Test results (Red Hat 8 and Ubuntu 24.04). Optimal Control tests are
disabled in this run on RH. This is the RST January 2025 release run.
Note: Tests are current (as of 1/17). Ignore failures related to
multibody gravity. On first glance, I don't see anything concerning
(but I do need to take a second glance still). If all agree, I'll
package this build for SpaceX as well.
- 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) 232-2533 www.thinksysinc.com
Cell: (520)425-3626 [email protected]
-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: RedHatEnterprise8
Tested build: RedHatEnterprise8-GMAT_Console
Regression build: RedHatEnterprise8Baseline
Total number of scripts: 17730 (+225 deferred)
Percent Passed: 98.99%
New issues: 52
Output changes: 0
New truth failures: 27
New crashes: 0
New script errors: 25
New comparator errors: 0
Fixed issues: 1
Total issues: 185
Test system warnings: 25
New deferred issues: 8
Fixed deferred issues: 2
Total deferred issues: 180
Run Time: 08 hours, 39 minutes, 26 seconds
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
BatchEstimator_ReportFile_AzimuthElevation [#37 failed]
BatchEstimator_ReportFile_BRTS [#39 failed]
BatchEstimator_ReportFile_Format [#37 failed]
BatchEstimator_ReportFile_GpsPosVec [#36 failed]
BatchEstimator_ReportFile_MultiSat_SpaceToSpace [#87 failed]
BatchEstimator_ReportFile_Range [#37 failed]
BatchEstimator_ReportFile_RangeRate [#37 failed]
BatchEstimator_ReportFile_RangeSkin [#37 failed]
BatchEstimator_ReportFile_SN [#38 failed]
BatchEstimator_ReportFile_XEastYNorth [#37 failed]
BatchEstimator_ReportFile_XSouthYEast [#37 failed]
BatchEstimator_ReportStyle_Concise [#37 failed]
BatchEstimator_ReportStyle_Debug [#37 failed]
BatchEstimator_ReportStyle_Normal [#37 failed]
BatchEstimator_ReportStyle_Verbose [#37 failed]
BatchEstimator_ReportStyle_Verbose_MultiSat_SpaceToSpace [#92 failed]
DynamicsModels_MultiHarmGrav_NotAPrimaryBody [#1 failed]
DynamicsModels_MultiHarmGrav_PrimaryBodyNoGravity [#1 failed]
EKFS_Plate_SolveFors_AreaCoefficient_DsnPnRange [Parameter
EstSat.EarthMJ2000Eq.VY error 0.000007 exceeds tolerance 0.000005]
EKFS_Plate_SolveFors_AreaCoefficient_DsnPnRange [Parameter
EstSat.EarthMJ2000Eq.VY error 0.000007 exceeds tolerance 0.000005]
ErrorModel_SolveFors_Bias_RangeRate2Way_RangeRate3Way [The test run
failed to converge]
KalmanFilter_ReportFile [#53 failed]
KalmanFilter_ReportFile_DSN_Moon [#54 failed]
KalmanFilter_ReportFile_DSN_Sun [#56 failed]
KalmanFilter_ReportFile_GpsPosVec [#53 failed]
KalmanFilter_ReportStyle_Verbose [#53 failed]
SpacecraftNavigation_SolveFors_CartesianState_RangeRate3Way [Parameter
EstSat.EarthMJ2000Eq.Y error 0.262941 exceeds tolerance 0.250000]
Output changes (but still pass):
None
Output changes (but still fail):
None
New crashes/hangs/etc.:
None
New script errors:
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_LargestState_RK89
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_MoonCB_ReportSTM
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_MoonCB
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_PropCopy
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSState_RK89
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSStep_ABM
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSStep_PD45
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSStep_PD78
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSStep_PD853
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSStep_RK56
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSStep_RK68
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSStep_RK89
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_ReportSTM
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_SunCB
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16
DynamicsModels_MultiHarmGrav_Earth30x30_Mars20x20_SRP_AllPlanets
DynamicsModels_MultiHarmGrav_Enceladus_Saturn_ReorderBodies
DynamicsModels_MultiHarmGrav_Enceladus_Saturn_ReportSTM
DynamicsModels_MultiHarmGrav_Enceladus_Saturn
DynamicsModels_MultiHarmGrav_Ex_LunarTransfer
DynamicsModels_MultiHarmGrav_PrimaryBodyDefaultGravity
FMParams_Acceleration_MultiHarmGrav_Earth12x12_Moon16x16_MoonCB
FMParams_Acceleration_MultiHarmGrav_Earth12x12_Moon16x16
Propagate_Covariance_SNC_MultiHarmGrav_Earth12x12_Moon16x16
Propagate_Covariance_SNC_None_MultiHarmGrav_Earth12x12_Moon16x16
New comparator errors:
None
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
SpacecraftNavigation_SolveFors_KeplerianState_DsnTcp3Way
Fixed crashes/hangs/etc.:
None
Fixed script errors:
None
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
None
Script errors:
*API_Command_MatlabFunction: (Python)
*AcceptFilter_DataTypes_SpaceToSpace_Range:
*AcceptFilter_Tracker_SpaceToSpace:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_BothTides:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_LargestState_RK89:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_LargestStep_RK89:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_MoonCB_ReportSTM:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_MoonCB:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_PropCopy:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSState_RK89:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSStep_ABM:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSStep_PD45:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSStep_PD78:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSStep_PD853:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSStep_RK56:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSStep_RK68:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_RSSStep_RK89:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_ReportSTM:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_SunCB:
*DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16:
*DynamicsModels_MultiHarmGrav_Earth30x30_Mars20x20_SRP_AllPlanets:
*DynamicsModels_MultiHarmGrav_EarthMoonL1:
*DynamicsModels_MultiHarmGrav_EarthMoonNRHO:
*DynamicsModels_MultiHarmGrav_Enceladus_Saturn_Moons_Planets_GR_SRP:
*DynamicsModels_MultiHarmGrav_Enceladus_Saturn_Moons_Planets_GR:
*DynamicsModels_MultiHarmGrav_Enceladus_Saturn_ReorderBodies:
*DynamicsModels_MultiHarmGrav_Enceladus_Saturn_ReportSTM:
*DynamicsModels_MultiHarmGrav_Enceladus_Saturn_Titan:
*DynamicsModels_MultiHarmGrav_Enceladus_Saturn:
*DynamicsModels_MultiHarmGrav_Ex_LunarTransfer:
*DynamicsModels_MultiHarmGrav_PrimaryBodyDefaultGravity:
*DynamicsModels_MultiHarmGrav_Validation_PrimaryBodyUseDefaultDegreeAndOrder:
*EKFS_SpacecraftNavigation_ExternalForceModel_PointMass:
EKFS_SpacecraftNavigation_MultiHarmGrav_EarthMoonNRHO_CAPSTONE:
[GMT-8282]
*EKF_RejectFilter_DataTypes_GpsPosVec:
*EKF_TrackingFileSet_DataFilters_GpsPosVec:
*ErrorModel_SolveFors_Bias_RangeRate3Way_Multiple:
*FMParams_Acceleration_MultiHarmGrav_Earth12x12_Moon16x16_MoonCB:
*FMParams_Acceleration_MultiHarmGrav_Earth12x12_Moon16x16:
*FMParams_Acceleration_MultiHarmGrav_EarthMoonNRHO:
*FMParams_Acceleration_MultiHarmGrav_Saturn_Enceladus_Cassini:
*FMParams_Acceleration_MultiHarmGrav_Saturn_Enceladus:
*ForceModel_External_Drag:
*ForceModel_External_ExcludeOtherForces_False:
*ForceModel_External_ExcludeOtherForces_True:
*ForceModel_External_NotInUserFunctions:
*ForceModel_External_PropFormation:
*ForceModel_External_PropSynchronized:
*ForceModel_External_PropagateCovariance:
*ForceModel_External_PropagateSTM:
*ForceModel_External_SNOPT_OptFiniteBurn:
*ForceModel_External_SimpleKeplerian_ABM_None:
*ForceModel_External_SimpleKeplerian_ABM_RSSState:
*ForceModel_External_SimpleKeplerian_ABM_RSSStep:
*ForceModel_External_SimpleKeplerian_BackProp:
*ForceModel_External_SimpleKeplerian_Moon:
*ForceModel_External_SimpleKeplerian_PD45_None:
*ForceModel_External_SimpleKeplerian_PD45_RSSState:
*ForceModel_External_SimpleKeplerian_PD45_RSSStep:
*ForceModel_External_SimpleKeplerian_PD78_None:
*ForceModel_External_SimpleKeplerian_PD78_RSSState:
*ForceModel_External_SimpleKeplerian_PD78_RSSStep:
*ForceModel_External_SimpleKeplerian_PD853_None:
*ForceModel_External_SimpleKeplerian_PD853_RSSState:
*ForceModel_External_SimpleKeplerian_PD853_RSSStep:
*ForceModel_External_SimpleKeplerian_RK68:
*ForceModel_External_SimpleKeplerian_RK89_None:
*ForceModel_External_SimpleKeplerian_RK89_RSSState:
*ForceModel_External_SimpleKeplerian_RK89_RSSStep:
*ForceModel_External_SimpleKeplerian_StopOnApogee:
*ForceModel_External_SimpleKeplerian:
ForceModel_External_SphericalSRP_FiniteBurn_RSSStep: [GMT-8022]
*ForceModel_External_SphericalSRP_FiniteBurn:
ForceModel_External_SphericalSRP: [GMT-8022]
*ForceModel_External_Targeter_HohmannTransfer:
*ForceModel_External_Yukon_OptFiniteBurn:
*MatAPI_Command_PythonFunction: (Matlab)
*Plate_SolveFors_EFM_DiffuseFraction_Test:
*Plate_SolveFors_EFM_SRP_AreaCoefficient_Test:
*Plate_SolveFors_EFM_SpecularFraction_Test:
*Propagate_Covariance_SNC_MultiHarmGrav_Earth12x12_Moon16x16_MoonCB:
*Propagate_Covariance_SNC_MultiHarmGrav_Earth12x12_Moon16x16:
*Propagate_Covariance_SNC_MultiHarmGrav_Enceladus_Saturn:
*Propagate_Covariance_SNC_None_MultiHarmGrav_Earth12x12_Moon16x16:
*RejectFilter_DataTypes_SpaceToSpace_Range:
*RejectFilter_Tracker_SpaceToSpace:
*Simulator_Propagator_ExternalForceModel_PointMass:
*SpacecraftNavigation_ExternalForceModel_MultiSat_TwoTdrsAndOneUser:
*SpacecraftNavigation_ExternalForceModel_PointMass:
*SpacecraftNavigation_ExternalForceModel_SolveCr:
SpacecraftNavigation_MultiHarmGrav_EarthMoonNRHO_CAPSTONE: [GMT-8282]
*SpacecraftNavigation_MultiSat_SpaceToSpace_EphPropNRHO_DSN_Moon:
*SpacecraftNavigation_MultiSat_SpaceToSpace_EphPropNRHO_GN_Moon:
*ThrustSegment_SolveFors_EFM_ThrustScaleFactor_Test:
*TrackingFileSet_DataFilters_SpaceToSpace:
*Transponder_TurnAroundRatio_RangeRate3Way_Sim:
Comparator errors:
None
Truth failures:
*BatchEstimator_ReportFile_AzimuthElevation [#37 failed]
*BatchEstimator_ReportFile_BRTS/BatchEstimator_ReportFile_BRTS.txt [#39
failed]
*BatchEstimator_ReportFile_Format [#37 failed]
*BatchEstimator_ReportFile_GpsPosVec [#36 failed]
*BatchEstimator_ReportFile_MultiSat_SpaceToSpace [#87 failed]
*BatchEstimator_ReportFile_Range [#37 failed]
*BatchEstimator_ReportFile_RangeRate [#37 failed]
*BatchEstimator_ReportFile_RangeSkin [#37 failed]
*BatchEstimator_ReportFile_SN/BatchEstimator_ReportFile_SN.txt [#38
failed]
*BatchEstimator_ReportFile_XEastYNorth [#37 failed]
*BatchEstimator_ReportFile_XSouthYEast [#37 failed]
*BatchEstimator_ReportStyle_Concise [#37 failed]
*BatchEstimator_ReportStyle_Debug [#37 failed]
*BatchEstimator_ReportStyle_Normal [#37 failed]
*BatchEstimator_ReportStyle_Verbose [#37 failed]
*BatchEstimator_ReportStyle_Verbose_MultiSat_SpaceToSpace [#92 failed]
DynamicsModels_Drag_Constant_CSSI [Failed to extract data records from
truth or output file] [GMT-8142]
DynamicsModels_Drag_CSSI_CSSI_PropOffEnd [Failed to extract data
records from truth or output file] [GMT-8142]
DynamicsModels_Drag_MSISE86_Constant_CSSI [Failed to extract data
records from truth or output file] [GMT-8142]
DynamicsModels_Drag_MSISE90_Constant_CSSI [Failed to extract data
records from truth or output file] [GMT-8142]
DynamicsModels_Drag_NRLMSISE00_Constant_CSSI [Failed to extract data
records from truth or output file] [GMT-8142]
*DynamicsModels_MultiHarmGrav_NotAPrimaryBody [#1 failed]
*DynamicsModels_MultiHarmGrav_PrimaryBodyNoGravity [#1 failed]
*DynamicsModels_MultiHarmGrav_Validation_MissingPrimaryBody [#1 failed]
*DynamicsModels_MultiHarmGrav_Validation_PrimaryBodyWithoutDegreeAndOrder [#1
failed]
*DynamicsModels_MultiHarmGrav_Validation_PrimaryBodyWithoutModelFile
[#1 failed]
*EKFS_ErrorModel_SolveFors_PassBiases_Disallowed [#1 failed]
*EKFS_Plate_SolveFors_AreaCoefficient_DsnPnRange/EKFS_Plate_SolveFors_AreaCoefficient_DsnPnRange_filter.txt
[Parameter EstSat.EarthMJ2000Eq.VY error 0.000007 exceeds tolerance 0.000005]
*EKFS_Plate_SolveFors_AreaCoefficient_DsnPnRange/EKFS_Plate_SolveFors_AreaCoefficient_DsnPnRange_smoother.txt
[Parameter EstSat.EarthMJ2000Eq.VY error 0.000007 exceeds tolerance 0.000005]
*EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_RangeRate3Way/EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_RangeRate3Way_filter.txt
[Parameter EstSat.EarthMJ2000Eq.X error 0.175488 exceeds tolerance 0.005000]
*EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_RangeRate3Way/EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_RangeRate3Way_smoother_backfilter.txt
[Parameter EstSat.EarthMJ2000Eq.Y error 0.057404 exceeds tolerance 0.050000]
*EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_RangeRate3Way/EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_RangeRate3Way_smoother.txt
[Parameter EstSat.EarthMJ2000Eq.X error 0.175488 exceeds tolerance 0.005000]
*EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr/EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr_Smoother.txt
[The test run failed to complete]
*EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr/EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr_Smoother_backfilter.txt
[The test run failed to complete]
*ErrorModel_Bias_Range_RangeRate [#2 failed]
*ErrorModel_SolveFors_Bias_RangeRate2Way_RangeRate3Way [The test run
failed to converge]
*ErrorModel_SolveFors_Bias_RangeRate3Way_MultipleOther [Parameter
EstSat.EarthMJ2000Eq.Y error 0.007370 exceeds tolerance 0.001000]
*ErrorModel_SolveFors_EFM_Measurement_Bias_SnRange_Test [#1 failed]
*Events_ContactLocator_ReportFormat_AERRangeRateReport [Output field
1902.338394 failed tolerance in record 26]
*Events_ContactLocator_ReportFormat_AERRangeRateReport_AzElMask [Output
field 250.600533 failed tolerance in record 2]
*Events_ContactLocator_ReportFormat_AERRangeRateReport_L2 [Output field
250.600533 failed tolerance in record 1]
*Events_ContactLocator_ReportFormat_AERRangeRateReport_LightTimeDirection_Receive
[Output field 1902.400686 failed tolerance in record 26]
*Events_ContactLocator_ReportFormat_AERRangeRateReport_RunMode_Automatic
[Output field 1902.338394 failed tolerance in record 27]
*Events_ContactLocator_ReportFormat_AERRangeRateReport_UseLightTime_False
[Output field 1568.450368 failed tolerance in record 25]
*Events_ContactLocator_ReportFormat_AERRangeRateReport_UseStellarAberration_True
[Output field 1902.518899 failed tolerance in record 26]
*ForceModel_External_IncorrectFunctionName [#1 failed]
*ForceModel_External_IncorrectFunctionSignature [#1 failed]
*GMAT_ISS_AllPlanets_0_0_0_Relativity [pos err 0.000205479, tol 0.0002]
GMATFunction_Hohmann_Targeter_Inside
Function_PassLocal_SC_In_Receive_LocalSC_Out_EphemerisFile [pos and vel interp
err : Inf , Inf] [GMT-7958]
GroundStation_Iono_SnDowd_Est [Residual failed at 27 Feb 2014
19:22:49.000] [GMT-6202]
*KalmanFilter_MeasDeweightingCoefficient_RangeRate3Way [Scaled residual
failed at 17 Sep 2005 00:10:00.000]
*KalmanFilter_MeasDeweightingCoefficient_RangeRate3Way [#1 failed]
*KalmanFilter_ReportFile [#53 failed]
*KalmanFilter_ReportFile_DSN_Moon [#54 failed]
*KalmanFilter_ReportFile_DSN_Sun [#56 failed]
*KalmanFilter_ReportFile_GpsPosVec [#53 failed]
*KalmanFilter_ReportFile_RangeRate3Way/KalmanFilter_ReportFile_RangeRate3Way.txt
[Test value 18.831310 exceeded tolerance in pattern #1]
*KalmanFilter_ReportStyle_Verbose [#53 failed]
*MatAPI_Command_MatlabFunction (Matlab) []
Matlab_IO_String [] [GMT-8122]
PythonFunction_PrintToLogFile [#2 failed] [GMT-7944]
SchattenFile_NominalCycle_Mean_JR [pos err 58.3124, tol 0.01] [GMT-8007]
*SchattenFile_PropBeforeBeginningOfFile [pos err 7.36281, tol 0.002]
*Simulator_AddData_DSN_GN [#2 failed]
*Simulator_AddData_SpaceToSpace_GN_DSN_Moon [#5 failed]
*Simulator_AddData_SpaceToSpace_GN_Moon [#4 failed]
Simulator_EarthFixedInitialState [Residual failed at 01 Mar 2005
00:19:00.000] [GMT-7923]
*Smoother_ReportFile_RangeRate3Way/Smoother_ReportFile_RangeRate3Way_Smoother.txt
[#12 failed]
*Smoother_ReportFile_RangeRate3Way/Smoother_ReportFile_RangeRate3Way_Smoother.txt
[Test value 0.000005 exceeded tolerance in pattern #1]
*SNOPT_LEOtoGEO_Monitored []
*SNOPT_LEOtoGEO_Monitored_Noopt []
*SNOPT_Problem_OptimalLCROSSTrajectory_Monitored []
*SpacecraftNavigation_Cislunar_DsnPnRangeTcp_Ramped_Orion/SpacecraftNavigation_Cislunar_DsnPnRangeTcp_Ramped_Orion.txt
[Test value 0.057207 exceeded tolerance in pattern #2]
SpacecraftNavigation_SolveFors_AreaCoefficient_FrequencyBias_DsnTcp3Way
[The test run failed to converge] [GMT-8135]
SpacecraftNavigation_SolveFors_AreaCoefficient_FrequencyBias_SnDopplerRtn [The
test run failed to converge] [GMT-8135]
SpacecraftNavigation_SolveFors_AreaCoefficient_FrequencyBias_SnDowd
[The test run failed to converge] [GMT-8135]
*SpacecraftNavigation_SolveFors_CartesianState_Cd_Cr_RangeRate3Way_GN_SN
[Parameter EstSat.Cd error 0.010695 exceeds tolerance 0.010000]
*SpacecraftNavigation_SolveFors_CartesianState_RangeRate3Way [Parameter
EstSat.EarthMJ2000Eq.Y error 0.262941 exceeds tolerance 0.250000]
*SpacecraftNavigation_SolveFors_KeplerianState_DsnPnRangeTcp2WayTcp3Way/SpacecraftNavigation_SolveFors_KeplerianState_DsnPnRangeTcp2WayTcp3Way.txt
[Parameter EstSat.EarthMJ2000Eq.RAAN error 0.000068 exceeds tolerance 0.000055]
*ThrustSegment_SolveFors_ThrustAngles_ThrustScaleFactor_RangeRate3Way
[Parameter EstSat.EarthMJ2000Eq.X error 0.011591 exceeds tolerance 0.005000]
TrackingFileSet_HORP_Sim_Earth_EphProp_All/TrackingFileSet_HORP_Sim_Earth_EphProp_All_Doppler.gmd
[ Observable Error: 2.276e-06 Hz on line 251] [GMT-7376]
*TrackingFileSet_SimDopplerCountInterval_5sec_SpaceToSpace [#2 failed]
*TrackingFileSet_SimDopplerCountInterval_DsnTcp_RangeRate/TrackingFileSet_SimDopplerCountInterval_DsnTcp_RangeRate_10.gmd
[#2 failed]
*TrackingFileSet_SimDopplerCountInterval_RangeRate_1 [#2 failed]
*TrackingFileSet_SimDopplerCountInterval_RangeRate_5 [#2 failed]
*TrackingFileSet_SimDopplerCountInterval_RangeRate_10 [#2 failed]
*VF13AD_Tut_MultipleShootingTutorial_Step4 []
*VF13AD_Tut_MultipleShootingTutorial_Step5 []
*VF13AD_Tut_MultipleShootingTutorial_Step5_Monitered []
-----------------------------------------------------------------
New Issues (Deferred)
-----------------------------------------------------------------
New truth failures (deferred):
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_SnDopplerRtn_Multiple
[Parameter EstWH2K.TDRS11_SnDopplerRtnEstBias.Bias error 0.010105 exceeds
tolerance 0.010000]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn
[Parameter EstSat.EarthMJ2000Eq.VY error 0.000001 exceeds tolerance 0.000001]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn
[Parameter EstSat.EarthMJ2000Eq.VY error 0.000001 exceeds tolerance 0.000001]
Output changes (but still pass) (deferred):
None
Output changes (but still fail) (deferred):
None
New crashes/hangs/etc. (deferred):
None
New script errors (deferred):
BatchEstimator_Propagator_MultiHarmGrav_Earth30x30_Moon20x20
EKFS_SpacecraftNavigation_MultiHarmGrav_Earth12x12_Moon16x16
KalmanFilter_Propagator_MultiHarmGrav_Earth30x30_Moon20x20
Simulator_Propagator_MultiHarmGrav_Earth30x30_Moon20x20
SpacecraftNavigation_MultiHarmGrav_Earth12x12_Moon16x16
New comparator errors (deferred):
None
-----------------------------------------------------------------
Fixed Issues (Deferred)
-----------------------------------------------------------------
Fixed truth failures (deferred):
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SN_OEM_SPK_RK
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SN_OEM_SPK_RK
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]
BatchEstimator_Propagator_MultiHarmGrav_Earth30x30_Moon20x20
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_MultiHarmGrav_Earth12x12_Moon16x16
EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_SN [GMT-7376]
EKF_AcceptFilter_Level2_DataTypes_SnDopplerRtn
EKF_AcceptFilter_Level2_Multiple_SnDopplerRtn
EKF_AcceptFilter_Level2_ThinningFrequency_SnDopplerRtn
EKF_AcceptFilter_Level2_Trackers_SnDopplerRtn
EKF_RejectFilter_Level2_DataTypes_SnDopplerRtn
EKF_RejectFilter_Level2_Multiple_SnDopplerRtn
EKF_RejectFilter_Level2_ThinningFrequency_SnDopplerRtn
EKF_RejectFilter_Level2_Trackers_SnDopplerRtn
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_DelayRectifyTimeSpan_SN
KalmanFilter_InputWarmStartFile_GN_Moon_Keplerian [GMT-7785]
KalmanFilter_InputWarmStartFile_GpsPosVec_KeplerianToCartesian
[GMT-7785]
KalmanFilter_InputWarmStartFile_SN [GMT-7914]
KalmanFilter_InputWarmStartFile_SnDopplerRtn [GMT-7914]
KalmanFilter_MeasDeweightingCoefficient_SN
KalmanFilter_MeasDeweightingSigmaThreshold_SN
KalmanFilter_Measurements_SN
KalmanFilter_OutputWarmStartFile_GpsPosVec_Keplerian [GMT-7785]
KalmanFilter_OutputWarmStartFile_SN
KalmanFilter_ProcessNoiseTimeStep_0sec_SN
KalmanFilter_ProcessNoiseTimeStep_SN
KalmanFilter_Propagator_MultiHarmGrav_Earth30x30_Moon20x20
KalmanFilter_Propagator_OEMV2 [GMT-7943]
KalmanFilter_Propagator_SN
KalmanFilter_Propagator_SPK_TDRS_Multiple
KalmanFilter_Propagator_SPK_TDRS
KalmanFilter_Propagator_STK_TDRS_Multiple
KalmanFilter_Propagator_STK_TDRS
KalmanFilter_ScaledResidualThreshold_SN
KalmanFilter_Smoother_PredictTimeSpan_Both_OEM [GMT-6949]
KalmanFilter_WarmStartEpoch_SN [GMT-7376]
MatAPI_PrecessingSpinner (Matlab) [GMT-7595]
Math_Shadowed_Builtins [GMT-3043]
RejectFilter_Multiple_BRTS
SNOPT_Tut_MultipleShootingTutorial_Step3 [GMT-8271]
SNOPT_Tut_MultipleShootingTutorial_Step5 [GMT-8271]
ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522]
Simulator_Propagator_MultiHarmGrav_Earth30x30_Moon20x20
Smoother_Filter_ProcessNoiseTimeStep_0sec_SN
SpacecraftNavigation_MultiHarmGrav_Earth12x12_Moon16x16
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
ThrustHistoryFile_EstimateTSF_EpochBeforeBurn_RSSStep_Aqua [GMT-6451]
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]
Yukon_Hohmann_CostVsNoCost [GMT-8241]
Yukon_Hohmann_LowerSMA [GMT-8241]
Yukon_Hohmann_MultipleOfSameConstraint [GMT-8241]
Yukon_Hohmann_TwoBoundsConstraint [GMT-8241]
Yukon_LEOtoGEO_AllConstraintTypes [GMT-8241]
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 (Python) [#1 failed] [GMT-7595]
BatchEstimator_NormalMatrixReduction_UseInitialCovariance [#1 failed]
[GMT-7274]
EKF_AcceptFilter_Level2_TimeSpan_SnDopplerRtn [#12 failed]
EKF_AcceptFilter_Level2_TimeSpan_SnDopplerRtn [#2 failed]
EKF_RejectFilter_Level2_TimeSpan_SnDopplerRtn [#2 failed]
EKF_RejectFilter_Level2_TimeSpan_SnDopplerRtn [#4 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/gmattest/output/RedHatEnterprise8-GMAT_Console/Resources/FRR-31_EphemerisFile/script/EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_DuringEstimationArc_STK_Smoother.e]
[GMT-7483]
EKFS_ErrorModel_NoiseSigma_SnDopplerRtn/EKFS_ErrorModel_NoiseSigma_SnDopplerRtn_Filter.txt
[Failed to match pattern #1]
EKFS_ErrorModel_NoiseSigma_SnDopplerRtn/EKFS_ErrorModel_NoiseSigma_SnDopplerRtn_Smoother.txt
[Failed to match pattern #1]
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_SnDopplerRtn_Multiple/EKFS_ErrorModel_SolveFors_Bias_RandomConstant_SnDopplerRtn_Multiple_Smoother_backfilter.txt
[Parameter EstWH2K.TDRS11_SnDopplerRtnEstBias.Bias error 0.010105 exceeds
tolerance 0.010000]
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]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn/EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn_Filter.txt
[Parameter EstSat.EarthMJ2000Eq.VY error 0.000001 exceeds tolerance 0.000001]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn/EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn_Smoother.txt
[Parameter EstSat.EarthMJ2000Eq.VY error 0.000001 exceeds tolerance 0.000001]
Ephem_GMAT_Code500_InterpolationOrder/Ephem_GMAT_Code500_InterpolationOrder_1.eph
[pos err 0.0200021, 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 15.2489, 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 0.000815327,
tol 1e-06] [GMT-2567]
GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_BS [pos err
0.00254499, tol 0.0023]
GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Max_Reduction_BS [pos
err 0.00254499, tol 0.0023]
GMAT_LEO_PropSynchronization_BS []
GMAT_LunarTran_PropSynchronization_BS [max diff 1.72678e-07 > tol 5e-08]
GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS [pos err 0.0781136, 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_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]
MatAPI_Epoch_LeapSecond_In (Matlab) [#7 failed] [2561]
MatAPI_Epoch_LeapSecond_Out (Matlab) [#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]
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 [Ephemeris file has extra member
SegmentBoundaryTimes] [GMT-7376]
SNOPT_Tut_MultipleShootingTutorial_Step4 [] [GMT-8271]
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: 145 lines, Truth:
290 lines] [GMT-8143]
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]
TrkFile_SimEst_TDRS_range_Solve_Cr []
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]
Yukon_Hohmann_DeltaVCost [] [GMT-8241]
Yukon_Problem_hs077 [] [GMT-8241]
-----------------------------------------------------------------
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_SnDoppler_EphProp_SPK [GMT-7376]
EKFS_ErrorModel_SolveFors_Bias_SnRangeSnDoppler_EphProp_SPK [GMT-7376]
EKFS_ErrorModel_SolveFors_Bias_SnRangeSnDoppler_EphProp_STK [GMT-7376]
EKFS_ErrorModel_SolveFors_Bias_SnRange_EphProp_SPK [GMT-7376]
EKFS_ErrorModel_SolveFors_Bias_SnRange_EphProp_STK [GMT-7376]
EKFS_SpacecraftNavigation_LEO_TDRS_EphProp_OEM_Aqua [GMT-7914]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_SN_OEM [GMT-7914]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_SN_OEM
[GMT-7376]
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]
MatAPI_PD45PropagationE8x8SMPM [GMT-7755]
Python_IO_String [5317]
SNOPT_Tut_MultipleShootingTutorial_Step2 [GMT-8271]
ScriptLanguage_LineContinuation_BeginningOfLine [GMT-3756]
Simulator_Propagator_EarthPointMass_Drag [GMT-5417]
SpacecraftNavigation_SPADDragScaleFactorSigma_ConstrainInc [GMT-7078,
Ubuntu only]
Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
Tut_MultipleShootingTutorial_Step3 [GMT-7280]
-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: No LSB modules are available.
UbuntuNo LSB modules are available.
24.04
Tested build: No LSB modules are available.
UbuntuNo LSB modules are available.
24.04-GMAT_Console
Regression build: No LSB modules are available.
UbuntuNo LSB modules are available.
24.04Baseline
Total number of scripts: 18021 (+222 deferred)
Percent Passed: 99.36%
New issues: 0
Output changes: 0
New truth failures: 0
New crashes: 0
New script errors: 0
New comparator errors: 0
Fixed issues: 0
Total issues: 122
Test system warnings: 25
New deferred issues: 0
Fixed deferred issues: 0
Total deferred issues: 173
Run Time: 07 hours, 13 minutes, 22 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:
None
Fixed crashes/hangs/etc.:
None
Fixed script errors:
None
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
None
Script errors:
*API_Command_MatlabFunction: (Python)
*AcceptFilter_DataTypes_SpaceToSpace_Range:
*AcceptFilter_Tracker_SpaceToSpace:
*EKFS_SpacecraftNavigation_ExternalForceModel_PointMass:
*EKF_RejectFilter_DataTypes_GpsPosVec:
*EKF_TrackingFileSet_DataFilters_GpsPosVec:
*ErrorModel_SolveFors_Bias_RangeRate3Way_Multiple:
*ForceModel_External_Drag:
*ForceModel_External_ExcludeOtherForces_False:
*ForceModel_External_ExcludeOtherForces_True:
*ForceModel_External_NotInUserFunctions:
*ForceModel_External_PropFormation:
*ForceModel_External_PropSynchronized:
*ForceModel_External_PropagateCovariance:
*ForceModel_External_PropagateSTM:
*ForceModel_External_SNOPT_OptFiniteBurn:
*ForceModel_External_SimpleKeplerian_ABM_None:
*ForceModel_External_SimpleKeplerian_ABM_RSSState:
*ForceModel_External_SimpleKeplerian_ABM_RSSStep:
*ForceModel_External_SimpleKeplerian_BackProp:
*ForceModel_External_SimpleKeplerian_Moon:
*ForceModel_External_SimpleKeplerian_PD45_None:
*ForceModel_External_SimpleKeplerian_PD45_RSSState:
*ForceModel_External_SimpleKeplerian_PD45_RSSStep:
*ForceModel_External_SimpleKeplerian_PD78_None:
*ForceModel_External_SimpleKeplerian_PD78_RSSState:
*ForceModel_External_SimpleKeplerian_PD78_RSSStep:
*ForceModel_External_SimpleKeplerian_PD853_None:
*ForceModel_External_SimpleKeplerian_PD853_RSSState:
*ForceModel_External_SimpleKeplerian_PD853_RSSStep:
*ForceModel_External_SimpleKeplerian_RK68:
*ForceModel_External_SimpleKeplerian_RK89_None:
*ForceModel_External_SimpleKeplerian_RK89_RSSState:
*ForceModel_External_SimpleKeplerian_RK89_RSSStep:
*ForceModel_External_SimpleKeplerian_StopOnApogee:
*ForceModel_External_SimpleKeplerian:
ForceModel_External_SphericalSRP_FiniteBurn_RSSStep: [GMT-8022]
*ForceModel_External_SphericalSRP_FiniteBurn:
ForceModel_External_SphericalSRP: [GMT-8022]
*ForceModel_External_Targeter_HohmannTransfer:
*ForceModel_External_Yukon_OptFiniteBurn:
*MatAPI_Command_MatlabFunction: (Matlab)
*Plate_SolveFors_EFM_DiffuseFraction_Test:
*Plate_SolveFors_EFM_SRP_AreaCoefficient_Test:
*Plate_SolveFors_EFM_SpecularFraction_Test:
*RejectFilter_DataTypes_SpaceToSpace_Range:
*RejectFilter_Tracker_SpaceToSpace:
*SNOPT_LEOtoGEO_Monitored:
*Simulator_Propagator_ExternalForceModel_PointMass:
*SpacecraftNavigation_ExternalForceModel_MultiSat_TwoTdrsAndOneUser:
*SpacecraftNavigation_ExternalForceModel_PointMass:
*SpacecraftNavigation_ExternalForceModel_SolveCr:
*SpacecraftNavigation_MultiSat_SpaceToSpace_EphPropNRHO_DSN_Moon:
*SpacecraftNavigation_MultiSat_SpaceToSpace_EphPropNRHO_GN_Moon:
*ThrustSegment_SolveFors_EFM_ThrustScaleFactor_Test:
*TrackingFileSet_DataFilters_SpaceToSpace:
*Transponder_TurnAroundRatio_RangeRate3Way_Sim:
Comparator errors:
None
Truth failures:
DynamicsModels_Drag_Constant_CSSI [Failed to extract data records from
truth or output file] [GMT-8142]
DynamicsModels_Drag_CSSI_CSSI_PropOffEnd [Failed to extract data
records from truth or output file] [GMT-8142]
DynamicsModels_Drag_MSISE86_Constant_CSSI [Failed to extract data
records from truth or output file] [GMT-8142]
DynamicsModels_Drag_MSISE90_Constant_CSSI [Failed to extract data
records from truth or output file] [GMT-8142]
DynamicsModels_Drag_NRLMSISE00_Constant_CSSI [Failed to extract data
records from truth or output file] [GMT-8142]
*DynamicsModels_MultiHarmGrav_Ex_LunarTransfer [Output field -0.553034
failed tolerance in record 4]
*EKFS_ErrorModel_SolveFors_PassBiases_Disallowed [#1 failed]
*EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_ColdStart/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_ColdStart_Smoother.e
[CovarianceTimePos failed tolerance at row 59686]
*EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_ColdStart/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_ColdStart_Filter.tab
[Output field -0.004853 failed tolerance in record 969]
*EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_RangeRate3Way/EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_RangeRate3Way_filter.txt
[Parameter EstSat.EarthMJ2000Eq.X error 0.175488 exceeds tolerance 0.005000]
*EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_RangeRate3Way/EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_RangeRate3Way_smoother_backfilter.txt
[Parameter EstSat.EarthMJ2000Eq.Y error 0.057404 exceeds tolerance 0.050000]
*EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_RangeRate3Way/EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_FogmADSF_RangeRate3Way_smoother.txt
[Parameter EstSat.EarthMJ2000Eq.X error 0.175488 exceeds tolerance 0.005000]
*EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr/EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr_Smoother.txt
[The test run failed to complete]
*EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr/EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr_Smoother_backfilter.txt
[The test run failed to complete]
*ErrorModel_Bias_Range_RangeRate [#2 failed]
*ErrorModel_SolveFors_Bias_RangeRate3Way_MultipleOther [Parameter
EstSat.EarthMJ2000Eq.Y error 0.007370 exceeds tolerance 0.001000]
*ErrorModel_SolveFors_EFM_Measurement_Bias_SnRange_Test [#1 failed]
*Events_ContactLocator_ReportFormat_AERRangeRateReport [Output field
1902.338394 failed tolerance in record 26]
*Events_ContactLocator_ReportFormat_AERRangeRateReport_AzElMask [Output
field 250.600533 failed tolerance in record 2]
*Events_ContactLocator_ReportFormat_AERRangeRateReport_L2 [Output field
250.600533 failed tolerance in record 1]
*Events_ContactLocator_ReportFormat_AERRangeRateReport_LightTimeDirection_Receive
[Output field 1902.400686 failed tolerance in record 26]
*Events_ContactLocator_ReportFormat_AERRangeRateReport_RunMode_Automatic
[Output field 1902.338394 failed tolerance in record 27]
*Events_ContactLocator_ReportFormat_AERRangeRateReport_UseLightTime_False
[Output field 1568.450368 failed tolerance in record 25]
*Events_ContactLocator_ReportFormat_AERRangeRateReport_UseStellarAberration_True
[Output field 1902.518899 failed tolerance in record 26]
*ForceModel_External_IncorrectFunctionName [#1 failed]
*ForceModel_External_IncorrectFunctionSignature [#1 failed]
GMATFunction_Hohmann_Targeter_Inside
Function_PassLocal_SC_In_Receive_LocalSC_Out_EphemerisFile [pos and vel interp
err : Inf , Inf] [GMT-7958]
GroundStation_Iono_SnDowd_Est [Residual failed at 27 Feb 2014
19:13:41.000] [GMT-6202]
*GroundStation_Tropo_Marini_SnDowd [Output field 0.031884 failed
tolerance in record 985]
*KalmanFilter_MeasDeweightingCoefficient_RangeRate3Way [Scaled residual
failed at 17 Sep 2005 00:10:00.000]
*KalmanFilter_MeasDeweightingCoefficient_RangeRate3Way [#1 failed]
*KalmanFilter_ReportFile_RangeRate3Way/KalmanFilter_ReportFile_RangeRate3Way.txt
[Test value 18.832575 exceeded tolerance in pattern #1]
Matlab_IO_String [] [GMT-8122]
*Plate_SolveFors_DiffuseFraction_SnDowd [Parameter
EstSat.EarthMJ2000Eq.VX error 0.000001 exceeds tolerance 0.000001]
PythonFunction_PrintToLogFile [#2 failed] [GMT-7944]
SchattenFile_NominalCycle_Mean_JR [pos err 58.3125, tol 0.01] [GMT-8007]
*SchattenFile_PropBeforeBeginningOfFile [pos err 7.36281, tol 0.002]
*Simulator_AddData_DSN_GN [#2 failed]
*Simulator_AddData_SpaceToSpace_GN_DSN_Moon [#5 failed]
*Simulator_AddData_SpaceToSpace_GN_Moon [#4 failed]
Simulator_EarthFixedInitialState [Residual failed at 01 Mar 2005
00:19:00.000] [GMT-7923]
*Smoother_ReportFile_RangeRate3Way/Smoother_ReportFile_RangeRate3Way_Smoother.txt
[#12 failed]
*Smoother_ReportFile_RangeRate3Way/Smoother_ReportFile_RangeRate3Way_Smoother.txt
[Test value 34.475582 exceeded tolerance in pattern #1]
*SNOPT_LEOtoGEO_Monitored_Noopt []
*SNOPT_LEOtoGEOExact_Monitored_ObjectParameter_Noopt []
*SpacecraftNavigation_Cislunar_DsnPnRangeTcp_Ramped_Orion/SpacecraftNavigation_Cislunar_DsnPnRangeTcp_Ramped_Orion.txt
[Test value 0.057208 exceeded tolerance in pattern #2]
*SpacecraftNavigation_Moon_DsnTcp_RangeRate_LRO/SpacecraftNavigation_Moon_DsnTcp_RangeRate_LRO.json
[Iteration 3 computed measurement 2601 Residual tolerance failure]
SpacecraftNavigation_SolveFors_AreaCoefficient_FrequencyBias_DsnTcp3Way
[The test run failed to converge] [GMT-8135]
SpacecraftNavigation_SolveFors_AreaCoefficient_FrequencyBias_SnDopplerRtn [The
test run failed to converge] [GMT-8135]
SpacecraftNavigation_SolveFors_AreaCoefficient_FrequencyBias_SnDowd
[The test run failed to converge] [GMT-8135]
*SpacecraftNavigation_SolveFors_CartesianState_Cd_Cr_RangeRate3Way_GN_SN
[Parameter EstSat.Cd error 0.010694 exceeds tolerance 0.010000]
*SpacecraftNavigation_SolveFors_CartesianState_Cd_Cr_SnDopplerRtn [The
test run failed to converge]
*SpacecraftNavigation_SolveFors_CartesianState_DsnPnRangeTcp2WayTcp3Way/SpacecraftNavigation_SolveFors_CartesianState_DsnPnRangeTcp2WayTcp3Way.txt
[Parameter EstSat.EarthMJ2000Eq.Y error 0.051911 exceeds tolerance 0.050000]
*SpacecraftNavigation_SolveFors_KeplerianState_ADSF_SnDowd [The test
run failed to converge]
*SpacecraftNavigation_SolveFors_KeplerianState_DsnPnRangeTcp2WayTcp3Way/SpacecraftNavigation_SolveFors_KeplerianState_DsnPnRangeTcp2WayTcp3Way.txt
[Parameter EstSat.EarthMJ2000Eq.RAAN error 0.000059 exceeds tolerance 0.000055]
*ThrustSegment_SolveFors_ThrustAngles_ThrustScaleFactor_RangeRate3Way
[Parameter EstSat.EarthMJ2000Eq.X error 0.011591 exceeds tolerance 0.005000]
TrackingFileSet_HORP_Sim_Earth_EphProp_All/TrackingFileSet_HORP_Sim_Earth_EphProp_All_Doppler.gmd
[ Observable Error: 2.276e-06 Hz on line 251] [GMT-7376]
*TrackingFileSet_SimDopplerCountInterval_5sec_SpaceToSpace [#2 failed]
*TrackingFileSet_SimDopplerCountInterval_DsnTcp_RangeRate/TrackingFileSet_SimDopplerCountInterval_DsnTcp_RangeRate_10.gmd
[#2 failed]
*TrackingFileSet_SimDopplerCountInterval_RangeRate_1 [#2 failed]
*TrackingFileSet_SimDopplerCountInterval_RangeRate_5 [#2 failed]
*TrackingFileSet_SimDopplerCountInterval_RangeRate_10 [#2 failed]
*VF13AD_Tut_MultipleShootingTutorial_Step4 []
*VF13AD_Tut_MultipleShootingTutorial_Step5 []
*VF13AD_Tut_MultipleShootingTutorial_Step5_Monitered []
-----------------------------------------------------------------
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_AcceptFilter_Level2_DataTypes_SnDopplerRtn
EKF_AcceptFilter_Level2_Multiple_SnDopplerRtn
EKF_AcceptFilter_Level2_ThinningFrequency_SnDopplerRtn
EKF_AcceptFilter_Level2_Trackers_SnDopplerRtn
EKF_RejectFilter_Level2_DataTypes_SnDopplerRtn
EKF_RejectFilter_Level2_Multiple_SnDopplerRtn
EKF_RejectFilter_Level2_ThinningFrequency_SnDopplerRtn
EKF_RejectFilter_Level2_Trackers_SnDopplerRtn
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_DelayRectifyTimeSpan_SN
KalmanFilter_InputWarmStartFile_GN_Moon_Keplerian [GMT-7785]
KalmanFilter_InputWarmStartFile_GpsPosVec_KeplerianToCartesian
[GMT-7785]
KalmanFilter_InputWarmStartFile_SN [GMT-7914]
KalmanFilter_InputWarmStartFile_SnDopplerRtn [GMT-7914]
KalmanFilter_MeasDeweightingCoefficient_SN
KalmanFilter_MeasDeweightingSigmaThreshold_SN
KalmanFilter_Measurements_SN
KalmanFilter_OutputWarmStartFile_GpsPosVec_Keplerian [GMT-7785]
KalmanFilter_OutputWarmStartFile_SN
KalmanFilter_ProcessNoiseTimeStep_0sec_SN
KalmanFilter_ProcessNoiseTimeStep_SN
KalmanFilter_Propagator_OEMV2 [GMT-7943]
KalmanFilter_Propagator_SN
KalmanFilter_Propagator_SPK_TDRS_Multiple
KalmanFilter_Propagator_SPK_TDRS
KalmanFilter_Propagator_STK_TDRS_Multiple
KalmanFilter_Propagator_STK_TDRS
KalmanFilter_ScaledResidualThreshold_SN
KalmanFilter_Smoother_PredictTimeSpan_Both_OEM [GMT-6949]
KalmanFilter_WarmStartEpoch_SN [GMT-7376]
MatAPI_PrecessingSpinner (Matlab) [GMT-7595]
Math_Shadowed_Builtins [GMT-3043]
OCPropTest_SPAD_Drag_1deg_Bicubic_LEO [GMT-7147]
OCPropTest_SPAD_Drag_SRP_1deg_Bicubic_LEO [GMT-7147]
RejectFilter_Multiple_BRTS
SNOPT_Tut_MultipleShootingTutorial_Step3 [GMT-8271]
SNOPT_Tut_MultipleShootingTutorial_Step5 [GMT-8271]
ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522]
Smoother_Filter_ProcessNoiseTimeStep_0sec_SN
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
ThrustHistoryFile_EstimateTSF_EpochBeforeBurn_RSSStep_Aqua [GMT-6451]
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]
Yukon_Hohmann_CostVsNoCost [GMT-8241]
Yukon_Hohmann_LowerSMA [GMT-8241]
Yukon_Hohmann_MultipleOfSameConstraint [GMT-8241]
Yukon_Hohmann_TwoBoundsConstraint [GMT-8241]
Yukon_LEOtoGEO_AllConstraintTypes [GMT-8241]
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 (Python) [#1 failed] [GMT-7595]
BatchEstimator_NormalMatrixReduction_UseInitialCovariance [#1 failed]
[GMT-7274]
EKF_AcceptFilter_Level2_TimeSpan_SnDopplerRtn [#12 failed]
EKF_AcceptFilter_Level2_TimeSpan_SnDopplerRtn [#2 failed]
EKF_RejectFilter_Level2_TimeSpan_SnDopplerRtn [#2 failed]
EKF_RejectFilter_Level2_TimeSpan_SnDopplerRtn [#4 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/gmattest/output/No LSB modules
are available.
UbuntuNo LSB modules are available.
24.04-GMAT_Console/Resources/FRR-31_EphemerisFile/script/EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_DuringEstimationArc_STK_Smoother.e]
[GMT-7483]
EKFS_ErrorModel_NoiseSigma_SnDopplerRtn/EKFS_ErrorModel_NoiseSigma_SnDopplerRtn_Filter.txt
[Failed to match pattern #1]
EKFS_ErrorModel_NoiseSigma_SnDopplerRtn/EKFS_ErrorModel_NoiseSigma_SnDopplerRtn_Smoother.txt
[Failed to match pattern #1]
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 0.000758 failed tolerance in record 521] [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]
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]
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 15.2552, 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 14.3613, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
[pos err 0.000215886, 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 0.000813043,
tol 1e-06] [GMT-2567]
GMAT_LEO_PropSynchronization_BS []
GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS [pos err 0.0752843, 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_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]
MatAPI_Epoch_LeapSecond_In (Matlab) [#7 failed] [2561]
MatAPI_Epoch_LeapSecond_Out (Matlab) [#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]
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 [Ephemeris file has extra member
SegmentBoundaryTimes] [GMT-7376]
SNOPT_Tut_MultipleShootingTutorial_Step4 [] [GMT-8271]
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: 145 lines, Truth:
290 lines] [GMT-8143]
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]
TrkFile_SimEst_TDRS_range_Solve_Cr []
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]
Yukon_Hohmann_DeltaVCost [] [GMT-8241]
Yukon_Problem_hs077 [] [GMT-8241]
-----------------------------------------------------------------
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_SnDoppler_EphProp_SPK [GMT-7376]
EKFS_ErrorModel_SolveFors_Bias_SnRangeSnDoppler_EphProp_SPK [GMT-7376]
EKFS_ErrorModel_SolveFors_Bias_SnRangeSnDoppler_EphProp_STK [GMT-7376]
EKFS_ErrorModel_SolveFors_Bias_SnRange_EphProp_SPK [GMT-7376]
EKFS_ErrorModel_SolveFors_Bias_SnRange_EphProp_STK [GMT-7376]
EKFS_SpacecraftNavigation_LEO_TDRS_EphProp_OEM_Aqua [GMT-7914]
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]
SNOPT_Tut_MultipleShootingTutorial_Step2 [GMT-8271]
ScriptLanguage_LineContinuation_BeginningOfLine [GMT-3756]
Simulator_Propagator_EarthPointMass_Drag [GMT-5417]
SpacecraftNavigation_SPADDragScaleFactorSigma_ConstrainInc [GMT-7078,
Ubuntu only]
Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
Tut_MultipleShootingTutorial_Step3 [GMT-7280]
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