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)[email protected]
-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Ubuntu
Tested build: Ubuntu-GMAT_Console
Regression build: UbuntuBaseline
Total number of scripts: 18028 (+227 deferred)
Percent Passed: 99.29%
New issues: 55
Output changes: 0
New truth failures: 12
New crashes: 0
New script errors: 43
New comparator errors: 0
Fixed issues: 31
Total issues: 130
Test system warnings: 22
New deferred issues: 9
Fixed deferred issues: 3
Total deferred issues: 185
Run Time: 07 hours, 24 minutes, 26 seconds
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
EKFS_SpacecraftNavigation_LEO_TDRS_EphProp_OEM_Aqua [The test run
failed to complete] [GMT-7914]
Optimize_Validation_Yukon_Disallowed_Sequences [ptrn 1 failed]
Optimize_Validation_Yukon_No_Vary_Command [ptrn 1 failed]
Optimize_Yukon_CostFunction_and_ConvergedStatus_Display [ptrn 1,2,3
failed]
Optimize_Yukon_CostFunction_and_ConvergedStatus_Display_2 [ptrn 1,2,3,4
failed]
Optimize_Yukon_Max_Function_Evals_Display [ptrn 1,2 failed]
Optimize_Yukon_Max_Iterations_Display [ptrn 1,2 failed]
SpacecraftNavigation_SolveFors_KeplerianState_ADSF_SnDowd [The test run
failed to converge]
SpacecraftNavigation_SolveFors_KeplerianState_DsnSeqRangeTcp2WayTcp3Way
[The test run failed to converge]
Yukon_Problem_hs077_ReportData [ptrn 1,2,3,4,10,11,12,13,14,15 failed]
Yukon_ShowProgress_Iteration [ptrn 1,2,3,4 failed]
Yukon_ShowProgress_Parameters [ptrn 1,2 failed]
Output changes (but still pass):
None
Output changes (but still fail):
None
New crashes/hangs/etc.:
None
New script errors:
Ex_MarsLaunchWindowAnalysis
ForceModel_External_SphericalSRP_FiniteBurn
Optimize_Yukon_ExitMode_DiscardAndContinue_2
Optimize_Yukon_ExitMode_DiscardAndContinue_3
Optimize_Yukon_ExitMode_DiscardAndContinue
Optimize_Yukon_ExitMode_SaveAndContinue_2
Optimize_Yukon_ExitMode_SaveAndContinue_3
Optimize_Yukon_ExitMode_SaveAndContinue_4
Optimize_Yukon_ExitMode_SaveAndContinue
Optimize_Yukon_ExitMode_Stop
Optimize_Yukon_Minimize_Height_on_circle_3
Optimize_Yukon_SolveMode_Defaultscript
Optimize_Yukon_SolveMode_DiscardAndContinue_GMT-4346
Optimize_Yukon_SolveMode_RunInitialGuess
Optimize_Yukon_SolveMode_SaveAndContinue_GMT-4346
Optimize_Yukon_SolveMode_Solve
Optimize_Yukon_cvg_status_FailsToConverge
Optimize_Yukon_cvg_status
Tut_MultipleShootingTutorial_Step2
Tut_MultipleShootingTutorial_Step3 [GMT-7280]
Tut_MultipleShootingTutorial_Step4
Tut_MultipleShootingTutorial_Step5
Yukon_ConvergenceTolerance
Yukon_DerivativeMethod_CentralDiff
Yukon_DerivativeMethod_ForwardDiff
Yukon_FeasibilityTolerance
Yukon_FunctionTolerance
Yukon_HessianUpdateMethod_Damped
Yukon_HessianUpdateMethod_SelfScaled
Yukon_Hohmann_RaiseSMA
Yukon_LRO2BurnApsidesRotation
Yukon_LRO3BurnApsidesRotation
Yukon_MaxFunctionEvaluations
Yukon_MaxIterations
Yukon_OptimalLunarTransfer
Yukon_OptimalityTolerance
Yukon_Problem_MarsPatchConic
Yukon_Problem_MinFuelLunarTransfer
Yukon_Problem_OptimalLCROSSTrajectory
Yukon_Problem_OptimalLunarApsidesRotation_2Burn
Yukon_Problem_SGR_P1_2
Yukon_Problem_TP254
Yukon_Problem_TP394
New comparator errors:
None
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
ForceModel_External_ExcludeOtherForces_True
ForceModel_External_NotInUserFunctions
ForceModel_External_PropagateCovariance
ForceModel_External_PropagateSTM
ForceModel_External_PropFormation
ForceModel_External_PropFormation
ForceModel_External_PropSynchronized
ForceModel_External_SimpleKeplerian
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_Targeter_HohmannTransfer
Plate_SolveFors_AreaCoefficient_DsnPnRange
SpacecraftNavigation_ExternalForceModel_PointMass
Fixed crashes/hangs/etc.:
None
Fixed script errors:
Simulator_Propagator_ExternalForceModel_PointMass
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
None
Script errors:
*API_Command_MatlabFunction: (Python)
EKFS_SpacecraftNavigation_MultiHarmGrav_EarthMoonNRHO_CAPSTONE:
[GMT-8282]
*Ex_MarsLaunchWindowAnalysis:
*ForceModel_External_Drag:
*ForceModel_External_SNOPT_OptFiniteBurn:
ForceModel_External_SphericalSRP_FiniteBurn_RSSStep: [GMT-8022]
*ForceModel_External_SphericalSRP_FiniteBurn:
*ForceModel_External_Yukon_OptFiniteBurn:
*MatAPI_Command_MatlabFunction: (Matlab)
*Optimize_Yukon_ExitMode_DiscardAndContinue_2:
*Optimize_Yukon_ExitMode_DiscardAndContinue_3:
*Optimize_Yukon_ExitMode_DiscardAndContinue:
*Optimize_Yukon_ExitMode_SaveAndContinue_2:
*Optimize_Yukon_ExitMode_SaveAndContinue_3:
*Optimize_Yukon_ExitMode_SaveAndContinue_4:
*Optimize_Yukon_ExitMode_SaveAndContinue:
*Optimize_Yukon_ExitMode_Stop:
*Optimize_Yukon_Minimize_Height_on_circle_3:
*Optimize_Yukon_SolveMode_Defaultscript:
*Optimize_Yukon_SolveMode_DiscardAndContinue_GMT-4346:
*Optimize_Yukon_SolveMode_RunInitialGuess:
*Optimize_Yukon_SolveMode_SaveAndContinue_GMT-4346:
*Optimize_Yukon_SolveMode_Solve:
*Optimize_Yukon_cvg_status_FailsToConverge:
*Optimize_Yukon_cvg_status:
*SNOPT_LEOtoGEO_Monitored:
SpacecraftNavigation_MultiHarmGrav_EarthMoonNRHO_CAPSTONE: [GMT-8282]
*Tut_MultipleShootingTutorial_Step2:
Tut_MultipleShootingTutorial_Step3: [GMT-7280]
*Tut_MultipleShootingTutorial_Step4:
*Tut_MultipleShootingTutorial_Step5:
*Yukon_ConvergenceTolerance:
*Yukon_DerivativeMethod_CentralDiff:
*Yukon_DerivativeMethod_ForwardDiff:
*Yukon_FeasibilityTolerance:
*Yukon_FunctionTolerance:
*Yukon_HessianUpdateMethod_Damped:
*Yukon_HessianUpdateMethod_SelfScaled:
*Yukon_Hohmann_RaiseSMA:
*Yukon_LRO2BurnApsidesRotation:
*Yukon_LRO3BurnApsidesRotation:
*Yukon_MaxFunctionEvaluations:
*Yukon_MaxIterations:
*Yukon_OptimalLunarTransfer:
*Yukon_OptimalityTolerance:
*Yukon_Problem_MarsPatchConic:
*Yukon_Problem_MinFuelLunarTransfer:
*Yukon_Problem_OptimalLCROSSTrajectory:
*Yukon_Problem_OptimalLunarApsidesRotation_2Burn:
*Yukon_Problem_SGR_P1_2:
*Yukon_Problem_TP254:
*Yukon_Problem_TP394:
Comparator errors:
None
Truth failures:
*BatchEstimator_ReportFile_AzimuthElevation [#42 failed]
*BatchEstimator_ReportFile_BRTS/BatchEstimator_ReportFile_BRTS.txt [#44
failed]
*BatchEstimator_ReportFile_Format [#42 failed]
*BatchEstimator_ReportFile_GpsPosVec [#41 failed]
*BatchEstimator_ReportFile_MultiSat_SpaceToSpace [#92 failed]
*BatchEstimator_ReportFile_Range [#42 failed]
*BatchEstimator_ReportFile_RangeRate [#42 failed]
*BatchEstimator_ReportFile_RangeSkin [#42 failed]
*BatchEstimator_ReportFile_SN/BatchEstimator_ReportFile_SN.txt [#43
failed]
*BatchEstimator_ReportFile_XEastYNorth [#42 failed]
*BatchEstimator_ReportFile_XSouthYEast [#42 failed]
*BatchEstimator_ReportStyle_Concise [#42 failed]
*BatchEstimator_ReportStyle_Debug [#42 failed]
*BatchEstimator_ReportStyle_Normal [#42 failed]
*BatchEstimator_ReportStyle_Verbose [#42 failed]
*BatchEstimator_ReportStyle_Verbose_MultiSat_SpaceToSpace [#97 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_Ex_LunarTransfer [Output field -0.553034
failed tolerance in record 4]
DynamicsModels_MultiHarmGrav_NotAPrimaryBody [#1 failed] [GMT-8282]
DynamicsModels_MultiHarmGrav_Validation_MissingPrimaryBody [#1 failed]
[GMT-8282]
*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_LEO_TDRS_EphProp_OEM_Aqua/EKFS_SpacecraftNavigation_LEO_TDRS_EphProp_OEM_Aqua_Smoother_backfilter.txt
[The test run failed to complete] [GMT-7914]
EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr/EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr_Smoother.txt
[The test run failed to complete] [GMT-8194]
EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr/EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr_Smoother_backfilter.txt
[The test run failed to complete] [GMT-8194]
*ErrorModel_SolveFors_EFM_Measurement_Bias_SnRange_Test [#1 failed]
ForceModel_External_SphericalSRP [Output field 35783.451450 failed
tolerance in record 3] [GMT-8022]
*ForceModel_Validation_Drag_DragModel_Mode [#1 failed]
*ForceModel_Validation_SRP_SRPModel_Mode [#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]
*GroundTrackPlot_RetrogradeMotion [#1 failed]
*GroundTrackPlot_Set_SolverIterations [#1 failed]
*KalmanFilter_MeasDeweightingCoefficient_RangeRate3Way [Sigma-V failed
at 17 Sep 2005 21:35:00.000]
*KalmanFilter_ReportFile [#58 failed]
*KalmanFilter_ReportFile_DSN_Moon [#59 failed]
*KalmanFilter_ReportFile_DSN_Sun [#61 failed]
*KalmanFilter_ReportFile_GpsPosVec [#58 failed]
*KalmanFilter_ReportFile_RangeRate3Way/KalmanFilter_ReportFile_RangeRate3Way.txt
[Test value 18.832575 exceeded tolerance in pattern #1]
*KalmanFilter_ReportStyle_Verbose [#58 failed]
Matlab_IO_String [] [GMT-8122]
*Optimize_Validation_Yukon_Disallowed_Sequences [ptrn 1 failed]
*Optimize_Validation_Yukon_No_Vary_Command [ptrn 1 failed]
*Optimize_Yukon_CostFunction_and_ConvergedStatus_Display [ptrn 1,2,3
failed]
*Optimize_Yukon_CostFunction_and_ConvergedStatus_Display_2 [ptrn
1,2,3,4 failed]
*Optimize_Yukon_Max_Function_Evals_Display [ptrn 1,2 failed]
*Optimize_Yukon_Max_Iterations_Display [ptrn 1,2 failed]
*Plate_SolveFors_EFM_DiffuseFraction_Test [The test run failed to
converge]
*Plate_SolveFors_EFM_SpecularFraction_Test [The test run failed to
converge]
*Plate_SolveFors_EFM_SRP_AreaCoefficient_Test [The test run failed to
converge]
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_EarthFixedInitialState [Residual failed at 01 Mar 2005
00:19:00.000] [GMT-7923]
*Smoother_ReportFile_RangeRate3Way/Smoother_ReportFile_RangeRate3Way_Smoother.txt
[Test value 0.000004 exceeded tolerance in pattern #1]
*SNOPT_LEOtoGEO_Monitored_Noopt []
*SNOPT_LEOtoGEOExact_Monitored_ObjectParameter_Noopt []
*SpacecraftNavigation_ExternalForceModel_MultiSat_TwoTdrsAndOneUser
[Parameter EstSat.EarthMJ2000Eq.VZ error 0.000001 exceeds tolerance 0.000001]
*SpacecraftNavigation_ExternalForceModel_SolveCr [Parameter
EstSat.EarthMJ2000Eq.VZ error 0.000003 exceeds tolerance 0.000002]
*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_KeplerianState_ADSF_SnDowd [The test
run failed to converge]
*SpacecraftNavigation_SolveFors_KeplerianState_DsnSeqRangeTcp2WayTcp3Way [The
test run failed to converge]
*ThrustSegment_SolveFors_EFM_ThrustScaleFactor_Test [The test run
failed to converge]
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]
*VF13AD_Tut_MultipleShootingTutorial_Step4 []
*VF13AD_Tut_MultipleShootingTutorial_Step5 []
*VF13AD_Tut_MultipleShootingTutorial_Step5_Monitered []
*Yukon_Problem_hs077_ReportData [ptrn 1,2,3,4,10,11,12,13,14,15 failed]
*Yukon_ShowProgress_Iteration [ptrn 1,2,3,4 failed]
*Yukon_ShowProgress_Parameters [ptrn 1,2 failed]
-----------------------------------------------------------------
New Issues (Deferred)
-----------------------------------------------------------------
New truth failures (deferred):
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_SnDopplerRtn_Multiple
[Parameter EstWH2K.TDRS11_SnDopplerRtnEstBias.Bias error 0.010316 exceeds
tolerance 0.010000]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_SN_OEM [The test
run failed to complete] [GMT-7914]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_SN_OEM [The test
run failed to complete] [GMT-7914]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn
[Parameter EstSat.EarthMJ2000Eq.VY error 0.000002 exceeds tolerance 0.000001]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn
[Parameter EstSat.EarthMJ2000Eq.VY error 0.000002 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):
Optimize_Yukon_Minimize_Height_on_circle_2 [GMT-6434]
Optimize_Yukon_Minimize_Height_on_circle_4 [GMT-6434]
Yukon_Hohmann_DeltaVCost [GMT-8241]
Yukon_Problem_hs077 [GMT-8241]
New comparator errors (deferred):
None
-----------------------------------------------------------------
Fixed Issues (Deferred)
-----------------------------------------------------------------
Fixed truth failures (deferred):
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_SnDopplerRtn_MultipleOther
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_SnDopplerRtn_MultipleOther
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_SnDopplerRtn_MultipleOther
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]
OCPropTest_SPAD_Drag_1deg_Bicubic_LEO [GMT-7147]
OCPropTest_SPAD_Drag_SRP_1deg_Bicubic_LEO [GMT-7147]
Optimize_Yukon_Minimize_Height_on_circle_2 [GMT-6434]
Optimize_Yukon_Minimize_Height_on_circle_4 [GMT-6434]
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_DeltaVCost [GMT-8241]
Yukon_Hohmann_LowerSMA [GMT-8241]
Yukon_Hohmann_MultipleOfSameConstraint [GMT-8241]
Yukon_Hohmann_TwoBoundsConstraint [GMT-8241]
Yukon_LEOtoGEO_AllConstraintTypes [GMT-8241]
Yukon_Problem_hs077 [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/Ubuntu-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 0.010316 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 0.000758 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_Cd_SN_OEM/EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_SN_OEM_Smoother_backfilter.txt
[The test run failed to complete] [GMT-7914]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_SN_OEM/EKFS_SpacecraftNavigation_SolveFors_CartesianState_Cd_SN_OEM_Smoother.txt
[The test run failed to complete] [GMT-7914]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_SN_OEM/EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_SN_OEM_Smoother_backfilter.txt
[The test run failed to complete] [GMT-7376]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_SN_OEM/EKFS_SpacecraftNavigation_SolveFors_CartesianState_FogmCd_SN_OEM_Smoother.txt
[The test run failed to complete] [GMT-7376]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn/EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn_Filter.txt
[Parameter EstSat.EarthMJ2000Eq.VY error 0.000002 exceeds tolerance 0.000001]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn/EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn_Smoother.txt
[Parameter EstSat.EarthMJ2000Eq.VY error 0.000002 exceeds tolerance 0.000001]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnRangeDopplerDopplerRtn/EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnRangeDopplerDopplerRtn_Filter.txt
[Parameter EstSat.EarthMJ2000Eq.VY error 0.000001 exceeds tolerance 0.000001]
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnRangeDopplerDopplerRtn/EKFS_SpacecraftNavigation_SolveFors_CartesianState_SnRangeDopplerDopplerRtn_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 0.0177967, 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]
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]
-----------------------------------------------------------------
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_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]
_______________________________________________
Gmat-buildtest mailing list
[email protected]
https://lists.sourceforge.net/lists/listinfo/gmat-buildtest
