The most recent test system results (Red Hat).
- 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: RedHatEnterpriseWorkstation7.9
Tested build: RedHatEnterpriseWorkstation7.9-GMAT_Console
Regression build: RedHatEnterpriseWorkstation7.9Baseline
Total number of scripts: 16136 (+124 deferred)
Percent Passed: 99.08%
New issues: 28
Output changes: 0
New truth failures: 13
New crashes: 3
New script errors: 12
New comparator errors: 0
Fixed issues: 4
Total issues: 159
Test system warnings: 45
New deferred issues: 0
Fixed deferred issues: 1
Total deferred issues: 101
Run Time: 02 hours, 42 minutes, 16 seconds
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
BatchEstimator_ResetBestRMSIfDiverging [#1 failed]
TrkFile_two_GS_same_ID [ptrn 1 failed]
Write_Multiple_LogFile_Concise []
Write_Multiple_LogFile_Concise_2 []
Write_Multiple_LogFile_Script []
Write_Multiple_LogFile_Script_2 []
Write_Multiple_LogFile_Verbose []
Write_Multiple_LogFile_Verbose_2 []
Write_Multiple_ReportFile_Concise []
Write_Multiple_ReportFile_Script []
Write_Multiple_ReportFile_Script_2 []
Write_TrackingFileSet_TimeGapForPassBreak [#9 failed]
Write_TrackingFileSet_TimeGapForPassBreak [#9 failed]
Output changes (but still pass):
None
Output changes (but still fail):
None
New crashes/hangs/etc.:
CallMatlabFunction_Validation_InvalidOutputs_ArrayElementForString
EKFS_Plate_SolveFors_SpecularFraction_RandomConstant
Matlab_Validation_NonExistFunc
New script errors:
ErrorModel_Bias_Range_RangeRate2
SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn
SpacecraftNavigation_SolveFors_CartesianState_SnDowd
TrackingFileSet_ChebyshevDEBoundary_1day
TrackingFileSet_ChebyshevDEBoundary_1hour
TrackingFileSet_SimTdrsDataFlag_STGT
TrackingFileSet_SimTdrsDataFlag_TDRSK
TrackingFileSet_SimTdrsNode4FrequencyBand_Kband
TrackingFileSet_SimTdrsNode4FrequencyBand_Sband
TrackingFileSet_TaylorSeriesEnabled
TrkFile_SimEst_GN_RangeRate_Solve_Cd
TrkFile_SimEst_GN_range_Solve_Cd
New comparator errors:
None
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
None
Fixed crashes/hangs/etc.:
CoordSysTest_YAxis_N_ZAxis_-R
Events_ContactLocator_Observers_GSCartesian
ScriptLanguage_Validation_NonASCIIChars_6
Fixed script errors:
EphemPropagator_SPK_CentralBody_Earth_MJ2000Eq [GMT-7606]
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
CallMatlabFunction_Validation_InvalidOutputs_ArrayElementForString
EKFS_Plate_SolveFors_SpecularFraction_RandomConstant
Matlab_Validation_NonExistFunc
PropOffEphem_Backward_SPK
PropOffEphem_Forward_SPK
Script errors:
BatchEstimator_Propagator_STK_EarthFixed_GN:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/BatchEstimator_Propagator_STK_EarthFixed_GN.txt
does not exist
EphemPropagator_OEM_Earth_GRC_60sec: [GMT-7563]
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/EphemPropagator_OEM_Earth_GRC_60sec.txt
does not exist
EphemPropagator_OEM_Earth_ICRF_60sec: [GMT-7563]
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/EphemPropagator_OEM_Earth_ICRF_60sec.txt
does not exist
EphemPropagator_SPK_CentralBody_Earth_MJ2000Ec:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/EphemPropagator_SPK_CentralBody_Earth_MJ2000Ec_SunJ2000EqRpt.txt
does not exist
EphemPropagator_SPK_CentralBody_Moon_PA: [GMT-7606]
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/EphemPropagator_SPK_CentralBody_Moon_PA_EarthJ2000Rpt.txt
does not exist
EphemPropagator_STK_CentralBody_Moon_PA:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/EphemPropagator_STK_CentralBody_Moon_PA_EarthJ2000Rpt.txt
does not exist
EphemPropagator_STK_CentralBody_Sun_Fixed:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/EphemPropagator_STK_CentralBody_Sun_Fixed_BodyJ2000Rpt.txt
does not exist
EphemPropagator_STK_CentralBody_Venus_Fixed:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/EphemPropagator_STK_CentralBody_Venus_Fixed_EarthJ2000Rpt.txt
does not exist
ErrorModel_Bias_Range_RangeRate2:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/ErrorModel_Bias_Range_RangeRate2.txt
does not exist
MatAPI_PrecessingSpinner: (MatAPI) [GMT-7595]
ERROR MESSAGE: GMAT MATLAB API failed with status 1
SPICESGP4Propagator_NoSpacecraftDateFormatEpoch:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SPICESGP4Propagator_NoSpacecraftDateFormatEpoch.txt
does not exist
SPICESGP4Propagator_TwoLineTLE:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SPICESGP4Propagator_TwoLineTLE.txt
does not exist
SpacecraftNavigation_IOD_ChooseGibbs_LEO_GN:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_ChooseGibbs_LEO_GN.txt
does not exist
SpacecraftNavigation_IOD_ChooseHerrickGibbs_LEO_GN:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_ChooseHerrickGibbs_LEO_GN.txt
does not exist
SpacecraftNavigation_IOD_Gibbs_GEO_GN:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_Gibbs_GEO_GN.txt
does not exist
SpacecraftNavigation_IOD_Gibbs_GEO_SDO:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_Gibbs_GEO_SDO.txt
does not exist
SpacecraftNavigation_IOD_Gibbs_LEO_FullFM_GN:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_Gibbs_LEO_FullFM_GN.txt
does not exist
SpacecraftNavigation_IOD_Gibbs_LEO_GN:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_Gibbs_LEO_GN.txt
does not exist
SpacecraftNavigation_IOD_Gibbs_LEO_ISS:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_Gibbs_LEO_ISS.txt
does not exist
SpacecraftNavigation_IOD_HerrickGibbs_Cislunar_GN:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_HerrickGibbs_Cislunar_GN.txt
does not exist
SpacecraftNavigation_IOD_HerrickGibbs_GEO_FullFM_GN:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_HerrickGibbs_GEO_FullFM_GN.txt
does not exist
SpacecraftNavigation_IOD_HerrickGibbs_GEO_GN:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_HerrickGibbs_GEO_GN.txt
does not exist
SpacecraftNavigation_IOD_HerrickGibbs_GEO_SDO:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_HerrickGibbs_GEO_SDO.txt
does not exist
SpacecraftNavigation_IOD_HerrickGibbs_LEO_GN:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_HerrickGibbs_LEO_GN.txt
does not exist
SpacecraftNavigation_IOD_HerrickGibbs_LEO_ISS:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_HerrickGibbs_LEO_ISS.txt
does not exist
SpacecraftNavigation_IOD_SpecifyMu:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_SpecifyMu.txt
does not exist
SpacecraftNavigation_IOD_Vallado:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_IOD_Vallado.txt
does not exist
SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_SolveFors_CartesianState_SnDopplerRtn.txt
does not exist
SpacecraftNavigation_SolveFors_CartesianState_SnDowd:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/SpacecraftNavigation_SolveFors_CartesianState_SnDowd.txt
does not exist
TrackingFileSet_ChebyshevDEBoundary_1day:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/TrackingFileSet_ChebyshevDEBoundary_1day.gmd
does not exist
TrackingFileSet_ChebyshevDEBoundary_1hour:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/TrackingFileSet_ChebyshevDEBoundary_1hour.gmd
does not exist
TrackingFileSet_SimTdrsDataFlag_STGT:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/TrackingFileSet_SimTdrsDataFlag_STGT.gmd
does not exist
TrackingFileSet_SimTdrsDataFlag_TDRSK:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/TrackingFileSet_SimTdrsDataFlag_TDRSK.gmd
does not exist
TrackingFileSet_SimTdrsNode4FrequencyBand_Kband:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/TrackingFileSet_SimTdrsNode4FrequencyBand_Kband.gmd
does not exist
TrackingFileSet_SimTdrsNode4FrequencyBand_Sband:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/TrackingFileSet_SimTdrsNode4FrequencyBand_Sband.gmd
does not exist
TrackingFileSet_TaylorSeriesEnabled:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/TrackingFileSet_TaylorSeriesEnabled.txt
does not exist
TrkFile_SimEst_GN_RangeRate_Solve_Cd:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/TrkFile_SimEst_GN_RangeRate_Solve_Cd.report
does not exist
TrkFile_SimEst_GN_range_Solve_Cd:
ERROR MESSAGE: Output file
~/gsfcgmat/TestTarget/GMAT-R2020a-Linux-x64/output/TrkFile_SimEst_GN_range_Solve_Cd.report
does not exist
Comparator errors:
EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_CCSDS: (truth)
[GMT-7483]
ERROR MESSAGE: Comparator STKEphemerisComparator failed: Output argument
"ephStruct" (and maybe others) not assigned during call to
"comparator.STKEphemerisComparator.Compare>read_stk_eph".
Truth failures:
API_PrecessingSpinner (API) [#1 failed] [GMT-7595]
API_ScriptFunctions (API) [#16 failed]
API_ScriptTest (API) [#1 failed]
BatchEstimator_Propagator_STK_TDRS_Multiple_EarthFixed [Parameter
EstSat.EarthMJ2000Eq.X error 0.099521 exceeds tolerance 0.005000] [GMT-7289]
BatchEstimator_ReportStyle_Verbose_MultiSat_SpaceToSpace [#177 failed]
BatchEstimator_ResetBestRMSIfDiverging [#1 failed]
EKFS_EphemerisFile_STK_PredDv/EKFS_EphemerisFile_STK_PredDv_Filter.e
[Test NumberOfCovariancePoints does not equal truth NumberOfCovariancePoints]
[GMT-7483]
EKFS_EphemerisFile_STK_PredDv/EKFS_EphemerisFile_STK_PredDv_Smoother.e
[Test NumberOfCovariancePoints does not equal truth NumberOfCovariancePoints]
[GMT-7483]
EKFS_EphemerisFile_STK_PredDv/EKFS_EphemerisFile_STK_PredDv_Filter.report
[Found 4466 output records and 4465 truth records] [GMT-7483]
EKFS_EphemerisFile_STK_PredDv/EKFS_EphemerisFile_STK_PredDv_Smooth.report
[Found 4466 output records and 4465 truth records] [GMT-7483]
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_GN/EKFS_ErrorModel_SolveFors_Bias_RandomConstant_GN_Smoother_backfilter.txt
[Parameter EstMAD.EstSat_EstRangeModel.Bias error 0.118138 exceeds tolerance
0.020000] [GMT-7434-Linux]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_Filter.e
[Test NumberOfCovariancePoints does not equal truth NumberOfCovariancePoints]
[GMT-7483]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_Smoother.e
[Test NumberOfCovariancePoints does not equal truth NumberOfCovariancePoints]
[GMT-7483]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_SmoEph/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_SmoEph_Smoother.e
[Test NumberOfCovariancePoints does not equal truth NumberOfCovariancePoints]
[GMT-7483]
EKFS_SpacecraftNavigation_OrbitErrorCovariance_GN_Moon [Failed to find
a covariance record at 10 Sep 2005 00:00:00.000] [GMT-6801]
EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr/EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr_Smoother_backfilter.txt
[Parameter STEREO_B.SunMJ2000Eq.X error 0.177174 exceeds tolerance 0.015000]
[GMT-7278-Linux]
EKFS_ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_GpsPosVec/EKFS_ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_GpsPosVec_Smoother_backfilter.txt
[Parameter FM.Est_Thruster1_SetPoint1.ThrustAngle1.C0 error 14.780763 exceeds
tolerance 0.005000] [GMT-7483]
EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_CCSDS [#4335 failed]
[GMT-7483]
EphemerisFile_SPK_GetEphemStates_Sun_MJ2000Ec [Output field
94210467.402783 failed tolerance in record 1] [GMT-7602]
EphemPropagator_OEM_CentralBody_Venus_MJ2000Eq/EphemPropagator_OEM_CentralBody_Venus_MJ2000Eq_VenusFixedRpt.txt
[pos err 1.6145e+08, tol 5e-06] [GMT-7598]
EphemPropagator_OEM_CentralBody_Venus_MJ2000Eq/EphemPropagator_OEM_CentralBody_Venus_MJ2000Eq_VenusJ2000Rpt.txt
[pos err 1.6145e+08, tol 3e-08] [GMT-7598]
EphemPropagator_OEM_CentralBody_Venus_MJ2000Eq/EphemPropagator_OEM_CentralBody_Venus_MJ2000Eq_EarthJ2000Rpt.txt
[pos err 1.6145e+08, tol 0.0005] [GMT-7598]
EphemPropagator_SPK_CentralBody_Earth_MJ2000Eq/EphemPropagator_SPK_CentralBody_Earth_MJ2000Eq_EarthJ2000Rpt.txt
[pos err 0.00127621, tol 5e-06] [GMT-7606]
EphemPropagator_SPK_CentralBody_Earth_MJ2000Eq/EphemPropagator_SPK_CentralBody_Earth_MJ2000Eq_SunJ2000Rpt.txt
[pos err 0.00575362, tol 0.0001] [GMT-7606]
EphemPropagator_SPK_CentralBody_Moon_MJ2000Eq/EphemPropagator_SPK_CentralBody_Moon_MJ2000Eq_BodyFixedRpt.txt
[pos err 0.00060908, tol 5e-05] [GMT-7606]
EphemPropagator_SPK_CentralBody_Moon_MJ2000Eq/EphemPropagator_SPK_CentralBody_Moon_MJ2000Eq_BodyJ2000Rpt.txt
[pos err 0.00061091, tol 1e-06] [GMT-7606]
EphemPropagator_SPK_CentralBody_Moon_MJ2000Eq/EphemPropagator_SPK_CentralBody_Moon_MJ2000Eq_EarthJ2000Rpt.txt
[pos err 0.00102931, tol 5e-05] [GMT-7606]
EphemPropagator_StartEpoch_A1Gregorian [pos err 0.0409948, tol 0.0016]
EphemPropagator_StartEpoch_A1ModJulian [pos err 0.0420186, tol 0.0016]
EphemPropagator_StartEpoch_ChangeInMission [pos err 0.0420186, tol
0.0016]
EphemPropagator_StartEpoch_FromSpacecraft [pos err 0.0420186, tol
0.0016]
EphemPropagator_StartEpoch_TAIGregorian [pos err 0.0420186, tol 0.0016]
EphemPropagator_StartEpoch_TAIModJulian [pos err 0.0420177, tol 0.0016]
EphemPropagator_StartEpoch_TDBGregorian [pos err 0.0421713, tol 0.0019]
EphemPropagator_StartEpoch_TDBModJulian [pos err 0.0420169, tol 0.0016]
EphemPropagator_StartEpoch_TTGregorian [pos err 0.0420194, tol 0.0016]
EphemPropagator_StartEpoch_TTModJulian [pos err 0.0420177, tol 0.0016]
EphemPropagator_StartEpoch_UTCGregorian [pos err 0.0420186, tol 0.0016]
EphemPropagator_StartEpoch_UTCModJulian [pos err 0.0420186, tol 0.0016]
Events_IntrusionLocator_MinimumPhase_MinValue [diff # events]
Events_IntrusionLocator_MultipleIntrudingBodies_Cone_FixedGrid [diff #
events]
Events_IntrusionLocator_SingleIntrudingBody_Cone_FixedGrid [diff #
events]
Events_IntrusionLocator_SingleIntrudingBody_LightTimeDelay_StellarAberration
[diff # events]
Events_IntrusionLocator_SingleIntrudingBody_MultipleSensors_FixedGrid
[diff # events]
Events_IntrusionLocator_SingleIntrudingBody_Rectangular_FixedGrid
[epoch diff = 2138572.346007s (event 653)]
Events_IntrusionLocator_StepSizeLarge [epoch diff = 2.256998s (event
40)]
Events_IntrusionLocator_StepSizeSmall [diff # events]
Events_IntrusionLocator_UserDefinedInterval [epoch diff = 2.239004s
(event 68)]
ForceModel_Validation_NoSPKforUserBody [no error or exception]
GMAT_Mars1_Mars_0_MarsGRAM2005_0_NonDefaultF107 [pos err 0.000406033,
tol 0.0003]
GroundStation_Iono_Range_DeepSpace [Found 13688 output records and
13695 truth records] [GMD-7061]
KalmanFilter_MatlabFile_GN_Moon [Variable EstimationConfig.StateNames
did not match at index 1] [GMT-6801]
KalmanFilter_Smoother_PredictTimeSpan_Both_OEM/KalmanFilter_Smoother_PredictTimeSpan_Both_OEM_filter.oem
[#1442 failed] [GMT-6949]
MatAPI_Epoch_LeapSecond_In (MatAPI) [#7 failed] [2561]
MatAPI_Epoch_LeapSecond_Out (MatAPI) [#7 failed] [2561]
MatAPI_LoadAndRunScript (MatAPI) [#3 failed]
MatAPI_MJ2000Ec (MatAPI) [#6 failed]
MatAPI_MJ2000Eq (MatAPI) [#12 failed]
MatAPI_PD45PropagationE8x8SMPM (MatAPI) [pos err 0.000753373, tol
1e-07]
MatAPI_ScriptFunctions (MatAPI) [#16 failed]
MatAPI_ScriptTest (MatAPI) [#2 failed]
Plate_Validation_PlateNormalHistoryFile [#1 failed] [GMT-7022]
RotationMatrixTest_MercuryMJ2000Ec [max diff 1.09735e-09 > tol 1e-12]
[GMT-7223]
Simulator_Propagator_SPK_MoonOccultation [#66 failed] [GMT-7289]
Simulator_Propagator_SPK_MultipleOccultation [#1 failed] [GMT-7289]
Simulator_Propagator_SPK_TDRS [Residual failed at 01 Mar 2005
01:00:00.000] [GMT-7289]
Simulator_Propagator_STK_TDRS [Residual failed at 01 Mar 2005
01:00:00.000] [GMT-7289]
Smoother_MatlabFile_BackfilterMatfileCorruption [Found extra field
BackwardComputed] [GMT-6949]
Spacecraft_Validation_AddPlates [#1 failed] [GMT-7022]
SpacecraftNavigation_IOD_Verbose_SpecifyGibbs [#1 failed]
SpacecraftNavigation_IOD_Verbose_SpecifyHerrickGibbs [#1 failed]
SpacecraftNavigation_LEO_TDRS_Aqua [The test run failed to converge]
SpacecraftNavigation_LEO_TDRS_EphProp_OEM_LeapSec_Terra [Residual
failed at 31 Dec 2016 23:55:00.000] [GMT-7598]
SpacecraftNavigation_Moon_DsnTcp_RangeRate_LRO_EarthInitialState_MoonFM_KeplerianState
[The test run failed to converge] [GMT-7515]
SpacecraftNavigation_Multisat_AquaTD6_Cd [The test run failed to
converge]
SpacecraftNavigation_Multisat_AquaTD6_Cd_Cr [The test run failed to
converge]
SpacecraftNavigation_Multisat_AquaTD6_Cd_Crosslink [The test run failed
to converge]
SpacecraftNavigation_Multisat_AquaTD6TD10_Cd_Cr [The test run failed to
converge]
SpacecraftNavigation_Multisat_GN_AquaTD10_Cd_Cr [The test run failed to
converge]
SpacecraftNavigation_MultiSat_J2000_EarthFixed [Residual failed at 01
Mar 2005 01:00:00.000] [GMT-7421]
SpacecraftNavigation_Multisat_SpaceToSpace_AquaTD10_Cd_Cr [The test run
failed to converge]
SpacecraftNavigation_MultiSat_TdrsAndUser_Cd_Cr [The test run failed to
converge]
SpacecraftNavigation_Multisat_TTC_AquaTD10_Cd_Cr [The test run failed
to converge]
SpacecraftNavigation_Multisat_TTC_GN_SN_AquaTD10_Cd_Cr [The test run
failed to converge]
SpacecraftNavigation_MultiSat_TwoTdrsAndOneUser [The test run failed to
converge]
SpacecraftNavigation_MultiSat_TwoTdrsAndTwoUser [The test run failed to
converge]
SpacecraftNavigation_MultiSat_TwoTdrsAndTwoUser_Cd_Cr [The test run
failed to converge]
SpacecraftNavigation_MultiSat_TwoTdrsAndTwoUser_Cd_Cr_Bias [The test
run failed to converge]
SpacecraftNavigation_SimEphProp_MixedInitialFrame_TDRS [Residual failed
at 01 Mar 2005 01:20:00.000] [GMT-7289]
SpacecraftNavigation_SPADSRPScaleFactorSigma_ConstrainInc [#3 failed]
[GMT-7078, Linux only]
SPICESGP4Propagator_CanaryTest_Propagation [pos err 2.15371e-06, tol
1e-09]
ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_EpochAfterBurn_GpsPosVec
[The test run failed to converge] [GMT-7483]
ThrustSegment_SolveFors_ThrustAngles_Constant_ThreeAxisKinematic_EpochAfterBurn_GpsPosVec
[The test run failed to converge] [GMT-7483]
ThrustSegment_SolveFors_ThrustAngles_ThrustScaleFactor_Cr_DSN_Keplerian
[Parameter EstSat.EarthMJ2000Eq.AOP error 0.618140 exceeds tolerance 0.500000]
[GMT-7483]
TrackingFileSet_AddTrackingConfig_DsnSeqRange [#1 failed] [GMR-7061]
TrackingFileSet_AddTrackingConfig_DsnTcp [#1 failed] [GMR-7061]
TrackingFileSet_AddTrackingConfig_Range [#1 failed] [GMR-7061]
TrackingFileSet_AddTrackingConfig_RangeRate [#1 failed] [GMR-7061]
TrackingFileSet_FileName2 [#2 failed] [GMR-7061]
Transponder_HardwareDelay_Sim_Range [GMAT: 617 lines, Truth: 619 lines]
[GMR-7061]
Transponder_HardwareDelay_Sim_Range_RangeSkin [GMAT: 65 lines, Truth:
66 lines] [GMR-7061]
Transponder_HardwareDelay_Sim_RangeSkin [GMAT: 65 lines, Truth: 66
lines] [GMR-7061]
TrkFile_two_GS_same_ID [ptrn 1 failed]
Write_Multiple_LogFile_Concise []
Write_Multiple_LogFile_Concise_2 []
Write_Multiple_LogFile_Script []
Write_Multiple_LogFile_Script_2 []
Write_Multiple_LogFile_Verbose []
Write_Multiple_LogFile_Verbose_2 []
Write_Multiple_ReportFile_Concise []
Write_Multiple_ReportFile_Script []
Write_Multiple_ReportFile_Script_2 []
Write_Spacecraft_NavigationHardware [#1 failed] [GMT-7578]
Write_TrackingFileSet_TimeGapForPassBreak [#9 failed]
Write_TrackingFileSet_TimeGapForPassBreak [#9 failed]
-----------------------------------------------------------------
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):
TrkFile_SimEst_TDRS_range_Solve_Cr [GMT-5416]
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
Smoother_Filter_ProcessNoiseTimeStep_0sec_SN [GMT-7376]
Script errors (deferred):
BatchEstimator_EstimationEpoch [GMT-5708]
EKFS_ErrorModel_SolveFors_PassBiases_GN
EKFS_SpacecraftNavigation_LEO_TDRS_Aqua_FogmCd [GMT-7376]
EKFS_SpacecraftNavigation_MultiSat_TdrsAndUser_DifferentProcessNoise
[GMT-7421]
EKFS_SpacecraftNavigation_MultiSat_TdrsAndUser
EKFS_SpacecraftNavigation_Multisat_AquaTD6_Cd
EKF_SpacecraftNavigation_OrbitErrorCovariance_Keplerian_GpsPosVec
EKF_SpacecraftNavigation_SolveFors_KeplerianState_Cd_RandomConstant_GN
EKF_SpacecraftNavigation_SolveFors_KeplerianState_Cr_RandomConstant_DSN
EKF_SpacecraftNavigation_SolveFors_KeplerianState_GN
EKF_SpacecraftNavigation_SolveFors_KeplerianState_GpsPosVec
KalmanFilter_InputWarmStartFile_GN_Moon_Keplerian [GMT-6801]
KalmanFilter_InputWarmStartFile_GpsPosVec_KeplerianToCartesian
[GMT-6801]
KalmanFilter_OutputWarmStartFile_GpsPosVec_Keplerian [GMT-6801]
KalmanFilter_Propagator_Multiple_MixedCentralBody [GMT-7421]
KalmanFilter_Propagator_Multiple_SunEarthMoon [GMT-7421]
KalmanFilter_Propagator_SN
KalmanFilter_Propagator_SPK_TDRS_Multiple
KalmanFilter_Propagator_SPK_TDRS
KalmanFilter_Propagator_STK_TDRS_Multiple
KalmanFilter_Propagator_STK_TDRS
Math_Shadowed_Builtins [GMT-3043]
OCPropTest_SPAD_Drag_1deg_Bicubic_LEO [GMT-7147]
OCPropTest_SPAD_Drag_SRP_1deg_Bicubic_LEO [GMT-7147]
Python_IO_String [5317]
ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522]
THF_Sim_Accel_ConfigD_None_NA_2 [GMT-6451]
THF_Sim_Accel_ConfigD_None_NA_3 [GMT-6451]
THF_Sim_Accel_ConfigD_None_NA_4 [GMT-6451]
THF_Sim_Accel_ConfigD_None_NA [GMT-6451]
THF_Sim_Thrust_CSF2_None_NA_ZeroTSF [GMT-6451]
ThrustHistoryFile_EstimateTSF_EpochBeforeBurn_RSSStep_Aqua [GMT-6451]
ThrustSegment_SolveFors_ThrustScaleFactor_Multiple_RSSStep [GMT-6451]
ThrustSegment_SolveFors_ThrustScaleFactor_RSSStep [GMT-6451]
TrkFile_SimEst_DSN_DS_Range_Solve_Bias_apriori [GMT-5709]
Comparator errors (deferred):
GroundStation_Iono_Range_Kband (truth) [GMT-5644]
GroundStation_Iono_RangeRate_Kband (truth) [GMT-5644]
GroundStation_TropoIono_Range_Kband (truth) [GMT-5644]
Truth failures (deferred):
AcceptFilter_Validation_RecordNumbers [#5 failed] [GMT-6034]
Achieve_Validation_LHS_Field [ptrn 1 failed] [GMT-3687]
Achieve_Validation_RHS_Field [no error or exception] [GMT-3687]
BatchEstimator_NormalMatrixReduction_UseInitialCovariance [#1 failed]
[GMT-7274]
BatchEstimator_ReportFile_InitialState [#1 failed]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond_Filter.e
[EphemerisTimePosVel failed epoch tolerance at row 988] [GMT-7291, GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond_Smoother.e
[EphemerisTimePosVel failed epoch tolerance at row 988] [GMT-7291, GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond_Filter.mat
[Found extra field CartesianStateNames] [GMT-7291, GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond_Smoother.mat
[Found extra field CartesianStateNames] [GMT-7291, GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond.tab
[Output field 0.000751 failed tolerance in record 575] [GMT-7291, GMT-7398]
EKFS_SpacecraftNavigation_MultiSat_DifferentInitialEpochs [#1 failed]
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]
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 15.2546, 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 14.3171, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
[pos err 0.000219127, tol 1e-12] [GMT-4112]
EphemStressTests_PD78_ABM_Prop_Code500_60Sec_Step_ForwardDirection [pos
err 21.5632, tol 1e-12] [GMT-4112]
EphemStressTests_SPK_Integrator_Code500_60Sec_ForwardDirection [pos err
0.000427977, tol 1e-12] [GMT-4112]
Epoch_LeapSecond_G2MJD [max mjd diff 1.000259s > tol 0.001000s] [2561]
Epoch_LeapSecond_In [max greg. diff 1.000005s > tol 0.001000s] [2561]
Epoch_LeapSecond_Out [max mjd diff 1.000146s > tol 0.001000s] [2561]
Formation_Validation_MissingComma [no error or exception] [GMT-3672]
GMAT_ISS_Earth_JGM2_0_0_NutationUpdateInterval [pos err 0.000808928,
tol 1e-06] [GMT-2567]
GMAT_LEO_PropSynchronization_BS []
GMAT_LunarTran_PropSynchronization_BS [max diff 2.79401e-07 > tol 5e-08]
GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS [pos err 0.0760295, tol 0.002]
GroundStation_Tropo_TRK223_DsnTcp_OREX/GroundStation_Tropo_TRK223_DsnTcp_OREX.txt
[Residual failed at 02 Feb 2021 09:25:00.000] [GMT-7455]
KalmanFilter_InputWarmStartFile_SN [Output field -4638.170949 failed
tolerance in record 1] [GMT-7376]
KalmanFilter_Propagator_Multiple_NonParticipatingSpacecraft [ptrn 1
failed]
KalmanFilter_Propagator_Multiple_SpacecraftDoesNotExist [ptrn 1 failed]
KalmanFilter_Propagator_Multiple_UnassignedSpacecraft [ptrn 1 failed]
KalmanFilter_WarmStartEpoch_SN [Output field -4638.170949 failed
tolerance in record 1] [GMT-7376]
Math_Inf [GMAT: 53 lines, Truth: 69 lines] [GMT-3195]
Minimize_Validation_Field [ptrn 1 failed] [GMT-3687]
Nonlinear_Validation_LHS_Field [ptrn 1 failed] [GMT-3687]
Nonlinear_Validation_RHS_Field [ptrn 1 failed] [GMT-3687]
Optimize_Yukon_Minimize_Height_on_circle_2 [diff 497, tol 0.001]
Optimize_Yukon_Minimize_Height_on_circle_4 [diff 497, tol 0.001]
RejectFilter_Validation_RecordNumbers [#5 failed] [GMT-6034]
ScriptLanguage_Comments_AfterControlFlow [] [GMT-3332]
ScriptLanguage_LiteralArrays_String [] [GMT-3680]
ScriptLanguage_ReferenceArrays_ForceModel_7 [] [GMT-3541]
ScriptLanguage_Validation_Semicolons_1 [no error or exception]
[GMT-3545]
Smoother_PredictTimeSpan_STK_SN [Test ScenarioEpoch does not match
truth ScenarioEpoch] [GMT-7376]
SpacecraftNavigation_MultiSat_SpaceToSpace_SharedBias_Angles [The test
run failed to converge] [GMT-7421]
SpacecraftNavigation_TDRS_SecondGen_MA2_Landsat7 [Residual failed at 28
Aug 2015 19:41:22.000] [GMT-7376]
SpacecraftNavigation_TDRS_SecondGen_MA4_Landsat7 [Failed to find a
SN_Range residual record at 28 Aug 2015 19:41:12.000] [GMT-7376]
SpacecraftNavigation_Validation_Mode [#1 failed] [GMT-5841]
String_AssignNumericParam [] [GMT-2888]
ThrustSegment_SolveFors_ThrustScaleFactor_SN [Parameter
EstSat.EarthMJ2000Eq.VZ error 0.000001 exceeds tolerance 0.000001]
ThrustSegment_ThrustAngle1_Cubic [diff. num. lines] [GMT-7483]
TrackingFileSet_InconsistentSpacecraftState [Output field
-1254560.770370 failed tolerance in record 1] [GMT-7553]
Vary_Validation_RHS_Field [no error or exception] [GMT-3687]
Write_Multiple_ReportFile_Concise_2 [#24 failed] [GMT-5801]
Write_Multiple_ReportFile_Verbose [#24 failed]
Write_Multiple_ReportFile_Verbose_2 [#24 failed] [GMT-5801]
-----------------------------------------------------------------
Test System Warnings
-----------------------------------------------------------------
Passing tests tagged with bugs:
(To fix, remove bug ID from Bugs key in .tc file)
Comet_Validation_OrientationEpoch_3 [GMT-3252]
CoordSysTest_Luna_MJ2000Eq_To_ICRF [GMT-3227]
CoordinateSystem_Validation_Axes_4 [GMT-3155]
EphemPropagator_Code500_CentralBody_Jupiter [GMT-5795]
EphemPropagator_Code500_CentralBody_Saturn [GMT-5795]
EphemPropagator_Code500_ForwardProp_Interp [GMT-5760]
EphemPropagator_OEM_Usable_Start_Stop [GMT-7563]
EphemPropagator_SatAssigmentToNewSatThenProp [GMT-3434]
EphemStressTests_Default_Prop_STK_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection
[GMT-6090]
EphemStressTests_Default_Prop_STK_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect
[GMT-6090]
Ephem_GMAT_SPK_60sec_backward [GMT-5286]
Ephem_GMAT_SPK_DefaultIntegrationStep_User_Defined_LagrangeOrder
[GMT-5286]
Ephem_GMAT_STK_60sec_IterativeProcess_Optimizer [GMT-6090]
Ephem_GMAT_STK_60sec_IterativeProcess_Optimizer_NoBoundaries [GMT-6090]
Events_ContactLocator_Ephemeris_DE405AllPlanets [GMT-5377]
Events_ContactLocator_Ephemeris_DE424AllPlanets [GMT-5377]
Events_ContactLocator_Heo2 [GMT-5302]
Events_ContactLocator_UseEntireInterval_False_MissionSequence [GMT-5292]
Ex_GmatFunction [GMT-3604]
FMParams_GMAT_UserAsteroid(OSIRIS)_HarmonicGravity_SRP_PointMasses
[GMT-6955]
ForceModel_SPAD_Drag_1deg_Bicubic_Mars [Linux, Mac]
ForceModel_SPAD_Drag_1deg_Bilinear_Mars [Linux, Mac]
Formation_Validation_PropFormSatInTwoProps [GMT-3581]
GMAT_GEO_EarthSunMoon_0_0_0_Relativity [3405]
GMAT_GEO_EarthSun_0_0_0_Relativity [3405]
GMAT_ISS_EarthSunMoon_0_0_0_Relativity [3405]
GMAT_ISS_EarthSunMoon_0_0_0_Relativity_Cmd [3405]
GMAT_ISS_EarthSun_0_0_0_Relativity [3405]
IntegratedFlyby_MarsFlyby [GMT-7169]
KalmanFilter_TimeUpdate_GpsPosVec [GMT-6801]
MatAPI_Functions [GMT-7597]
Math_Validation_Cross_WrongDim2 [GMT-5676]
Phase_EpochFormat_TAIGregorian [GMT-7168]
Phase_Type_Radau [GMT-7168]
ScriptLanguage_LineContinuation_BeginningOfLine [GMT-3756]
ScriptLanguage_Validation_DataTypes_ReferenceArray_Formation_5
[GMT-6064]
Simulator_Propagator_EarthPointMass_Drag [GMT-5417]
SpacePointParams_CelestialBody_EpochOutput [3939]
SpacecraftNavigation_CdSigma_Range_MSISE86 [GMT-6829 Linux only]
SpacecraftNavigation_SPADDragScaleFactorSigma_ConstrainInc [GMT-7078,
Ubuntu only]
SpacecraftNavigation_SPADDragScaleFactorSigma_GN_MSISE86 [GMT-6829
Linux only]
SpacecraftNavigation_SolveFors_CartesianState_SPADDragScaleFactor_GN_MSISE86
[GMT-6829 Linux only]
Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
TrkFile_SimEst_TDRS_range_Solve_Cr [GMT-5416]
Tut_MultipleShootingTutorial_Step3 [GMT-7280]
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