Test results (Ubuntu).
- 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)425-3626darrel.con...@thinksysinc.com
-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Ubuntu20.04
Tested build: Ubuntu20.04-GMAT_Console
Regression build: Ubuntu20.04Baseline
Total number of scripts: 16622 (+136 deferred)
Percent Passed: 99.14%
New issues: 1
Output changes: 0
New truth failures: 0
New crashes: 0
New script errors: 1
New comparator errors: 0
Fixed issues: 9
Total issues: 150
Test system warnings: 53
New deferred issues: 1
Fixed deferred issues: 0
Total deferred issues: 112
Run Time: 23 hours, 25 minutes, 39 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:
EphemPropagator_OEM_Earth_GRC_60sec
New comparator errors:
None
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
API_ShowObjects (API)
EKF_EphemerisFile_Code500_Disallowed
EKFS_SpacecraftNavigation_OrbitErrorCovariance_GN_Moon
EphemPropagator_OEM_CentralBody_Jupiter_MJ2000Eq
EphemPropagator_OEM_CentralBody_Jupiter_MJ2000Eq
EphemPropagator_OEM_CentralBody_Jupiter_MJ2000Eq
PlanetographicRegion_Validation_WrongCentralBody
Fixed crashes/hangs/etc.:
None
Fixed script errors:
EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_SPICE
MatAPI_ForceModelDerivatives (MatAPI)
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
None
Script errors:
*ContactLocator_PlanetoRegion_EOSLATarea_File:
*ContactLocator_PlanetoRegion_FermiGBMarea_File:
*ContactLocator_PlanetoRegion_FermiLATarea_File:
*ContactLocator_PlanetoRegion_FermiMultiArea2_1A1F:
*ContactLocator_PlanetoRegion_FermiMultiArea2_2F:
ContactLocator_PlanetoRegion_TDRSLATarea_File: [GMT-7699]
*CustomFOV_FOVFileName_AzimuthElevationAngles:
*CustomFOV_FOVFileName_StkFormatMask:
*EphemPropagator_OEM_Earth_GRC_60sec:
*EphemPropagator_SPK_CentralBody_Moon_PA:
*Events_ContactLocator_IntervalStepSize_60sec:
Events_ContactLocator_ReportFormat_AzimuthElevationRangeReport_CeresBase:
[GMT-7614]
*Events_ContactLocator_ReportFormat_AzimuthElevationRangeReport_MarsBase:
*Events_ContactLocator_ReportFormat_AzimuthElevationRangeReport_MoonBase:
*Events_ContactLocator_ReportFormat_AzimuthElevationRangeReport:
*Events_ContactLocator_ReportFormat_Legacy:
*Events_ContactLocator_ReportFormat_SiteViewMaxElevationReport:
*Events_ContactLocator_StationMaskingAndMinimumElevation:
Events_ContactLocator_StationMasking_CeresBase: [GMT-7614]
*Events_ContactLocator_StationMasking_CustomFOVIsNotClosed:
*Events_ContactLocator_StationMasking_Lunar:
*Events_ContactLocator_StationMasking_MarsBase:
*Events_ContactLocator_StationMasking_MaskFileIsNotClosed:
*Events_ContactLocator_StationMasking_MoonBase:
*Events_ContactLocator_StationMasking_MultipleFOV:
Events_ContactLocator_StationMasking_Multiple_Many: [GMT-7614]
Events_ContactLocator_StationMasking_OEMEphemeris_Lunar: [GMT-7614]
Events_ContactLocator_StationMasking_OEMEphemeris_Mars: [GMT-7614]
*Events_ContactLocator_StationMasking_OEMEphemeris:
*Events_ContactLocator_StationMasking_RunMode_Disabled:
Events_ContactLocator_StationMasking_RunMode_Manual_Append: [GMT-7614]
*Events_ContactLocator_StationMasking_RunMode_Manual:
*Events_ContactLocator_StationMasking_STKEphemeris_Earth_TOD:
*Events_ContactLocator_StationMasking_STKEphemeris_Lunar:
*Events_ContactLocator_StationMasking_STKEphemeris:
*Events_ContactLocator_StationMasking:
*FMParams_AngularMomentum_AttitudeType_CCSDS-AEM:
*FMParams_AngularMomentum_AttitudeType_NadirPointing:
*FMParams_AngularMomentum_AttitudeType_PrecessingSpinner:
*FMParams_AngularMomentum_AttitudeType_SpiceAttitude:
*FMParams_AngularMomentum_AttitudeType_Spinner:
*FMParams_AngularMomentum_Calculation:
*FMParams_BurnTorque_OffsetCM:
*GroundStation_HorizonMaskFileName_FormatCompressed:
*GroundStation_HorizonMaskFileName_FormatTabbed:
*GroundStation_HorizonMaskFileName_MacLineEndings:
*GroundStation_HorizonMaskFileName_MoonBase:
*GroundStation_HorizonMaskFileName_StkFormat:
*GroundStation_HorizonMaskFileName_UnixLineEndings:
*GroundStation_HorizonMaskFileName:
*LookupTable_InterpRange_Both_Lower_03:
MatAPI_PrecessingSpinner: (MatAPI) [GMT-7595]
OrbitTime_Collinearity_Angle_LibrationPoint: [GMT-7621]
Comparator errors:
*CustomFOV_FOVFileName_ClockConeAngles: (truth)
Truth failures:
API_PrecessingSpinner (API) [#1 failed] [GMT-7595]
*BatchEstimator_ReportStyle_Verbose_MultiSat_SpaceToSpace [#177 failed]
ContactLocator_PlanetoRegion_TDRSdatelineArea [start diff = 1.783002s
(event 3)] [GMT-7699]
*CustomFOV_El_GreaterThan90 [#3 failed]
*CustomFOV_InterpolationStepSize_1deg [diff # events]
*EKFS_EphemerisFile_STK_PredDv/EKFS_EphemerisFile_STK_PredDv_Filter.e
[CovarianceTimePos failed tolerance at row 30613]
*EKFS_EphemerisFile_STK_PredDv/EKFS_EphemerisFile_STK_PredDv_Smoother.e
[CovarianceTimePos failed tolerance at row 30613]
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_GN/EKFS_ErrorModel_SolveFors_Bias_RandomConstant_GN_Smoother_backfilter.txt
[Parameter EstMAD.EstSat_EstRangeModel.Bias error 0.118112 exceeds tolerance
0.020000] [GMT-7434-Linux]
*EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_Filter.e
[CovarianceTimePos failed tolerance at row 17343]
*EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_Smoother.e
[CovarianceTimePos failed tolerance at row 17350]
*EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_SmoEph/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_SmoEph_Smoother.e
[CovarianceTimePos failed tolerance at row 17350]
*EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_PropagateCovariance/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_PropagateCovariance_Filter.e
[CovarianceTimePosVel failed tolerance at row 2400]
*EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_PropagateCovariance/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_PropagateCovariance_Smoother.e
[CovarianceTimePosVel failed tolerance at row 162936]
*EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantADSF_GN/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantADSF_GN_FPS_backfilter.txt
[Sigma-B failed at 10 Jun 2010 04:12:00.000]
*EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantADSF_GN/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantADSF_GN_FPS.mat
[Covariance comparison failed tolerance at 11 of 12 significant digits at
index (6,2,162)]
*EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantBias_DSN/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantBias_DSN_FPS_backfilter.txt
[Sigma-V failed at 10 Jun 2012 12:29:00.000]
*EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantBias_DSN/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantBias_DSN_FPS.mat
[Covariance comparison failed tolerance at 13 of 14 significant digits at
index (8,2,589)]
*EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantCd_GN/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantCd_GN_FPS_backfilter.txt
[Sigma-B failed at 10 Jun 2010 04:12:00.000]
*EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantCd_GN/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantCd_GN_FPS.mat
[Covariance comparison failed tolerance at 13 of 14 significant digits at
index (4,4,173)]
*EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantSPADDrag_GN/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantSPADDrag_GN_FPS.mat
[Covariance comparison failed tolerance at 13 of 14 significant digits at
index (6,2,173)]
*EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantTSF_DSN/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantTSF_DSN_FPS.mat
[Covariance comparison failed tolerance at 8 of 14 significant digits at index
(7,6,349)]
*EKFS_SpacecraftNavigation_PropagateCovariance_SNC/EKFS_SpacecraftNavigation_PropagateCovariance_SNC_Filter.txt
[max diff 6.52846e-05 > tol 1e-06]
EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr/EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr_Smoother_backfilter.txt
[Parameter STEREO_B.SunMJ2000Eq.X error 0.177174 exceeds tolerance 0.015000]
[GMT-7278-Linux]
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 14.780763 exceeds
tolerance 0.005000] [GMT-7483]
*EphemerisFile_STK_LeapSecond_2d_60sec [EphemerisTimePosVel failed
velocity magnitude tolerance at row 2]
EphemPropagator_OEM_Earth_ICRF_60sec [pos err 0.00181204, tol 1.2e-05]
[GMT-7563]
*Events_ContactLocator_StationMasking_DeepSpace [diff # events]
*Events_ContactLocator_StationMasking_DeepSpace_LightTimeDirection_Transmit
[diff # events]
*Events_ContactLocator_StationMasking_DeepSpace_UseLightTimeDelay_False
[diff # events]
*Events_ContactLocator_StationMasking_DeepSpace_UseStellarAberration_False
[diff # events]
Events_IntrusionLocator_RunMode_Automatic [#1 failed] [GMT-7739]
Events_IntrusionLocator_SingleIntrudingBody_LightTimeDelay_StellarAberration
[diff # events] [GMT-7739]
Events_IntrusionLocator_SingleIntrudingBody_MultipleSensors_FixedGrid
[diff # events] [GMT-7739]
Events_IntrusionLocator_Validation_CentralBody_MatchesIntruding_Mars
[no error or exception] [GMT-7739]
Events_IntrusionLocator_Validation_CustomFOV_AzimuthElevation [no error
or exception] [GMT-7739]
*FMParams_BurnTorque_ChangingThrust [max diff 1.42219e-07 > tol 1e-12]
*FMParams_BurnTorque_ElectricThruster [max diff 5.16489e-12 > tol 1e-12]
*FMParams_GravityTorque_Earth [max diff 1.91197e-06 > tol 1e-12]
*FMParams_GravityTorque_Earth_MOITable [max diff 1.91197e-06 > tol
1e-12]
*FMParams_GravityTorque_EarthWithPointMasses [max diff 1.28095e-06 >
tol 1e-12]
*FMParams_GravityTorque_Mars [max diff 1.87411e-08 > tol 1e-12]
*FMParams_SRPTorque_InEarthsShadow [max diff 1.52434e-07 > tol 1e-12]
*FMParams_SRPTorque_PlateNotFacingSun [max diff 5.04812e-11 > tol 1e-12]
*FMParams_TotalTorque_CMTables [diff. num elements]
*GOES_NSSK_Target_Inclination_And_RAAN/GOES_NSSK_Target_Inclination_And_RAAN_Data.txt
[Output field 308.760004 failed tolerance in record 2]
*GroundStation_Validation_CentralBody [#1 failed]
*GroundStation_Validation_HorizonMaskFileName [#7 failed]
*KalmanFilter_InputWarmStartFile_RangeSkinAzimuthElevation_SPADDrag
[Output field -4.546907 failed tolerance in record 1]
*KalmanFilter_OutputWarmStartFile_GN_Moon [Output field -0.032253
failed tolerance in record 506]
*KalmanFilter_OutputWarmStartFile_GpsPosVec_FogmCd [Output field
0.174298 failed tolerance in record 202]
MatAPI_Epoch_LeapSecond_In (MatAPI) [#7 failed] [2561]
MatAPI_Epoch_LeapSecond_Out (MatAPI) [#7 failed] [2561]
MatAPI_LoadAndRunScript (MatAPI) [#2 failed] [GMT-7755]
MatAPI_MJ2000Ec (MatAPI) [#6 failed] [GMT-7755]
MatAPI_MJ2000Eq (MatAPI) [#7 failed] [GMT-7755]
MatAPI_ScriptTest (MatAPI) [#1 failed] [GMT-7738]
*Matlab_IO_String []
OrbitTime_Collinearity_Angle_Barycenter [max diff 0.000742891 > tol
1e-07] [GMT-7621]
*OrbitTime_Collinearity_Angle_ScStationSc [max diff 0.00334597 > tol 0]
*OrbitTime_Collinearity_Angle_SunStationSc [max diff 1.31486e-05 > tol
0]
*OREx_Outbound_Cruise_Optimization_With_Global_Subscribers_And_Objects
[diff 0.000776695, tol 0.00075]
*PlanetographicRegion_Validation_FileRead [#1 failed]
Plate_Validation_PlateNormalHistoryFile [#1 failed] [GMT-7022]
*ProcessNoiseModel_Validation_UpdateTimeStep [#8 failed]
*Propagate_Covariance_FilterSmoother_Ephemeris_STK_CovPositionVelocity/Propagate_Covariance_FilterSmoother_Ephemeris_STK_CovPositionVelocity_Filter.e
[CovarianceTimePosVel failed tolerance at row 33205]
*Propagate_Covariance_FilterSmoother_Ephemeris_STK_CovPositionVelocity/Propagate_Covariance_FilterSmoother_Ephemeris_STK_CovPositionVelocity_Smoother.e
[CovarianceTimePosVel failed tolerance at row 32850]
*Propagate_Covariance_SNC_EarthMJ2000Eq_EarthFull [max diff 6.99953e-05
> tol 1e-06]
*Propagate_Covariance_SNC_MoonMJ2000Eq_MoonFull [max diff 3.98449e-06 >
tol 1e-06]
*Propagate_Covariance_SNC_None_EarthFull [max diff 4.61422e-08 > tol
1e-10]
*Propagate_Covariance_SNC_None_Formation_Disallowed [#3 failed]
*Propagate_Covariance_SNC_None_MoonFull [max diff 1.7825e-10 > tol
1e-10]
RotationMatrixTest_MercuryMJ2000Ec [max diff 1.09735e-09 > tol 1e-12]
[GMT-7223]
Simulator_Propagator_OEM_MoonMJ2000Eq_GN [Residual failed at 10 Jun
2011 04:00:00.000] [GMT-7289]
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_STK_TDRS [Residual failed at 01 Mar 2005
01:00:00.000] [GMT-7289]
*Smoother_AddPredictToMatlabFile_NPlateCoefs_DSN [Variable
Smoother.State(9,:) error 6.23964e-06 failed tolerance 1e-06 at linear index 7]
*Smoother_DelayRectifyTimeSpan_RangeSkinAzimuthElevation_Sun [Scaled
residual failed at 10 Jun 2010 19:20:00.000]
*Smoother_Filter_FogmCd_FogmADSF_GpsPosVec [Covariance comparison
failed tolerance at 7 of 8 significant digits at index (2,2,360)]
*Smoother_Filter_FogmCd_GpsPosVec [Covariance comparison failed
tolerance at 7 of 8 significant digits at index (7,3,357)]
*Smoother_Filter_ProcessNoiseTimeStep_0sec_SN [Sigma-V failed at 01 Mar
2005 22:05:00.000]
Smoother_MatlabFile_BackfilterMatfileCorruption [Found extra field
BackwardComputed] [GMT-6949]
*Smoother_TimeUpdate_GpsPosVec [Variable Smoother.Covariance error
1.51936e-07 failed tolerance 4e-08 at linear index 13715]
Spacecraft_Validation_AddPlates [#1 failed] [GMT-7022]
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_PropagateCovariance_SNC/SpacecraftNavigation_PropagateCovariance_SNC.txt
[max diff 0.000760518 > tol 1e-06]
SpacecraftNavigation_SimEphProp_MixedInitialFrame_TDRS [Residual failed
at 01 Mar 2005 01:20:00.000] [GMT-7289]
SpacecraftNavigation_SPADSRPScaleFactorSigma_ConstrainInc [#3 failed]
[GMT-7078, Linux only]
*SpacecraftNavigation_WriteEstimatedOrbitErrorCovariance [max diff
3.66077e-10 > tol 1e-10]
*StopCond_GMAT_MoonSPK_ParamBattery []
*THF_Validation_EndThrustMissing [#1 failed]
*THF_Validation_InvalidRecordData [#1 failed]
*ThrustSegment_SolveFors_ThrustAngles_SN [Parameter
EstSat.EarthMJ2000Eq.VZ error 0.000002 exceeds tolerance 0.000001]
Tut_MultipleShootingTutorial_Step3 [] [GMT-7280]
-----------------------------------------------------------------
New Issues (Deferred)
-----------------------------------------------------------------
New truth failures (deferred):
TrkFile_SimEst_TDRS_range_Solve_Cr [] [GMT-5416]
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_SpacecraftNavigation_LEO_TDRS_Aqua_FogmCd [GMT-7376]
EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_SN [GMT-7376]
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
Events_ContactLocator_IntervalStepSize_0sec
Events_ContactLocator_ReportColumnsInOrder_Observer_Multiple_Many
Events_ContactLocator_ReportColumnsInOrder_Observer_Multiple
KalmanFilter_InputWarmStartFile_GN_Moon_Keplerian [GMT-6801]
KalmanFilter_InputWarmStartFile_GpsPosVec_KeplerianToCartesian
[GMT-6801]
KalmanFilter_OutputWarmStartFile_GpsPosVec_Keplerian [GMT-6801]
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]
Math_Shadowed_Builtins [GMT-3043]
OCPropTest_SPAD_Drag_1deg_Bicubic_LEO [GMT-7147]
OCPropTest_SPAD_Drag_SRP_1deg_Bicubic_LEO [GMT-7147]
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_ThrustAngles_Constant_Spinner_EpochAfterBurn_GpsPosVec
[GMT-7633]
ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_GpsPosVec
ThrustSegment_SolveFors_ThrustAngles_Constant_ThreeAxisKinematic_EpochAfterBurn_GpsPosVec
[GMT-7633]
ThrustSegment_SolveFors_ThrustAngles_Linear_ThreeAxisKinematic_GpsPosVec
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_Propagator_OEM_TDRS_Multiple_EarthFixed [Parameter
EstSat.EarthMJ2000Eq.X error 0.093592 exceeds tolerance 0.005000] [GMT-7598]
BatchEstimator_Propagator_STK_TDRS_Multiple_EarthFixed [Parameter
EstSat.EarthMJ2000Eq.X error 0.099521 exceeds tolerance 0.005000] [GMT-7289]
BatchEstimator_ReportFile_InitialState [#1 failed]
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/jazz/test/script/output/Ubuntu20.04-GMAT_Console/Resources/FRR-31_EphemerisFile/script/EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_DuringEstimationArc_STK_Smoother.e]
[GMT-7483]
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]
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]
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]
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]
KalmanFilter_Propagator_Multiple_SpacecraftDoesNotExist [ptrn 1 failed]
KalmanFilter_Propagator_Multiple_SunEarthMoon [Observed measurement
failed at 10 Jun 2010 00:00:00.000] [GMT-7421]
KalmanFilter_Propagator_Multiple_UnassignedSpacecraft [ptrn 1 failed]
KalmanFilter_WarmStartEpoch_SN [Output field -4638.170949 failed
tolerance in record 1] [GMT-7376]
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]
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]
Smoother_PredictTimeSpan_STK_SN [Test ScenarioEpoch does not match
truth ScenarioEpoch] [GMT-7376]
SpacecraftNavigation_Validation_Mode [#1 failed] [GMT-5841]
String_AssignNumericParam [] [GMT-2888]
ThrustSegment_ThrustAngle1_Cubic [diff. num. lines] [GMT-7483]
TrackingFileSet_InconsistentSpacecraftState [Output field
-1254560.770370 failed tolerance in record 1] [GMT-7553]
TrkFile_SimEst_TDRS_range_Solve_Cr [] [GMT-5416]
Vary_Validation_RHS_Field [no error or exception] [GMT-3687]
Write_Multiple_ReportFile_Concise_2 [#24 failed] [GMT-5801]
Write_Multiple_ReportFile_Verbose [#24 failed]
Write_Multiple_ReportFile_Verbose_2 [#24 failed] [GMT-5801]
-----------------------------------------------------------------
Test System Warnings
-----------------------------------------------------------------
Passing tests tagged with bugs:
(To fix, remove bug ID from Bugs key in .tc file)
API_ScriptFunctions [GMT-7755]
API_ScriptTest [GMT-7738]
BatchEstimator_Propagator_OEM_EarthICRF_GN [GMT-7598]
CoordSysTest_Luna_MJ2000Eq_To_ICRF [GMT-3227]
CoordinateSystem_Validation_Axes_4 [GMT-3155]
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]
EphemPropagator_OEM_Usable_Start_Stop [GMT-7563]
EphemPropagator_STK_CentralBody_Sun_Fixed [GMT-7594]
EphemPropagator_SatAssigmentToNewSatThenProp [GMT-3434]
EphemStressTests_Default_Prop_STK_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection
[GMT-6090]
EphemStressTests_Default_Prop_STK_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect
[GMT-6090]
Ephem_GMAT_SPK_60sec_backward [GMT-5286]
Ephem_GMAT_SPK_DefaultIntegrationStep_User_Defined_LagrangeOrder
[GMT-5286]
Ephem_GMAT_STK_60sec_IterativeProcess_Optimizer [GMT-6090]
Ephem_GMAT_STK_60sec_IterativeProcess_Optimizer_NoBoundaries [GMT-6090]
Events_ContactLocator_Ephemeris_DE405AllPlanets [GMT-5377]
Events_ContactLocator_Ephemeris_DE424AllPlanets [GMT-5377]
Events_ContactLocator_Heo2 [GMT-5302]
Events_ContactLocator_UseEntireInterval_False_MissionSequence [GMT-5292]
Events_IntrusionLocator_CentralBody_Luna [GMT-7739]
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]
MatAPI_Functions [GMT-7597]
MatAPI_PD45PropagationE8x8SMPM [GMT-7755]
MatAPI_ScriptFunctions [GMT-7755]
Math_Validation_Cross_WrongDim2 [GMT-5676]
Phase_EpochFormat_TAIGregorian [GMT-7168]
Phase_Type_Radau [GMT-7168]
Python_IO_String [5317]
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_SolveFors_CartesianState_SPADDragScaleFactor_GN_MSISE86
[GMT-6829 Linux only]
Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
TrackingFileSet_HORP_Sim_Earth_EphProp_All [GMT-7598]
Write_Spacecraft_NavigationHardware [GMT-7578]
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