-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Windows 10/MATLAB R2017a/VS 2013
Tested build: 2021-06-07
Regression build: 2021-06-04
Total number of scripts: 15700 (+96 deferred)
Percent Passed: 99.40%
New issues: 61
Output changes: 28
New truth failures: 18
New crashes: 0
New script errors: 13
New comparator errors: 2
Fixed issues: 149
Total issues: 98
Test system warnings: 61
New deferred issues: 14
Fixed deferred issues: 1
Total deferred issues: 73
Run Time: 23 hours, 10 minutes, 46 seconds
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
Matlab_NoOutputs []
THF_Accel_CSB_None_NA []
THF_Accel_CSC_None_None []
THF_Accel_CSC_None_None_2 []
THF_AccelMass_CSB_None_None []
THF_AccelMass_CSC_None_None []
THF_AccelMass_CSC_None_None_2 []
THF_Thrust_CSB_None_NA []
THF_Thrust_CSC_None_None []
THF_ThrustMass_CSB_None_None []
THF_ThrustMass_CSC_None_None []
THF_ThrustMass_InterpolateLinear_RSSStep_ABM [diff. num. lines]
THF_ThrustMass_InterpolateLinear_RSSStep_PD45 [diff. num. lines]
THF_ThrustMass_InterpolateLinear_RSSStep_RK56 [diff. num. lines]
ThrustSegment_ThrustAngles_Constant_ThrustMass_InterpolateLinear [pos
err
0.000037]
ThrustSegment_ThrustAngles_Constant_ThrustMass_InterpolateNone [pos err
0.000058]
ThrustSegment_ThrustAngles_Quadratic [diff. num. lines]
Vary_optimizer_fmincon_Additive_and_Multiplicative_ScaleFactor_RealNumber
[ptrn 1,2 failed]
Output changes (but still pass):
EKF_THF_Prop_AccelMass_InterpolateLinear
KalmanFilter_InputWarmStartFile_GN_Moon
KalmanFilter_InputWarmStartFile_GN_Moon_MoonFixed
KalmanFilter_InputWarmStartFile_GN_NPlateSRP_AreaCoefficient
KalmanFilter_InputWarmStartFile_GN_NPlateSRP_DiffuseFraction
KalmanFilter_InputWarmStartFile_GN_NPlateSRP_SpecularFraction
Simulator_AddData_DSN_GN
Simulator_AddData_Range_RangeRate
Simulator_AddData_RangeRate
THF_AccelMass_InterpolateLinear
THF_AccelMass_InterpolateNone
THF_AccelMass_InterpolateSpline
THF_AccelMass_InterpolateSpline_BackProp
THF_Sim_AccelMass_InterpolateLinear
THF_Sim_AccelMass_InterpolateNone
THF_Sim_AccelMass_InterpolateSpline
THF_ThrustMass_InterpolateLinear
THF_ThrustMass_InterpolateLinear_RSSStep
THF_ThrustMass_InterpolateLinear_RSSStep_PD78
THF_ThrustMass_InterpolateLinear_RSSStep_PD853
THF_ThrustMass_InterpolateNone
THF_ThrustMass_InterpolateSpline
THF_ThrustMass_InterpolateSpline_BackProp
ThrustSegment_SolveFors_ThrustAngles_EpochAfterBurn_GpsPosVec
ThrustSegment_StepOverBurnStartTime
TrackingFileSet_SimDopplerCountInterval_5sec_SpaceToSpace
Write_Multiple_ReportFile_Script
Write_Multiple_ReportFile_Script_2
Output changes (but still fail):
None
New crashes/hangs/etc.:
None
New script errors:
MatlabFunction_Custom_DegToRad
MatlabFunction_FunctionPath_Relative
Matlab_NoInputs
Optimize_fmincon_ExitMode_DiscardAndContinue_2
Optimize_fmincon_ExitMode_SaveAndContinue_3
Optimize_fmincon_Minimize_Height_on_circle_4
Optimize_fmincon_Minimize_Height_on_circle
Optimize_fmincon_SolveMode_RunInitialGuess
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2
Vary_optimizer_fmincon__InitialValue_RealNumber
Vary_optimizer_fmincon__LowerBound_Array
Vary_optimizer_fmincon__LowerBound_Variable
scriptEvent_optimizer_fmincon__InitialValue_Variable
New comparator errors:
EKFS_EphemerisFile_STK_PredDv (truth)
EKFS_EphemerisFile_STK_PredDv (truth)
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
BatchEstimator_AbsoluteTol_MultiSat_SpaceToSpace
BatchEstimator_InversionAlgorithm_Internal_MultiSat_SpaceToSpace
BatchEstimator_InversionAlgorithm_Schur_MultiSat_SpaceToSpace
EKFS_Plate_DiffuseFractionSigma_GN_Moon
EKFS_Plate_DiffuseFractionSigma_GN_Moon
EKFS_Plate_DiffuseFractionSigma_GN_Moon
EKFS_Plate_SolveFors_SpecularFraction_RandomConstant
EKFS_Plate_SpecularFractionSigma_GN_Moon
EKFS_Plate_SpecularFractionSigma_GN_Moon
EKFS_Plate_SpecularFractionSigma_GN_Moon
EKFS_SpacecraftNavigation_AtmosDensityScaleFactorSigma_GN
EKFS_SpacecraftNavigation_AtmosDensityScaleFactorSigma_GN
EKFS_SpacecraftNavigation_CrSigma_RandomConstant_GN_Moon
EKFS_SpacecraftNavigation_CrSigma_RandomConstant_GN_Moon
EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_FOGM_GN
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCdConstr_FogmADSF_GN
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCdConstr_FogmADSF_GN
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCdConstr_FogmADSF_GN
EKFS_ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_GpsPosVec
[GMT-7483]
EKFS_ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_GpsPosVec
[GMT-7483]
EKFS_ThrustSegment_SolveFors_ThrustAngles_ThrustScaleFactor_Cr_GN
EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_GN_L1
EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_GN_L1
EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_GN_L1
EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_GN_Moon
EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_GN_Moon
EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_GN_Moon
ErrorModel_NoiseSigma_Range_RangeRate
ErrorModel_NoiseSigma_Range_RangeRate2
ErrorModel_NoiseSigma_RangeRate
ErrorModel_NoiseSigma_RangeRate2
ErrorModel_NoiseSigma_SpaceToSpace_GN
ErrorModel_SolveFors_Bias_SpaceToSpace_Range
ErrorModel_Type_Range_RangeRate
KalmanFilter_InputWarmStartFile_GN_NPlateSRP_AreaCoefficient
KalmanFilter_InputWarmStartFile_GN_NPlateSRP_DiffuseFraction
KalmanFilter_InputWarmStartFile_GN_NPlateSRP_SpecularFraction
Python_NoInputsOutputs
Python_NoOutputs
Simulator_Propagator_Multiple_SpacecraftDoesNotExist
SpacecraftNavigation_SolveFors_CartesianState_Cr_GN
SpacecraftNavigation_SolveFors_CartesianState_GN
SpacecraftNavigation_SolveFors_KeplerianState_Cr_GN
SpacecraftNavigation_SolveFors_KeplerianState_SPADDragScaleFactor_SPADSRPScaleFactor_GN
Vary_optimizer_fmincon_AdditiveScaleFactor_RealNumber
Vary_optimizer_fmincon_MultiplicativeScaleFactor_Variable
Fixed crashes/hangs/etc.:
None
Fixed script errors:
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_ColdStart
[GMT-7398]
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]
GmatFunction_SystemTime_TimeAccuracy
GroundStation_Iono_AzimuthElevation_DeepSpace
GroundStation_Iono_Azimuth
GroundStation_Iono_DsnSeqRange_DeepSpace
GroundStation_Iono_Elevation
GroundStation_Iono_L1
GroundStation_Iono_Moon
GroundStation_Iono_RangeRate_DeepSpace
GroundStation_Iono_RangeSkin
GroundStation_Iono_Range_TurnAround
GroundStation_Iono_Range_Xband
GroundStation_Iono_Range
GroundStation_Iono_Sun
GroundStation_Iono_XEastYNorth_DeepSpace
GroundStation_Iono_XEast
GroundStation_Iono_XSouthYEast_DeepSpace
GroundStation_Iono_XSouth
GroundStation_Iono_YEast
GroundStation_Iono_YNorth
GroundStation_TropoIono_AzimuthElevation
GroundStation_TropoIono_DsnSeqRange_DeepSpace
GroundStation_TropoIono_DsnTcp_DeepSpace
GroundStation_TropoIono_RangeRate_DeepSpace
GroundStation_TropoIono_RangeSkin
GroundStation_TropoIono_Range_DeepSpace
GroundStation_TropoIono_XEastYNorth
GroundStation_TropoIono_XSouthYEast
GroundStation_Tropo_Azimuth
GroundStation_Tropo_DsnSeqRange
GroundStation_Tropo_DsnTcp_DeepSpace
GroundStation_Tropo_Elevation
GroundStation_Tropo_L1
GroundStation_Tropo_Marini_AzimuthElevation_DeepSpace
GroundStation_Tropo_Marini_Azimuth
GroundStation_Tropo_Marini_DsnSeqRange
GroundStation_Tropo_Marini_DsnTcp
GroundStation_Tropo_Marini_Elevation
GroundStation_Tropo_Marini_L1
GroundStation_Tropo_Marini_Moon
GroundStation_Tropo_Marini_RangeRate
GroundStation_Tropo_Marini_RangeSkin
GroundStation_Tropo_Marini_Range
GroundStation_Tropo_Marini_Sun
GroundStation_Tropo_Marini_XEastYNorth_DeepSpace
GroundStation_Tropo_Marini_XEast
GroundStation_Tropo_Marini_XSouthYEast_DeepSpace
GroundStation_Tropo_Marini_XSouth
GroundStation_Tropo_Marini_YEast
GroundStation_Tropo_Marini_YNorth
GroundStation_Tropo_Moon
GroundStation_Tropo_Range2
GroundStation_Tropo_RangeRate_DeepSpace
GroundStation_Tropo_Range_DeepSpace
GroundStation_Tropo_Sun
GroundStation_Tropo_XEast
GroundStation_Tropo_XSouth
GroundStation_Tropo_YEast
GroundStation_Tropo_YNorth
KalmanFilter_OutputWarmStartFile_DSN_Sun_Cr
KalmanFilter_OutputWarmStartFile_DSN_Sun_NPlateAreaCoefficient
KalmanFilter_OutputWarmStartFile_DSN_Sun_SPADSRP
KalmanFilter_OutputWarmStartFile_DSN_Sun
KalmanFilter_OutputWarmStartFile_DSN_TSF_L1
KalmanFilter_OutputWarmStartFile_GN_Moon
KalmanFilter_OutputWarmStartFile_GpsPosVec_Cd
KalmanFilter_OutputWarmStartFile_GpsPosVec_FogmCd_FogmADSF
KalmanFilter_OutputWarmStartFile_GpsPosVec_FogmCd_RandomConstantADSF
KalmanFilter_OutputWarmStartFile_GpsPosVec_FogmCd
KalmanFilter_OutputWarmStartFile_GpsPosVec
KalmanFilter_OutputWarmStartFile_RangeSkinAzimuthElevation_Bias_Multiple
KalmanFilter_OutputWarmStartFile_RangeSkinAzimuthElevation_Bias
KalmanFilter_OutputWarmStartFile_RangeSkinAzimuthElevation_Cd_Cr_Bias
KalmanFilter_OutputWarmStartFile_RangeSkinAzimuthElevation_SPADDrag
KalmanFilter_OutputWarmStartFile_RangeSkinAzimuthElevation
KalmanFilter_OutputWarmStartFile_SN
KalmanFilter_OutputWarmStartFile_XYAngles
Optimize_fmincon_ExitMode_SaveAndContinue_2
Optimize_fmincon_ExitMode_Stop
Optimize_fmincon_SolveMode_Defaultscript
PythonArray2dReturn
PythonArrayReal
PythonFunction_Builtin
PythonFunction_Custom_DegToRad_Assignment
PythonFunction_Custom_DegToRad
PythonFunction_Custom_magic
PythonFunction_Custom
PythonRealArrayReal
PythonReal
PythonStringArrayArrayOp
PythonStringArrayArray
PythonStringRealRealOp
PythonStringRealReal
PythonStringToString
Python_NoInputs
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable
Vary_optimizer_fmincon__InitialValue_Array
Vary_optimizer_fmincon__InitialValue_Variable
Vary_optimizer_fmincon__LowerBound_RealNumber
scriptEvent_optimizer_fmincon__InitialValue_RealNumber
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_Multiple_SunEarthMoon: [GMT-7421]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\BatchEstimator_Propagator_Multiple_SunEarthMoon_SimVec.report
does not exist
BatchEstimator_Propagator_SPK_EGAPMultiple_TDRS: [GMT-7050]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\BatchEstimator_Propagator_SPK_EGAPMultiple_TDRS.txt
does not exist
BatchEstimator_Propagator_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
Matlab_NoInputs:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Matlab_NoInputs.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_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
Smoother_Filter_ProcessNoiseTimeStep_0sec_SN: [GMT-7376]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Smoother_Filter_ProcessNoiseTimeStep_0sec_SN.txt
does not exist
ThrustSegment_SolveFors_ThrustScaleFactor_SN: [GMT-7376]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\ThrustSegment_SolveFors_ThrustScaleFactor_SN.txt
does not exist
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2.report
does not exist
Vary_optimizer_fmincon_UpperBound_ArrayElement:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_UpperBound_ArrayElement.report
does not exist
Vary_optimizer_fmincon__InitialValue_RealNumber:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__InitialValue_RealNumber.report
does not exist
Vary_optimizer_fmincon__LowerBound_Array:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__LowerBound_Array.report
does not exist
Vary_optimizer_fmincon__LowerBound_Variable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__LowerBound_Variable.report
does not exist
scriptEvent_optimizer_fmincon__InitialValue_Variable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\scriptEvent_optimizer_fmincon__InitialValue_Variable.report
does not exist
Comparator errors:
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.
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_SPK_EndEarly_TDRS/BatchEstimator_Propagator_SPK_EndEarly_TDRS.log
[ptrn 1 failed] [GMT-7289]
BatchEstimator_Propagator_SPK_HasGap_TDRS/BatchEstimator_Propagator_SPK_HasGap_TDRS.log
[ptrn 1 failed] [GMT-7289]
BatchEstimator_Propagator_SPK_TDRS [ptrn 1 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 EstSat.EarthMJ2000Eq.Z error 0.006640 exceeds tolerance 0.005000]
[GMT-7483]
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_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_Multiple_MixedCentralBody [Output field
-30669344.616161 failed tolerance in record 4] [GMT-7421]
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_SharedBias [The test run
failed
to converge] [GMT-7421]
THF_Accel_CSB_None_NA []
THF_Accel_CSC_None_None []
THF_Accel_CSC_None_None_2 []
THF_AccelMass_CSB_None_None []
THF_AccelMass_CSC_None_None []
THF_AccelMass_CSC_None_None_2 []
THF_Thrust_CSB_None_NA []
THF_Thrust_CSC_None_None []
THF_ThrustMass_CSB_None_None []
THF_ThrustMass_CSC_None_None []
THF_ThrustMass_InterpolateLinear_RSSStep_ABM [diff. num. lines]
THF_ThrustMass_InterpolateLinear_RSSStep_PD45 [diff. num. lines]
THF_ThrustMass_InterpolateLinear_RSSStep_RK56 [diff. num. lines]
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]
Transponder_HardwareDelay_Sim_SnRange [ Observable Error: 4.909e-05 Km]
[GMT-7376]
Tut_MultipleShootingTutorial_Step3 [] [GMT-7280]
Vary_optimizer_fmincon_Additive_and_Multiplicative_ScaleFactor_RealNumber
[ptrn 1,2 failed]
-----------------------------------------------------------------
New Issues (Deferred)
-----------------------------------------------------------------
New truth failures (deferred):
None
Output changes (but still pass) (deferred):
Ephem_GMAT_Code500_InterpolationOrder [GMT-4075, GMT-4112]
Ephem_GMAT_Code500_InterpolationOrder [GMT-4075, 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_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]
ThrustSegment_ThrustAngle1_Cubic [diff. num. lines] [GMT-7483]
Write_Multiple_ReportFile_Concise_2 [#24 failed] [GMT-5801]
Write_Multiple_ReportFile_Verbose [#24 failed]
Write_Multiple_ReportFile_Verbose_2 [#24 failed] [GMT-5801]
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]
TrkFile_SimEst_TDRS_range_Solve_Cr [] [GMT-5416]
Vary_Validation_RHS_Field [no error or exception] [GMT-3687]
Write_Multiple_ReportFile_Concise_2 [#24 failed] [GMT-5801]
Write_Multiple_ReportFile_Verbose [#24 failed]
Write_Multiple_ReportFile_Verbose_2 [#24 failed] [GMT-5801]
-----------------------------------------------------------------
Test System Warnings
-----------------------------------------------------------------
Passing tests tagged with bugs:
(To fix, remove bug ID from Bugs key in .tc file)
Comet_Validation_OrientationEpoch_3 [GMT-3252]
CoordSysTest_Luna_MJ2000Eq_To_ICRF [GMT-3227]
CoordinateSystem_Validation_Axes_4 [GMT-3155]
EKFS_EphemerisFile_STK_IncludeCovariance_None_Moon [GMT-7398]
EKFS_EphemerisFile_STK_IncludeCovariance_None_Sun [GMT-7398]
EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Moon
[GMT-7398]
EKFS_EphemerisFile_STK_IncludeCovariance_PositionAndVelocity_Sun
[GMT-7398]
EKFS_EphemerisFile_STK_IncludeCovariance_Position_Moon [GMT-7398]
EKFS_EphemerisFile_STK_IncludeCovariance_Position_Sun [GMT-7398]
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_GN [GMT-7434-Linux]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_ColdStart
[GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_EarthFixed
[GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart
[GMT-7398]
EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr [GMT-7278-Linux]
EphemPropagator_Code500_CentralBody_Jupiter [GMT-5795]
EphemPropagator_Code500_CentralBody_Saturn [GMT-5795]
EphemPropagator_Code500_ForwardProp_Interp [GMT-5760]
EphemPropagator_SatAssigmentToNewSatThenProp [GMT-3434]
EphemStressTests_Default_Prop_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]
Simulator_Propagator_Multiple_SunEarthMoon [GMT-7421]
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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