-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Windows 10/MATLAB R2017a/VS 2013
Tested build: 2021-09-15
Regression build: 2021-09-14

Total number of scripts: 15872 (+98 deferred)
Percent Passed: 99.41%
New issues: 16
        Output changes: 4
        New truth failures: 7
        New crashes: 0
        New script errors: 5
        New comparator errors: 0
Fixed issues: 38
Total issues: 106

Test system warnings: 52
New deferred issues: 9
Fixed deferred issues: 0
Total deferred issues: 74

Run Time: 00 hours, 10 minutes, 56 seconds

-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
        EKFS_SpacecraftNavigation_GEO_Range_SDO_NPlateAreaCoefficient [The test
run failed to complete]
        
EKFS_SpacecraftNavigation_Moon_DsnTcp_RangeRate_LRO_EarthInitialState_MoonFM 
[The test run failed to complete] [GMT-6801]
        EKFS_SpacecraftNavigation_Sun_DSN_STEREOA_EarthInitialState_SunFM [The
test run failed to complete]
        EKFS_SpacecraftNavigation_Sun_DSN_STEREOA_SunInitialState_EarthFM [The
test run failed to complete]
        Matlab_NoOutputs []
        Vary_optimizer_fmincon__AdditiveScaleFactor_Variable [ptrn 1,2 failed]
        Vary_optimizer_fmincon_MultiplicativeScaleFactor_ArrayElement [ptrn 1,2
failed]

Output changes (but still pass):
        BatchEstimator_Propagator_SPK_GN
        KalmanFilter_Propagator_SPK_TDRS
        RunEstimator_SolveMode_RunInitialGuess
        Smoother_PredictTimeSpan_STK

Output changes (but still fail):
        None

New crashes/hangs/etc.:
        None

New script errors:
        MatlabFunction_Custom
        Optimize_fmincon_ExitMode_DiscardAndContinue_2
        Optimize_fmincon_SolveMode_Solve
        Vary_optimizer_fmincon_InitialGuess_ForLoopVariable
        scriptEvent_optimizer_fmincon__InitialValue_RealNumber

New comparator errors:
        None

-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
        EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_STK
        EKFS_EphemerisFile_STK_IncludeCovariance_None_Moon
        EKFS_EphemerisFile_STK_IncludeCovariance_None_Sun
        EKFS_EphemerisFile_STK_IncludeCovariance_Position_Moon
        EKFS_EphemerisFile_STK_IncludeCovariance_Position_Sun
        EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Moon
        EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Sun
        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
[GMT-7398]
        EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantADSF_GN
        EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantBias_DSN
        EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantCd_GN
        EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantCr_DSN_Sun
        EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantNPlate_DSN_Sun
        EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantSPADDrag_GN
        
EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantSPADSRP_DSN_Sun
        EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantTSF_DSN
        Matlab_NoInputsOutputs
        Smoother_AddPredictToMatlabFile_ADSF_GpsPosVec
        Smoother_AddPredictToMatlabFile_Cd_Cr_GpsPosVec
        Smoother_AddPredictToMatlabFile_NPlateCoefs_DSN
        Smoother_AddPredictToMatlabFile_SPADDragScaleFactor_GN
        Smoother_AddPredictToMatlabFile_SPADSRP_XSouthYEast
        Smoother_AddPredictToMatlabFile_TSF_Lunar_DSN
        Smoother_Filter_FogmCd_FogmADSF_GpsPosVec
        Smoother_Filter_FogmCd_GpsPosVec
        Smoother_MeasurementUpdate_GpsPosVec
        Smoother_ReportFile_DuringEstimation_AllSolverIterations
        Smoother_ReportFile_FogmCd_FogmADSF_GpsPosVec
        Smoother_TimeUpdate_GpsPosVec
        StopCond_GMAT_MultiProp_StopGroupings_FirstStep
        Vary_optimizer_fmincon_MultiplicativeScaleFactor_RealNumber

Fixed crashes/hangs/etc.:
        None

Fixed script errors:
        MatlabFunction_Custom_magic
        Optimize_fmincon_SolveMode_RunInitialGuess
        Optimize_fmincon_cvg_status
        Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2
        scriptEvent_optimizer_fmincon__InitialValue_Variable

Fixed comparator errors:
        None

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

Script errors:
        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
        KalmanFilter_InputWarmStartFile_RangeSkinAzimuthElevation_Bias_Multiple:
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\KalmanFilter_InputWarmStartFile_RangeSkinAzimuthElevation_Bias_Multiple_EkfWarmStart.txt
 does not exist
        KalmanFilter_InputWarmStartFile_RangeSkinAzimuthElevation_Cd_Cr_Bias:
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\KalmanFilter_InputWarmStartFile_RangeSkinAzimuthElevation_Cd_Cr_Bias_EkfWarmStart.txt
 does not exist
        
KalmanFilter_OutputWarmStartFile_RangeSkinAzimuthElevation_Bias_Multiple:
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\KalmanFilter_OutputWarmStartFile_RangeSkinAzimuthElevation_Bias_Multiple.tab
 does not exist
        KalmanFilter_OutputWarmStartFile_RangeSkinAzimuthElevation_Cd_Cr_Bias:
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\KalmanFilter_OutputWarmStartFile_RangeSkinAzimuthElevation_Cd_Cr_Bias.tab
 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_Solve:
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_SolveMode_Solve.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
        SpacecraftNavigation_Multisat_AquaTD6_Cd_Crosslink: [GMT-7421]
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\SpacecraftNavigation_Multisat_AquaTD6_Cd_Crosslink.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
        Vary_optimizer_fmincon_InitialGuess_ForLoopVariable:
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_InitialGuess_ForLoopVariable.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_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_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. 

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_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_ErrorModel_SolveFors_Bias_RandomConstant_AzimuthElevation/EKFS_ErrorModel_SolveFors_Bias_RandomConstant_AzimuthElevation_Filter.txt
 [Parameter EstCAN.EstSat_EstAngle1Model.Bias error 0.313744 exceeds tolerance 
0.005000]
        
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_AzimuthElevation/EKFS_ErrorModel_SolveFors_Bias_RandomConstant_AzimuthElevation_Smoother_backfilter.txt
 [Parameter EstCAN.EstSat_EstAngle1Model.Bias error 0.141966 exceeds tolerance 
0.020000]
        
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_AzimuthElevation/EKFS_ErrorModel_SolveFors_Bias_RandomConstant_AzimuthElevation_Smoother.txt
 [Parameter EstCAN.EstSat_EstAngle1Model.Bias error 0.313744 exceeds tolerance 
0.005000]
        
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_XEastYNorth/EKFS_ErrorModel_SolveFors_Bias_RandomConstant_XEastYNorth.txt
 [Parameter EstCAN.EstSat_EstAngle1Model.Bias error 0.287026 exceeds tolerance 
0.005000]
        
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_XEastYNorth/EKFS_ErrorModel_SolveFors_Bias_RandomConstant_XEastYNorth_Smoother.txt
 [Parameter EstCAN.EstSat_EstAngle1Model.Bias error 0.287026 exceeds tolerance 
0.005000]
        
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_XEastYNorth/EKFS_ErrorModel_SolveFors_Bias_RandomConstant_XEastYNorth_Smoother_backfilter.txt
 [Parameter EstCAN.EstSat_EstAngle1Model.Bias error 0.287636 exceeds tolerance 
0.050000]
        
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_XSouthYEast/EKFS_ErrorModel_SolveFors_Bias_RandomConstant_XSouthYEast.txt
 [Parameter EstCAN.EstSat_EstAngle1Model.Bias error 0.133549 exceeds tolerance 
0.005000]
        
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_XSouthYEast/EKFS_ErrorModel_SolveFors_Bias_RandomConstant_XSouthYEast_Smoother.txt
 [Parameter EstCAN.EstSat_EstAngle1Model.Bias error 0.133549 exceeds tolerance 
0.005000]
        
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_XSouthYEast/EKFS_ErrorModel_SolveFors_Bias_RandomConstant_XSouthYEast_Smoother_backfilter.txt
 [Parameter EstCAN.EstSat_EstAngle1Model.Bias error 0.172173 exceeds tolerance 
0.050000]
        
EKFS_SpacecraftNavigation_GEO_Angles_GOES14_Bias/EKFS_SpacecraftNavigation_GEO_Angles_GOES14_Bias_Filter.txt
 [Parameter GOES14.EarthMJ2000Eq.X error 0.641482 exceeds tolerance 0.010000]
        
EKFS_SpacecraftNavigation_GEO_Angles_GOES14_Bias/EKFS_SpacecraftNavigation_GEO_Angles_GOES14_Bias_Smoother_backfilter.txt
 [Parameter GOES14.EarthMJ2000Eq.X error 31.066048 exceeds tolerance 0.010000]
        
EKFS_SpacecraftNavigation_GEO_Angles_GOES14_Bias/EKFS_SpacecraftNavigation_GEO_Angles_GOES14_Bias_Smoother.txt
 [Parameter GOES14.EarthMJ2000Eq.X error 0.641482 exceeds tolerance 0.010000]
        
EKFS_SpacecraftNavigation_GEO_Range_SDO_NPlateAreaCoefficient/EKFS_SpacecraftNavigation_GEO_Range_SDO_NPlateAreaCoefficient_Smoother.txt
 [The test run failed to complete]
        
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_Filter.e
 [Test NumberOfCovariancePoints does not equal truth NumberOfCovariancePoints] 
[GMT-7483]
        
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_Smoother.e
 [Test NumberOfCovariancePoints does not equal truth NumberOfCovariancePoints] 
[GMT-7483]
        
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_SmoEph/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_SmoEph_Smoother.e
 [Test NumberOfCovariancePoints does not equal truth NumberOfCovariancePoints] 
[GMT-7483]
        
EKFS_SpacecraftNavigation_Moon_DsnTcp_RangeRate_LRO_EarthInitialState_MoonFM/EKFS_SpacecraftNavigation_Moon_DsnTcp_RangeRate_LRO_EarthInitialState_MoonFM_Smoother.txt
 [The test run failed to complete] [GMT-6801]
        EKFS_SpacecraftNavigation_MultiSat_TdrsAndUser_DifferentProcessNoise [0
truth states are present but 12 tolerances were provided] [GMT-7421]
        EKFS_SpacecraftNavigation_OrbitErrorCovariance_GN_Moon [Failed to find a
covariance record at 10 Sep 2005 00:00:00.000] [GMT-6801]
        
EKFS_SpacecraftNavigation_Sun_DSN_STEREOA_EarthInitialState_SunFM/EKFS_SpacecraftNavigation_Sun_DSN_STEREOA_EarthInitialState_SunFM_Smoother.txt
 [The test run failed to complete]
        
EKFS_SpacecraftNavigation_Sun_DSN_STEREOA_SunInitialState_EarthFM/EKFS_SpacecraftNavigation_Sun_DSN_STEREOA_SunInitialState_EarthFM_Smoother.txt
 [The test run failed to complete]
        
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 14.750640 exceeds 
tolerance 0.005000] [GMT-7483]
        EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_CCSDS [#11 failed]
        EphemStressTests_Default_Prop_CCSDS_Forward_and_BackwardDirect []
[GMT-6840]
        ErrorModel_SolveFors_Bias_XEastYNorthDsnSeqRange [Parameter
EstMAD.EstSat_EstRangeBiasModel.Bias error 49.985818 exceeds tolerance
2.000000]
        ErrorModel_SolveFors_PassBiases_SpaceToSpace_DSN [0 truth states are
present but 8 tolerances were provided] [GMT-7565]
        fmincon_Report [#1 failed]
        GroundStation_Iono_Range_DeepSpace [Found 13688 output records and 13695
truth records] [GMD-7061]
        KalmanFilter_AddPredictToMatlabFile_Bias_RangeSkinAzimuthElevation
[Variable Filter.State(7,:) error 0.174599 failed tolerance 1e-06 at linear
index 226]
        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_OutputWarmStartFile_RangeSkinAzimuthElevation_Bias [Output
field 1693.271454 failed tolerance in record 226]
        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_Bias_RangeSkinAzimuthElevation [Variable
Smoother.State(7,:) error 21.1309 failed tolerance 1e-06 at linear index 1]
        Smoother_Filter_Bias_RangeSkinAzimuthElevation_Sun [Parameter
EstSat.SunMJ2000Eq.X error 10.349946 exceeds tolerance 5.000000]
        Smoother_MatlabFile_BackfilterMatfileCorruption [Found extra field
BackwardComputed] [GMT-6949]
        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_SharedBias_Angles [The test 
run
failed to converge] [GMT-7421]
        SpacecraftNavigation_MultiSat_SpaceToSpace_SharedBias_Range [The test 
run
failed to converge]
        SpacecraftNavigation_TDRS_SecondGen_MA2_Landsat7 [Residual failed at 28
Aug 2015 19:41:22.000] [GMT-7376]
        SpacecraftNavigation_TDRS_SecondGen_MA4_Landsat7 [Failed to find a
SN_Range residual record at 28 Aug 2015 19:41:12.000] [GMT-7376]
        
ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_EpochAfterBurn_GpsPosVec 
[The test run failed to converge] [GMT-7483]
        
ThrustSegment_SolveFors_ThrustAngles_Constant_ThreeAxisKinematic_EpochAfterBurn_GpsPosVec
 [The test run failed to converge] [GMT-7483]
        TrackingFileSet_AddTrackingConfig_DsnSeqRange [#1 failed] [GMR-7061]
        TrackingFileSet_AddTrackingConfig_DsnTcp [#1 failed] [GMR-7061]
        TrackingFileSet_AddTrackingConfig_Range [#1 failed] [GMR-7061]
        TrackingFileSet_AddTrackingConfig_RangeRate [#1 failed] [GMR-7061]
        TrackingFileSet_FileName2 [#2 failed] [GMR-7061]
        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_ArrayElement [ptrn 1,2
failed]

-----------------------------------------------------------------
New Issues (Deferred)
-----------------------------------------------------------------
New truth failures (deferred):
        None

Output changes (but still pass) (deferred):
        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]
        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):
        None

Fixed comparator errors (deferred):
        None

-----------------------------------------------------------------
All Known Issues (Deferred)
-----------------------------------------------------------------
Crashes/hangs/etc. (deferred):
        GMAT_LunarTransfer_AllPlanets_DE421_BS
        GMAT_MarsTransfer_4_BS

Script errors (deferred):
        BatchEstimator_EstimationEpoch [GMT-5708]
        EKF_SpacecraftNavigation_OrbitErrorCovariance_Keplerian_GpsPosVec
        EKF_SpacecraftNavigation_SolveFors_KeplerianState_Cd_RandomConstant_GN
        EKF_SpacecraftNavigation_SolveFors_KeplerianState_Cr_RandomConstant_DSN
        EKF_SpacecraftNavigation_SolveFors_KeplerianState_GN
        EKF_SpacecraftNavigation_SolveFors_KeplerianState_GpsPosVec
        KalmanFilter_InputWarmStartFile_GN_Moon_Keplerian [GMT-6801]
        KalmanFilter_InputWarmStartFile_GpsPosVec_KeplerianToCartesian 
[GMT-6801]
        KalmanFilter_OutputWarmStartFile_GpsPosVec_Keplerian [GMT-6801]
        Math_Shadowed_Builtins [GMT-3043]
        OCPropTest_SPAD_Drag_1deg_Bicubic_LEO [GMT-7147]
        OCPropTest_SPAD_Drag_SRP_1deg_Bicubic_LEO [GMT-7147]
        Python_IO_String [5317]
        ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522]
        THF_Sim_Accel_ConfigD_None_NA_2 [GMT-6451]
        THF_Sim_Accel_ConfigD_None_NA_3 [GMT-6451]
        THF_Sim_Accel_ConfigD_None_NA_4 [GMT-6451]
        THF_Sim_Accel_ConfigD_None_NA [GMT-6451]
        THF_Sim_Thrust_CSF2_None_NA_ZeroTSF [GMT-6451]
        ThrustHistoryFile_EstimateTSF_EpochBeforeBurn_RSSStep_Aqua [GMT-6451]
        ThrustSegment_SolveFors_ThrustScaleFactor_Multiple_RSSStep [GMT-6451]
        ThrustSegment_SolveFors_ThrustScaleFactor_RSSStep [GMT-6451]
        TrkFile_SimEst_DSN_DS_Range_Solve_Bias_apriori [GMT-5709]

Comparator errors (deferred):
        GroundStation_Iono_Range_Kband (truth) [GMT-5644]
        GroundStation_Iono_RangeRate_Kband (truth) [GMT-5644]
        GroundStation_TropoIono_Range_Kband (truth) [GMT-5644]

Truth failures (deferred):
        AcceptFilter_Validation_RecordNumbers [#5 failed] [GMT-6034]
        Achieve_Validation_LHS_Field [ptrn 1 failed] [GMT-3687]
        Achieve_Validation_RHS_Field [no error or exception] [GMT-3687]
        BatchEstimator_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
 [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]
        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)
        BatchEstimator_Propagator_STK_TDRS [GMT-7289]
        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_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]
        ErrorModel_SolveFors_PassBiases_AzimuthElevation [GMT-7565]
        ErrorModel_SolveFors_PassBiases_XEastYNorth [GMT-7565]
        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]
        TrkFile_SimEst_TDRS_range_Solve_Cr [GMT-5416]



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