKEphemerisComparator failed: Matrix
dimensions must agree.  
        EKFS_EphemerisFile_STK_PredDv: (truth)
     ERROR MESSAGE: Comparator STKEphemerisComparator failed: Matrix
dimensions must agree.  
        
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv: 
(truth)
     ERROR MESSAGE: Comparator STKEphemerisComparator failed: Matrix
dimensions must agree.  
        
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv: 
(truth)
     ERROR MESSAGE: Comparator STKEphemerisComparator failed: Matrix
dimensions must agree.  
        
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_SmoEph:
 (truth)
     ERROR MESSAGE: Comparator STKEphemerisComparator failed: Matrix
dimensions must agree.  
        EKFS_SpacecraftNavigation_OrbitErrorCovariance_GN_Moon: (truth) 
[GMT-6801]
     ERROR MESSAGE: Comparator EKFCovarianceReportComparator failed: Error
using fileread (line 23)
Could not open file
C:\Users\gsfc580gmattest\Documents\ScriptTest\input\Resources\FRR-59_SpacecraftNavigation\truth\EKFS_SpacecraftNavigation_OrbitErrorCovariance_GN_Moon.truth.
 No such file or directory.        
        EphemerisFile_LongFiniteBurn_EphemerisSegmentation_STK: (truth) 
[GMT-7483]
     ERROR MESSAGE: Comparator STKEphemerisComparator failed: Error using
fgets
Invalid file identifier. Use fopen to generate a valid file identifier. 
        Smoother_Filter_EphemerisPredictionsMatch_GpsPosVec: (reg)
     ERROR MESSAGE: Array indices must be positive integers or logical
values. 
        Smoother_PredictTimeSpan_STK: (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_NormalMatrixReduction_UseInitialCovariance [#1 failed]
[GMT-7274]
        BatchEstimator_Propagator_Code500_TDRS [The test run failed to converge]
[GMT-7289]
        BatchEstimator_Propagator_Code500_TDRS [ptrn 1,2 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.txt
 [The test run failed to converge] [GMT-7289]
        
BatchEstimator_Propagator_SPK_EndEarly_TDRS/BatchEstimator_Propagator_SPK_EndEarly_TDRS.txt
 [#1 failed] [GMT-7289]
        
BatchEstimator_Propagator_SPK_EndEarly_TDRS/BatchEstimator_Propagator_SPK_EndEarly_TDRS.log
 [ptrn 1,2 failed] [GMT-7289]
        
BatchEstimator_Propagator_SPK_HasGap_TDRS/BatchEstimator_Propagator_SPK_HasGap_TDRS.txt
 [The test run failed to converge] [GMT-7289]
        
BatchEstimator_Propagator_SPK_HasGap_TDRS/BatchEstimator_Propagator_SPK_HasGap_TDRS.txt
 [#1 failed] [GMT-7289]
        
BatchEstimator_Propagator_SPK_HasGap_TDRS/BatchEstimator_Propagator_SPK_HasGap_TDRS.log
 [ptrn 1,2 failed] [GMT-7289]
        BatchEstimator_Propagator_SPK_TDRS [The test run failed to converge]
[GMT-7289]
        BatchEstimator_Propagator_SPK_TDRS [ptrn 1,2 failed] [GMT-7289]
        BatchEstimator_Propagator_STK_TDRS [The test run failed to converge]
[GMT-7289]
        BatchEstimator_Propagator_STK_TDRS [ptrn 1,2 failed] [GMT-7289]
        BatchEstimator_ReportFile_MultiSat_SpaceToSpace [#3 failed] [GMT-7421]
        
EKFS_SpacecraftNavigation_GEO_Range_SDO_NPlateAreaCoefficient/EKFS_SpacecraftNavigation_GEO_Range_SDO_NPlateAreaCoefficient_Smoother.txt
 [The test run failed to complete] [GMT-6801]
        
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_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 14.753774 exceeds 
tolerance 0.005000] [GMT-7483]
        ErrorModel_SolveFors_Bias_SpaceToSpace_Range [Parameter
EstSatTarg.MoonMJ2000Eq.VX error 0.000030 exceeds tolerance 0.000020]
        fmincon_Report [#1 failed]
        GroundStation_Iono_Range_DeepSpace [Found 13688 output records and 13695
truth records] [GMD-7061]
        KalmanFilter_DelayRectifyTimeSpan_XSouthYEast_L1 [#1 failed] [GMT-6801]
        KalmanFilter_InputWarmStartFile_SN [Output field -4638.173817 failed
tolerance in record 1] [GMT-7376]
        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_GN [Residual failed at 01 Mar 2005 
01:00:00.000]
[GMT-7289]
        Simulator_Propagator_SPK_TDRS [Residual failed at 01 Mar 2005
01:00:00.000] [GMT-7289]
        Smoother_PredictTimeSpan_STK_SN [Test ScenarioEpoch does not match truth
ScenarioEpoch] [GMT-7376]
        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_EphProp_GN_Moon [The test run
failed to converge]
        SpacecraftNavigation_MultiSat_SpaceToSpace_EphPropNRHO_GN_Moon [The test
run failed to converge]
        StopCond_GMAT_MultiProp_StopGroupings_FirstStep []
        
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_ThrustAngles_Constant_ThrustMass_InterpolateLinear [pos 
err
0.000037]
        ThrustSegment_ThrustAngles_Constant_ThrustMass_InterpolateNone [pos err
0.000058]
        ThrustSegment_ThrustAngles_Quadratic [diff. num. lines]
        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_Additive_and_Multiplicative_ScaleFactor_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_InterpolationOrder [GMT-4075, GMT-4112]

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]
        Ephem_GMAT_Code500_StepSize [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_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]

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_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_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_CCSDS_Forward_and_BackwardDirect 
[GMT-6840]
        
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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