Test results (Ubuntu).  These are run on the GMT-7781 ("multibody harmonic gravity") branch.

- DJC

--
Darrel J. Conway, Ph.D.      Thinking Systems, Inc.
Senior Scientist and CEO     437 W Thurber Road, Suite 6
Phone: (623) 298-4530        Tucson, AZ 85705
FAX:   (520) 232-2533www.thinksysinc.com
Cell:  (520)[email protected]
-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Ubuntu20.04
Tested build: Ubuntu20.04-GMAT_Console
Regression build: Ubuntu20.04Baseline

Total number of scripts: 17038 (+180 deferred)
Percent Passed: 99.70%
New issues: 0
        Output changes: 0
        New truth failures: 0
        New crashes: 0
        New script errors: 0
        New comparator errors: 0
Fixed issues: 27
Total issues: 57

Test system warnings: 22
New deferred issues: 0
Fixed deferred issues: 0
Total deferred issues: 145

Run Time: 00 hours, 42 minutes, 12 seconds

-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
        None

Output changes (but still pass):
        None

Output changes (but still fail):
        None

New crashes/hangs/etc.:
        None

New script errors:
        None

New comparator errors:
        None

-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
        BatchEstimator_ReportFile_AzimuthElevation
        BatchEstimator_ReportFile_BRTS
        BatchEstimator_ReportFile_Format
        BatchEstimator_ReportFile_GpsPosVec
        BatchEstimator_ReportFile_MultiSat_SpaceToSpace
        BatchEstimator_ReportFile_Range
        BatchEstimator_ReportFile_RangeRate
        BatchEstimator_ReportFile_RangeSkin
        BatchEstimator_ReportFile_SN
        BatchEstimator_ReportFile_XEastYNorth
        BatchEstimator_ReportFile_XSouthYEast
        BatchEstimator_ReportStyle_Concise
        BatchEstimator_ReportStyle_Debug
        BatchEstimator_ReportStyle_Normal
        BatchEstimator_ReportStyle_Verbose
        BatchEstimator_ReportStyle_Verbose_MultiSat_SpaceToSpace
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_SN_OEM [GMT-7914]
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_SN_OEM [GMT-7914]
        KalmanFilter_ReportFile
        KalmanFilter_ReportFile_DSN_Moon
        KalmanFilter_ReportFile_DSN_Sun
        KalmanFilter_ReportFile_GpsPosVec
        KalmanFilter_ReportStyle_Verbose
        Transponder_HardwareDelay_SpaceToSpace_AddHardwareOrder
        Transponder_HardwareDelay_SpaceToSpace_AddHardwareOrder
        Transponder_HardwareDelay_SpaceToSpace_AddHardwareOrder
        Transponder_HardwareDelay_SpaceToSpace_Est_AddHardwareOrder

Fixed crashes/hangs/etc.:
        None

Fixed script errors:
        None

Fixed comparator errors:
        None

-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
        *ForceModel_Validation_HarmonicGravityNearOrigin

Script errors:
        *API_Command_MatlabFunction: (API) 
        EKFS_TrackingFileSet_HORP_Est_Earth_EphProp_TDRS: [GMT-7376]
        *ForceModel_DeprecatedDragFlux_JR:
        *ForceModel_DeprecatedDragFlux_MSISE00:
        *ForceModel_DeprecatedDragFlux_MSISE86:
        *ForceModel_DeprecatedDragFlux_MSISE90:
        KalmanFilter_Propagator_OEMV2: [GMT-7943]
        *MatAPI_Command_MatlabFunction: (MatAPI) 
        TrackingFileSet_HORP_Est_Earth_EphProp_All: [GMT-7376]

Comparator errors:
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_SN_OEM_SPK_RK: 
(truth) [GMT-7376]
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_SN_OEM_SPK_RK: 
(truth) [GMT-7376]
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_SN_OEM_SPK_RK: 
(truth) [GMT-7376]

Truth failures:
        *API_ForceModelDerivatives (API)  [#2 failed]
        *BatchEstimator_ReportFile_MeasurementStatistics_UserEdit_DataType [#12 
failed]
        *BatchEstimator_ReportFile_MeasurementStatistics_UserEdit_TimeSpan [#10 
failed]
        *BatchEstimator_ReportFile_MeasurementStatistics_UserEdit_Tracker [#12 
failed]
        
*BatchEstimator_ReportFile_MeasurementStatistics_UserEdit_TrackerDataType [#12 
failed]
        *BeginFBurn_Successive_Burns []
        
*DynamicsModels_MultiHarmGrav_Enceladus_Saturn_ReportSTM/DynamicsModels_MultiHarmGrav_Enceladus_Saturn_ReportSTM_PctDiff.txt
 [Output field 5.879441 failed tolerance in record 2]
        
*DynamicsModels_MultiHarmGrav_Enceladus_Saturn_SaturnCB_ReportSTM/DynamicsModels_MultiHarmGrav_Enceladus_Saturn_SaturnCB_ReportSTM_PctDiff.txt
 [Output field 30.921627 failed tolerance in record 2]
        *DynamicsModels_MultiHarmGrav_NotAPrimaryBody [#1 failed]
        *DynamicsModels_MultiHarmGrav_Validation_MissingPrimaryBody [#1 failed]
        *EKF_ErrorModel_NoiseSigma_DSN [Variable Filter.State error 6.29782e-08 
failed tolerance 5e-08 at linear index 289]
        
EKFS_SpacecraftNavigation_LEO_TDRS_EphProp_OEM_Aqua/EKFS_SpacecraftNavigation_LEO_TDRS_EphProp_OEM_Aqua_Smoother_backfilter.txt
 [The test run failed to complete] [GMT-7914]
        
*EKFS_SpacecraftNavigation_MultiHarmGrav_EarthMoonNRHO_CAPSTONE/EKFS_SpacecraftNavigation_MultiHarmGrav_EarthMoonNRHO_CAPSTONE_Smoother.e
 [EphemerisTimePosVel failed velocity magnitude tolerance at row 5647]
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_SN_OEM/EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_SN_OEM_Smoother_backfilter.txt
 [The test run failed to complete] [GMT-7376]
        
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_SN_OEM/EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_SN_OEM_Smoother.txt
 [The test run failed to complete] [GMT-7376]
        
*EKFS_SpacecraftNavigation_Sun_DSN_STEREOA_EarthInitialState_SunFM/EKFS_SpacecraftNavigation_Sun_DSN_STEREOA_EarthInitialState_SunFM_Smoother_backfilter.txt
 [Parameter STEREO_A.EarthMJ2000Eq.X error 0.009250 exceeds tolerance 0.005000]
        
EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr/EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr_Smoother.txt
 [The test run failed to complete] [GMT-7278-Linux/Mac]
        
EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr/EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr_Smoother_backfilter.txt
 [The test run failed to complete] [GMT-7278-Linux/Mac]
        *ForceModel_Validation_Drag_DragModel_Mode [#1 failed]
        *ForceModel_Validation_SRP_SRPModel_Mode [#1 failed]
        *GMAT_PenToggleOpenGL_MiddlePenDown_FourPlots [#1 failed]
        *GroundTrackPlot_RetrogradeMotion [#1 failed]
        *GroundTrackPlot_Set_SolverIterations [#1 failed]
        *KalmanFilter_MatlabFile_DSN_Sun [Variable Filter.State error 1.74836 
failed tolerance 1e-06 at linear index 145]
        *KalmanFilter_MeasDeweightingCoefficient_DSN_Sun [Sigma-B failed at 17 
Sep 2005 00:11:00.000]
        *KalmanFilter_MeasurementUpdate_DSN_Sun [Variable Filter.State(4:6,:) 
error 1.73677e-06 failed tolerance 1e-09 at linear index 1310]
        *KalmanFilter_OutputWarmStartFile_DSN_Sun [Output field 0.038997 failed 
tolerance in record 281]
        *KalmanFilter_OutputWarmStartFile_DSN_Sun_Cr [Output field 0.002283 
failed tolerance in record 209]
        *KalmanFilter_OutputWarmStartFile_DSN_Sun_NPlateAreaCoefficient [Output 
field 9.796451 failed tolerance in record 219]
        *KalmanFilter_ProcessNoiseTimeStep_DSN_Sun [Scaled residual failed at 
17 Sep 2005 00:11:00.000]
        *Matlab_IO_String []
        *Propagate_Covariance_SNC_MultiHarmGrav_Enceladus_Saturn [Output field 
0.013717 failed tolerance in record 1]
        PythonFunction_PrintToLogFile [#2 failed] [GMT-7944]
        SchattenFile_NominalCycle_Mean_JR [pos err 75.5997, tol 0.01] [GMT-8007]
        Simulator_EarthFixedInitialState [Residual failed at 01 Mar 2005 
00:19:00.000] [GMT-7923]
        *Smoother_MeasDeweightingCoefficient_DSN_Sun [Sigma-B failed at 18 Sep 
2005 00:00:00.000]
        *Smoother_MeasDeweightingCoefficient_DSN_Sun [#578 failed]
        *Smoother_ReportFile_FogmCd_FogmADSF_GpsPosVec [#67 failed]
        *Smoother_ReportStyle_Normal [#68 failed]
        *Smoother_ReportStyle_Verbose/Smoother_ReportStyle_Verbose_Smoother.txt 
[#71 failed]
        
*Smoother_ReportStyle_Verbose/Smoother_ReportStyle_Verbose_Smoother_backfilter.txt
 [#68 failed]
        SpacecraftNavigation_LEO_TDRS_GN_Landsat7 [#1 failed] [GMT-7376]
        *SpacecraftNavigation_Multisat_CAPSTONE_LRO_Crosslink [Residual failed 
at 10 May 2023 04:02:30.000]
        *SpacecraftNavigation_Sun_DSN_STEREOB_Cr [Parameter 
STEREO_B.SunMJ2000Eq.X error 0.011097 exceeds tolerance 0.001000]

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

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

Output changes (but still fail) (deferred):
        None

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]
        
EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_DuringEstimationArc_CCSDS
 [GMT-7483]
        
EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_DuringEstimationArc_SPICE
 [GMT-7483]
        EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_SPICE [GMT-7633]
        EKFS_ErrorModel_SolveFors_PassBiases_GN
        EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_SN [GMT-7376]
        EKF_SpacecraftNavigation_OrbitErrorCovariance_Keplerian_GpsPosVec 
[GMT-7785]
        EKF_SpacecraftNavigation_SolveFors_KeplerianState_Cd_RandomConstant_GN 
[GMT-7785]
        EKF_SpacecraftNavigation_SolveFors_KeplerianState_Cr_RandomConstant_DSN 
[GMT-7785]
        EKF_SpacecraftNavigation_SolveFors_KeplerianState_GN [GMT-7785]
        EKF_SpacecraftNavigation_SolveFors_KeplerianState_GpsPosVec [GMT-7785]
        Events_ContactLocator_ReportColumnsInOrder_Observer_Multiple_Many
        Events_ContactLocator_ReportColumnsInOrder_Observer_Multiple
        
Events_ContactLocator_ReportFormat_AzimuthElevationRangeReport_CeresBase 
[GMT-7784]
        Events_ContactLocator_ReportFormat_Legacy_CeresBase [GMT-7843]
        Events_ContactLocator_StationMasking_CeresBase [GMT-7784]
        KalmanFilter_InputWarmStartFile_GN_Moon_Keplerian [GMT-7785]
        KalmanFilter_InputWarmStartFile_GpsPosVec_KeplerianToCartesian 
[GMT-7785]
        KalmanFilter_OutputWarmStartFile_GpsPosVec_Keplerian [GMT-7785]
        KalmanFilter_Propagator_SN
        KalmanFilter_Propagator_SPK_TDRS_Multiple
        KalmanFilter_Propagator_SPK_TDRS
        KalmanFilter_Propagator_STK_TDRS_Multiple
        KalmanFilter_Propagator_STK_TDRS
        KalmanFilter_Smoother_PredictTimeSpan_Both_OEM [GMT-6949]
        MatAPI_PrecessingSpinner (MatAPI)  [GMT-7595]
        Math_Shadowed_Builtins [GMT-3043]
        OCPropTest_SPAD_Drag_1deg_Bicubic_LEO [GMT-7147]
        OCPropTest_SPAD_Drag_SRP_1deg_Bicubic_LEO [GMT-7147]
        SPICESGP4Propagator_60sec_Propagation_TDRS
        SPICESGP4Propagator_DaysBeforeTLE_Propagation_TDRS
        SPICESGP4Propagator_MonthsAfterTLE_Propagation_TDRS
        SPICESGP4Propagator_MonthsBeforeTLE_Propagation_TDRS
        ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522]
        SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn
        SpacecraftNavigation_SolveFors_CartesianState_SnDowd
        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]
        TLEWriter_CreateTLEFromSTKEphemeris_ISS [GMT-7677]
        TLEWriter_CreateTLEFromSTKEphemeris_MMS [GMT-7677]
        TLEWriter_CreateTLEFromSTKEphemeris_MOLNIYA [GMT-7677]
        TLEWriter_CreateTLEFromSTKEphemeris_TDRS [GMT-7677]
        TLEWriter_CreateTLEFromSTKEphemeris_TERRA [GMT-7677]
        TLEWriter_Validation_InvalidClassification_InvalidString [GMT-7677]
        TLEWriter_Validation_ValidDesignator_OneCharacter
        
ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_EpochAfterBurn_GpsPosVec 
[GMT-7633]
        ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_GpsPosVec 
[GMT-7633]
        
ThrustSegment_SolveFors_ThrustAngles_Constant_ThreeAxisKinematic_EpochAfterBurn_GpsPosVec
 [GMT-7633]
        
ThrustSegment_SolveFors_ThrustAngles_Linear_ThreeAxisKinematic_GpsPosVec 
[GMT-7633]
        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):
        None

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]
        API_PrecessingSpinner (API)  [#1 failed] [GMT-7595]
        BatchEstimator_NormalMatrixReduction_UseInitialCovariance [#1 failed] 
[GMT-7274]
        EKFS_EphemerisFile_FiniteBurnTHF_DuringEstimationArc_CCSDS_Disallowed 
[#1 failed]
        EKFS_EphemerisFile_FiniteBurnTHF_DuringEstimationArc_SPICE_Disallowed 
[#1 failed]
        
EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_DuringEstimationArc_STK/EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_DuringEstimationArc_STK_Smoother.e
 [Unable to read STK ephemeris 
/home/buildbot/gmattest/output/Ubuntu20.04-GMAT_Console/Resources/FRR-31_EphemerisFile/script/EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_DuringEstimationArc_STK_Smoother.e]
 [GMT-7483]
        
EKFS_ErrorModel_SolveFors_Bias_SnDoppler_EphProp_SPK/EKFS_ErrorModel_SolveFors_Bias_SnDoppler_EphProp_SPK_smoother.txt
 [The test run failed to complete] [GMT-7376]
        
EKFS_ErrorModel_SolveFors_Bias_SnRange_EphProp_SPK/EKFS_ErrorModel_SolveFors_Bias_SnRange_EphProp_SPK_smoother.txt
 [The test run failed to complete] [GMT-7376]
        
EKFS_ErrorModel_SolveFors_Bias_SnRangeSnDoppler_EphProp_SPK/EKFS_ErrorModel_SolveFors_Bias_SnRangeSnDoppler_EphProp_SPK_smoother.txt
 [The test run failed to complete] [GMT-7376]
        
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 0.000964 failed tolerance in record 919] [GMT-7291, GMT-7398]
        EKFS_SpacecraftNavigation_MultiSat_DifferentInitialEpochs [#1 failed] 
[GMT-7421]
        EKFS_SpacecraftNavigation_MultiSat_TdrsAndUser_DifferentProcessNoise [0 
truth states are present but 12 tolerances were provided] [GMT-7421]
        
Ephem_GMAT_Code500_InterpolationOrder/Ephem_GMAT_Code500_InterpolationOrder_1.eph
 [pos err 0.0177967, 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 
305.166, tol 0.002] [GMT-4112]
        EphemerisFile_OEM_CoordinateSystem_ObjectReferenced_LeapSecond [pos and 
vel interp err : 0.00018929 , 0.0001] [GMT-7877]
        EphemerisFile_OEM_Earth_ICRF_LeapSecond [pos and vel interp err : 
7.6013 , 0.0083853] [GMT-7877]
        EphemerisFile_OEM_Earth_MJ2000Ec_LeapSecond [pos and vel interp err : 
7.6034 , 0.0083832] [GMT-7877]
        
EphemPropagator_STK_CentralBody_Moon_ME/EphemPropagator_STK_CentralBody_Moon_ME_BodyJ2000Rpt.txt
 [pos err 138.57, tol 1e-06] [GMT-7604]
        
EphemPropagator_STK_CentralBody_Moon_ME/EphemPropagator_STK_CentralBody_Moon_ME_EarthJ2000Rpt.txt
 [pos err 138.57, tol 5e-05] [GMT-7604]
        
EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection
 [pos err 15.2492, 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 14.3905, tol 1e-12] [GMT-4077]
        
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
 [pos err 0.000206179, 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 
0.000421243, 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]
        Events_ContactLocator_IntervalStepSize_0sec [#2 failed]
        
Events_ContactLocator_ReportFormat_AzimuthElevationRangeReport_AzElMask_RST [#4 
failed] [GMT-7772]
        
Events_ContactLocator_ReportFormat_SiteViewMaxElevationReport_AzElMask_RST [#4 
failed] [GMT-7772]
        Events_ContactLocator_StationMasking_Multiple_Many [start diff = 
13.082005s (event 542)] [GMT-7614]
        Formation_Validation_MissingComma [no error or exception] [GMT-3672]
        GMAT_ISS_Earth_JGM2_0_0_NutationUpdateInterval [pos err 0.000809869, 
tol 1e-06] [GMT-2567]
        GMAT_LEO_PropSynchronization_BS []
        GMAT_LunarTran_PropSynchronization_BS [max diff 1.33129e-07 > tol 5e-08]
        GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS [pos err 0.0764667, 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]
        KalmanFilter_InputWarmStartFile_SN [Output field -4638.170949 failed 
tolerance in record 1] [GMT-7376]
        KalmanFilter_MatlabFile_GN_Moon [Variable EstimationConfig.StateNames 
did not match at index 1] [GMT-6801]
        KalmanFilter_Propagator_Multiple_MixedCentralBody [Observed measurement 
failed at 10 Jun 2010 00:40:00.000] [GMT-7421]
        KalmanFilter_Propagator_Multiple_NonParticipatingSpacecraft [ptrn 1 
failed] [GMT-7421]
        KalmanFilter_Propagator_Multiple_SpacecraftDoesNotExist [ptrn 1 failed] 
[GMT-7421]
        KalmanFilter_Propagator_Multiple_SunEarthMoon [Observed measurement 
failed at 10 Jun 2010 00:00:00.000] [GMT-7421]
        KalmanFilter_Propagator_Multiple_UnassignedSpacecraft [ptrn 1 failed] 
[GMT-7421]
        KalmanFilter_WarmStartEpoch_SN [Output field -4638.170949 failed 
tolerance in record 1] [GMT-7376]
        MatAPI_Epoch_LeapSecond_In (MatAPI)  [#7 failed] [2561]
        MatAPI_Epoch_LeapSecond_Out (MatAPI)  [#7 failed] [2561]
        Math_Inf [GMAT: 53 lines, Truth: 69 lines] [GMT-3195]
        Minimize_Validation_Field [ptrn 1 failed] [GMT-3687]
        Nonlinear_Validation_LHS_Field [ptrn 1 failed] [GMT-3687]
        Nonlinear_Validation_RHS_Field [ptrn 1 failed] [GMT-3687]
        Optimize_Yukon_Minimize_Height_on_circle_2 [diff 497, tol 0.001] 
[GMT-6434]
        Optimize_Yukon_Minimize_Height_on_circle_4 [diff 497, tol 0.001] 
[GMT-6434]
        Plate_Validation_PlateNormalHistoryFile [#1 failed] [GMT-7022]
        RejectFilter_Validation_RecordNumbers [#5 failed] [GMT-6034]
        RotationMatrixTest_MercuryMJ2000Ec [max diff 1.09735e-09 > tol 1e-12] 
[GMT-7223]
        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]
        Simulator_Propagator_OEM_MoonMJ2000Eq_GN [Residual failed at 10 Jun 
2011 04:00:00.000] [GMT-7768]
        Simulator_Propagator_SPK_MoonOccultation [#66 failed] [GMT-7768]
        Simulator_Propagator_SPK_MultipleOccultation [#1 failed] [GMT-7768]
        Simulator_Propagator_SPK_TDRS [Residual failed at 01 Mar 2005 
01:00:00.000] [GMT-7289]
        Simulator_Propagator_STK_TDRS [Residual failed at 01 Mar 2005 
01:00:00.000] [GMT-7289]
        Smoother_MatlabFile_BackfilterMatfileCorruption [Found extra field 
BackwardComputed] [GMT-6949]
        Smoother_PredictTimeSpan_STK_SN [Test ScenarioEpoch does not match 
truth ScenarioEpoch] [GMT-7376]
        SpacecraftNavigation_LEO_TDRS_EphProp_OEM_LeapSec_Terra [Residual 
failed at 31 Dec 2016 23:55:00.000] [GMT-7598]
        SpacecraftNavigation_MultiSat_J2000_EarthFixed [Residual failed at 01 
Mar 2005 01:00:00.000] [GMT-7421]
        SpacecraftNavigation_SimEphProp_MixedInitialFrame_TDRS [Residual failed 
at 01 Mar 2005 01:20:00.000] [GMT-7289]
        SPICESGP4Propagator_EarthIntersection [#1 failed] [GMT-7584]
        SPICESGP4Propagator_LeapSecond_Propagation_v1 [GMAT: 289 lines, Truth: 
290 lines]
        StartupFile_DoesNotExist [#1 failed] [GMT-7802]
        StopCond_GMAT_MoonSPK_ParamBattery [] [GMT-7829]
        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_2 [#24 failed] [GMT-5801]

-----------------------------------------------------------------
Test System Warnings
-----------------------------------------------------------------
Passing tests tagged with bugs:
        (To fix, remove bug ID from Bugs key in .tc file)
        EKFS_ErrorModel_SolveFors_Bias_SnDoppler_EphProp_OEM [GMT-7641]
        EKFS_ErrorModel_SolveFors_Bias_SnRangeSnDoppler_EphProp_STK [GMT-7376]
        EKFS_ErrorModel_SolveFors_Bias_SnRange_EphProp_STK [GMT-7376]
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_SN_OEM [GMT-7914]
        EKFS_SpacecraftNavigation_SolveFors_CartesianState_SN_OEM [GMT-7914]
        EphemPropagator_Code500_CentralBody_Jupiter [GMT-5795]
        EphemPropagator_Code500_CentralBody_Saturn [GMT-5795]
        EphemPropagator_Code500_ForwardProp_Interp [GMT-5760]
        EphemPropagator_OEM_CentralBody_Earth_MJ2000Eq_BackProp [GMT-7598]
        Events_ContactLocator_StationMasking_MultipleFOV [Save]
        ForceModel_SPAD_Drag_1deg_Bicubic_Mars [Linux, Mac]
        ForceModel_SPAD_Drag_1deg_Bilinear_Mars [Linux, Mac]
        IntegratedFlyby_MarsFlyby [GMT-7169]
        MatAPI_PD45PropagationE8x8SMPM [GMT-7755]
        Python_IO_String [5317]
        ScriptLanguage_LineContinuation_BeginningOfLine [GMT-3756]
        Simulator_Propagator_EarthPointMass_Drag [GMT-5417]
        SpacecraftNavigation_SPADDragScaleFactorSigma_ConstrainInc [GMT-7078, 
Ubuntu only]
        ThrustHistoryFile_EstimateTSF_EpochBeforeBurn_RSSStep_Aqua [GMT-6451]
        Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
        TrackingFileSet_HORP_Sim_Earth_EphProp_All [GMT-7598]
        Tut_MultipleShootingTutorial_Step3 [GMT-7280]
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