Test results (Red Hat 8). Optimal Control tests are disabled in this
run. (To be corrected when time permits.)
- 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 darrel.con...@thinksysinc.com
-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration:
Host: catsclaw
OS: Linux 4.18.0-553.40.1.el8_10.x86_64 #1 SMP Thu Feb 6 21:20:51 EST
2025 x86_64
Matlab Version: 24.2.0.2923080 (R2024b) Update 6
Parallel Config: Disabled
Note: RedHatEnterprise8
Tested build: RedHatEnterprise8-GMAT_Console
Regression build: Disabled
Total number of scripts: 17904 (+246 deferred)
Script Pass Percentage: 99.70%
Initialization Issues: 0
New issues: 3
Output changes: 0
New truth failures: 1
New crashes: 2
New script errors: 0
New comparator errors: 0
Fixed issues: 422
Total issues: 55
Test system warnings: 25
New deferred issues: 0
Fixed deferred issues: 5
Total deferred issues: 200
Run Time: 37 hours, 59 minutes, 52.77 seconds
-----------------------------------------------------------------
Initialization Issues
-----------------------------------------------------------------
None
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
Write_Plate_ReportFile_Script []
Output changes (but still pass):
None
Output changes (but still fail):
None
New crashes/hangs/etc.:
For_PiC_Parameter
SPICESGP4Propagator_300sec_Propagation
New script errors:
None
New comparator errors:
None
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
API_FuelTank (Python)
API_Thruster (Python)
Ballistic_and_Mass_Case_SpacecraftAndTank_CM_MOI
BatchEstimator_InversionAlgorithm_Cholesky_Singular
BatchEstimator_InversionAlgorithm_Internal_Singular
BatchEstimator_InversionAlgorithm_Schur_Singular
EphemPropagator_Code500_Validation_EndTooLate
EphemPropagator_Code500_Validation_StartTooEarly
EphemPropagator_STK_Validation_PropMultipleSats
MatAPI_FuelTank (Matlab)
MatAPI_Thruster (Matlab)
ScriptLanguage_DataTypes_Reference
ScriptLanguage_ReferenceArrays
Spacecraft_CommandMode_VisProperties
SpacecraftBallisticMass_Validation_SPADDrag_Mode
SpacecraftBallisticMass_Validation_SPADSRP_Mode
TrackingFileSet_AddTrackingConfig_None
TrkFile_two_GS_same_ID_2
Write_EphemerisFile_ReportFile_Concise
Write_EphemerisFile_ReportFile_Script
Write_EphemerisFile_ReportFile_Verbose
Write_Spacecraft_FuelTank
Write_Spacecraft_FuelTank_ScriptForm
Write_Spacecraft_MultipleObjects
Write_Spacecraft_Thruster
Fixed crashes/hangs/etc.:
None
Fixed script errors:
ACE_impulsive_493_In_FunctionMode
ACE_impulsive_493
AcceptFilter_Level2_ObservedObjects_All
CCSDS_EdgeCornerStress_ChangeModeInCommand
CoordinateSystem_Axes_LocalAlignedConstrained_StateInput
DynamicsModels_MultiHarmGrav_Earth12x12_Moon16x16_MoonCB_ReportSTM
DynamicsModels_MultiHarmGrav_Enceladus_Saturn_SaturnCB_ReportSTM
EphemPropagator_Code500_CentralBody_Earth
EphemPropagator_Code500_CentralBody_Jupiter [GMT-5795]
EphemPropagator_Code500_CentralBody_Mars
EphemPropagator_Code500_CentralBody_Moon
EphemPropagator_Code500_CentralBody_Saturn [GMT-5795]
EphemPropagator_Code500_CentralBody_Sun
EphemPropagator_Code500_CentralBody_Venus
EphemPropagator_Code500_EarthFixed
EphemPropagator_Code500_EphemCompare_LeapSecond
EphemPropagator_Code500_EphemCompare_Moon
EphemPropagator_Code500_EphemCompare_Sun
EphemPropagator_Code500_EphemCompare
EphemPropagator_Code500_EphemMerge_Moon
EphemPropagator_Code500_ForwardBackward
EphemPropagator_Code500_ForwardProp_ElapsedSecs
EphemPropagator_Code500_ForwardProp_Interp [GMT-5760]
EphemPropagator_Code500_ForwardProp
EphemPropagator_Code500_InputFormat_BigEndian
EphemPropagator_Code500_InputFormat_LittleEndian
EphemPropagator_Code500_StartEpoch_Inherit
EphemPropagator_Code500_StepSize_10min
EphemPropagator_Code500_StepSize_1min
EphemPropagator_Code500_StepSize_60min
EphemPropagator_Code500_StepToLastVector
EphemPropagator_Code500_TrueOfDate_Moon
EphemPropagator_Code500_TrueOfDate
EphemPropagator_Code500_TwoRecordsInLastBlock
EphemPropagator_Code500_Validation_CentralBody_NoEffect
EphemPropagator_CommandMode_StepSize_StartEpoch
EphemPropagator_FieldDataType_StepSize_StartEpoch
EphemPropagator_OEM_CentralBody_Venus_MJ2000Eq
EphemPropagator_STK_CentralBody_Jupiter
EphemPropagator_STK_CentralBody_Mars
EphemPropagator_STK_CentralBody_Moon_Meters
EphemPropagator_STK_CentralBody_Moon
EphemPropagator_STK_CentralBody_Saturn
EphemPropagator_STK_CentralBody_Sun
EphemPropagator_STK_CentralBody_Venus_Fixed
EphemPropagator_STK_CentralBody_Venus_MJ2000Eq
EphemPropagator_STK_CentralBody_Venus
EphemPropagator_STK_EphemCompare_LeapSecond
EphemPropagator_STK_EphemCompare_Moon
EphemPropagator_STK_EphemCompare_Sun
EphemPropagator_STK_EphemCompare
EphemPropagator_STK_ForwardBackward
EphemPropagator_STK_ForwardProp_ElapsedSecs
EphemPropagator_STK_ForwardProp
EphemPropagator_STK_OneDigitDay
EphemPropagator_STK_PropTimeJump
EphemPropagator_STK_StartEpoch_Inherit
EphemPropagator_STK_StepSize_10min
EphemPropagator_STK_StepSize_1min
EphemPropagator_STK_StepSize_60min
EphemPropagator_STK_TessEphemerisCheck
EphemPropagator_STK_Validation_CentralBody_NoEffect
EphemTest_DE405_Earth_Earth
EphemTest_DE405_Earth_Jupiter
EphemTest_DE405_Earth_Mars
EphemTest_DE405_Earth_Mercury
EphemTest_DE405_Earth_Moon
EphemTest_DE405_Earth_Neptune
EphemTest_DE405_Earth_Pluto
EphemTest_DE405_Earth_SSB
EphemTest_DE405_Earth_Saturn
EphemTest_DE405_Earth_Sun
EphemTest_DE405_Earth_Uranus
EphemTest_DE405_Earth_Venus
EphemTest_DE405_Mars_Earth
EphemTest_DE405_Mars_Jupiter
EphemTest_DE405_Mars_Mars
EphemTest_DE405_Mars_Mercury
EphemTest_DE405_Mars_Moon
EphemTest_DE405_Mars_Neptune
EphemTest_DE405_Mars_Pluto
EphemTest_DE405_Mars_SSB
EphemTest_DE405_Mars_Saturn
EphemTest_DE405_Mars_Sun
EphemTest_DE405_Mars_Uranus
EphemTest_DE405_Mars_Venus
EphemTest_DE405_Moon_Earth
EphemTest_DE405_Moon_Jupiter
EphemTest_DE405_Moon_Mars
EphemTest_DE405_Moon_Mercury
EphemTest_DE405_Moon_Moon
EphemTest_DE405_Moon_Neptune
EphemTest_DE405_Moon_Pluto
EphemTest_DE405_Moon_SSB
EphemTest_DE405_Moon_Saturn
EphemTest_DE405_Moon_Sun
EphemTest_DE405_Moon_Uranus
EphemTest_DE405_Moon_Venus
EphemTest_DE405_SSB_Earth
EphemTest_DE405_SSB_Jupiter
EphemTest_DE405_SSB_Mars
EphemTest_DE405_SSB_Mercury
EphemTest_DE405_SSB_Moon
EphemTest_DE405_SSB_Neptune
EphemTest_DE405_SSB_Pluto
EphemTest_DE405_SSB_SSB
EphemTest_DE405_SSB_Saturn
EphemTest_DE405_SSB_Sun
EphemTest_DE405_SSB_Uranus
EphemTest_DE405_SSB_Venus
EphemTest_DE405_Sun_Earth
EphemTest_DE405_Sun_Jupiter
EphemTest_DE405_Sun_Mars
EphemTest_DE405_Sun_Mercury
EphemTest_DE405_Sun_Moon
EphemTest_DE405_Sun_Neptune
EphemTest_DE405_Sun_Pluto
EphemTest_DE405_Sun_SSB
EphemTest_DE405_Sun_Saturn
EphemTest_DE405_Sun_Sun
EphemTest_DE405_Sun_Uranus
EphemTest_DE405_Sun_Venus
EphemTest_DE421_Earth_Earth
EphemTest_DE421_Earth_Jupiter
EphemTest_DE421_Earth_Mars
EphemTest_DE421_Earth_Mercury
EphemTest_DE421_Earth_Moon
EphemTest_DE421_Earth_Neptune
EphemTest_DE421_Earth_Pluto
EphemTest_DE421_Earth_Saturn
EphemTest_DE421_Earth_Sun
EphemTest_DE421_Earth_Uranus
EphemTest_DE421_Earth_Venus
EphemTest_DE421_Mars_Earth
EphemTest_DE421_Mars_Jupiter
EphemTest_DE421_Mars_Mars
EphemTest_DE421_Mars_Mercury
EphemTest_DE421_Mars_Moon
EphemTest_DE421_Mars_Neptune
EphemTest_DE421_Mars_Pluto
EphemTest_DE421_Mars_Saturn
EphemTest_DE421_Mars_Sun
EphemTest_DE421_Mars_Uranus
EphemTest_DE421_Mars_Venus
EphemTest_DE421_Moon_Earth
EphemTest_DE421_Moon_Jupiter
EphemTest_DE421_Moon_Mars
EphemTest_DE421_Moon_Mercury
EphemTest_DE421_Moon_Moon
EphemTest_DE421_Moon_Neptune
EphemTest_DE421_Moon_Pluto
EphemTest_DE421_Moon_Saturn
EphemTest_DE421_Moon_Sun
EphemTest_DE421_Moon_Uranus
EphemTest_DE421_Moon_Venus
EphemTest_DE421_Sun_Earth
EphemTest_DE421_Sun_Jupiter
EphemTest_DE421_Sun_Mars
EphemTest_DE421_Sun_Mercury
EphemTest_DE421_Sun_Moon
EphemTest_DE421_Sun_Neptune
EphemTest_DE421_Sun_Pluto
EphemTest_DE421_Sun_Saturn
EphemTest_DE421_Sun_Sun
EphemTest_DE421_Sun_Uranus
EphemTest_DE421_Sun_Venus
EphemTest_DE424_Earth_Earth
EphemTest_DE424_Earth_Jupiter
EphemTest_DE424_Earth_Mars
EphemTest_DE424_Earth_Mercury
EphemTest_DE424_Earth_Moon
EphemTest_DE424_Earth_Neptune
EphemTest_DE424_Earth_Pluto
EphemTest_DE424_Earth_Saturn
EphemTest_DE424_Earth_Sun
EphemTest_DE424_Earth_Uranus
EphemTest_DE424_Earth_Venus
EphemTest_DE424_Mars_Earth
EphemTest_DE424_Mars_Jupiter
EphemTest_DE424_Mars_Mars
EphemTest_DE424_Mars_Mercury
EphemTest_DE424_Mars_Moon
EphemTest_DE424_Mars_Neptune
EphemTest_DE424_Mars_Pluto
EphemTest_DE424_Mars_Saturn
EphemTest_DE424_Mars_Sun
EphemTest_DE424_Mars_Uranus
EphemTest_DE424_Mars_Venus
EphemTest_DE424_Moon_Earth
EphemTest_DE424_Moon_Jupiter
EphemTest_DE424_Moon_Mars
EphemTest_DE424_Moon_Mercury
EphemTest_DE424_Moon_Moon
EphemTest_DE424_Moon_Neptune
EphemTest_DE424_Moon_Pluto
EphemTest_DE424_Moon_Saturn
EphemTest_DE424_Moon_Sun
EphemTest_DE424_Moon_Uranus
EphemTest_DE424_Moon_Venus
EphemTest_DE424_Sun_Earth
EphemTest_DE424_Sun_Jupiter
EphemTest_DE424_Sun_Mars
EphemTest_DE424_Sun_Mercury
EphemTest_DE424_Sun_Moon
EphemTest_DE424_Sun_Neptune
EphemTest_DE424_Sun_Pluto
EphemTest_DE424_Sun_Saturn
EphemTest_DE424_Sun_Sun
EphemTest_DE424_Sun_Uranus
EphemTest_DE424_Sun_Venus
EphemTest_SPK_DE430_Earth_Earth
EphemTest_SPK_DE430_Earth_Jupiter
EphemTest_SPK_DE430_Earth_Mars
EphemTest_SPK_DE430_Earth_Mercury
EphemTest_SPK_DE430_Earth_Moon
EphemTest_SPK_DE430_Earth_Neptune
EphemTest_SPK_DE430_Earth_Saturn
EphemTest_SPK_DE430_Earth_Sun
EphemTest_SPK_DE430_Earth_Uranus
EphemTest_SPK_DE430_Earth_Venus
EphemTest_SPK_DE430_Mars_Earth
EphemTest_SPK_DE430_Mars_Jupiter
EphemTest_SPK_DE430_Mars_Mars
EphemTest_SPK_DE430_Mars_Mercury
EphemTest_SPK_DE430_Mars_Moon
EphemTest_SPK_DE430_Mars_Neptune
EphemTest_SPK_DE430_Mars_Saturn
EphemTest_SPK_DE430_Mars_Sun
EphemTest_SPK_DE430_Mars_Uranus
EphemTest_SPK_DE430_Mars_Venus
EphemTest_SPK_DE430_Moon_Earth
EphemTest_SPK_DE430_Moon_Jupiter
EphemTest_SPK_DE430_Moon_Mars
EphemTest_SPK_DE430_Moon_Mercury
EphemTest_SPK_DE430_Moon_Moon
EphemTest_SPK_DE430_Moon_Neptune
EphemTest_SPK_DE430_Moon_Saturn
EphemTest_SPK_DE430_Moon_Sun
EphemTest_SPK_DE430_Moon_Uranus
EphemTest_SPK_DE430_Moon_Venus
EphemTest_SPK_DE430_Sun_Earth
EphemTest_SPK_DE430_Sun_Jupiter
EphemTest_SPK_DE430_Sun_Mars
EphemTest_SPK_DE430_Sun_Mercury
EphemTest_SPK_DE430_Sun_Moon
EphemTest_SPK_DE430_Sun_Neptune
EphemTest_SPK_DE430_Sun_Saturn
EphemTest_SPK_DE430_Sun_Sun
EphemTest_SPK_DE430_Sun_Uranus
EphemTest_SPK_DE430_Sun_Venus
EphemTest_SPK_Earth_Earth
EphemTest_SPK_Earth_Jupiter
EphemTest_SPK_Earth_Mars
EphemTest_SPK_Earth_Mercury
EphemTest_SPK_Earth_Moon
EphemTest_SPK_Earth_Neptune
EphemTest_SPK_Earth_Phobos
EphemTest_SPK_Earth_Pluto
EphemTest_SPK_Earth_SSB
EphemTest_SPK_Earth_Saturn
EphemTest_SPK_Earth_Sun
EphemTest_SPK_Earth_Uranus
EphemTest_SPK_Earth_Venus
EphemTest_SPK_Earth_Vesta
EphemTest_SPK_Mars_Earth
EphemTest_SPK_Mars_Jupiter
EphemTest_SPK_Mars_Mars
EphemTest_SPK_Mars_Mercury
EphemTest_SPK_Mars_Moon
EphemTest_SPK_Mars_Neptune
EphemTest_SPK_Mars_Phobos
EphemTest_SPK_Mars_Pluto
EphemTest_SPK_Mars_SSB
EphemTest_SPK_Mars_Saturn
EphemTest_SPK_Mars_Sun
EphemTest_SPK_Mars_Uranus
EphemTest_SPK_Mars_Venus
EphemTest_SPK_Mars_Vesta
EphemTest_SPK_Moon_Earth
EphemTest_SPK_Moon_Jupiter
EphemTest_SPK_Moon_Mars
EphemTest_SPK_Moon_Mercury
EphemTest_SPK_Moon_Moon
EphemTest_SPK_Moon_Neptune
EphemTest_SPK_Moon_Phobos
EphemTest_SPK_Moon_Pluto
EphemTest_SPK_Moon_SSB
EphemTest_SPK_Moon_Saturn
EphemTest_SPK_Moon_Sun
EphemTest_SPK_Moon_Uranus
EphemTest_SPK_Moon_Venus
EphemTest_SPK_Moon_Vesta
EphemTest_SPK_SSB_Earth
EphemTest_SPK_SSB_Jupiter
EphemTest_SPK_SSB_Mars
EphemTest_SPK_SSB_Mercury
EphemTest_SPK_SSB_Moon
EphemTest_SPK_SSB_Neptune
EphemTest_SPK_SSB_Phobos
EphemTest_SPK_SSB_Pluto
EphemTest_SPK_SSB_SSB
EphemTest_SPK_SSB_Saturn
EphemTest_SPK_SSB_Sun
EphemTest_SPK_SSB_Uranus
EphemTest_SPK_SSB_Venus
EphemTest_SPK_SSB_Vesta
EphemTest_SPK_Sun_Earth
EphemTest_SPK_Sun_Jupiter
EphemTest_SPK_Sun_Mars
EphemTest_SPK_Sun_Mercury
EphemTest_SPK_Sun_Moon
EphemTest_SPK_Sun_Neptune
EphemTest_SPK_Sun_Phobos
EphemTest_SPK_Sun_Pluto
EphemTest_SPK_Sun_SSB
EphemTest_SPK_Sun_Saturn
EphemTest_SPK_Sun_Sun
EphemTest_SPK_Sun_Uranus
EphemTest_SPK_Sun_Venus
EphemTest_SPK_Sun_Vesta
Ephem_GMAT_Code500_ACE_OpsPrototype_v13
Epoch_DateFormat_Cmd
Epoch_LeapCentury
Epoch_LeapSecond_In_NoLeapSecond
Epoch_LeapSecond_MJD2G
Epoch_LeapSecond_Out_NoLeapSecond
Epoch_LeapYear_NonLeapYear
Epoch_LeapYear
Ex_MarsLaunchWindowAnalysis
FMParams_Thruster_FullPoly_EarthSat_EarthProp_3EarthThrusters_3CS_2
GMATFunction_ACE_Ops_Global_Objects_Send_GlobalSCs_As__Input_And_Output
GMATFunction_ACE_Ops_Global_Objects_Send_GlobalSCs_As__Output
GMATFunction_ACE_impulsive_493_Global_Subscribers_User_Defined_Parameters
GMATFunction_RuntimePerformance
GMT-3436b
GMT-4119
GMT-6393-CrashWithTwoEphemPropagators
GmatFunction_SystemTime_TimeAccuracy
GroundStation_Iono_DsnTcp_DeepSpace_Est
IBurn_Impulsive_Burn_Permutations_LVLH_Cmd_2
IBurn_Impulsive_Burn_Permutations_LVLH
IBurn_Impulsive_Burn_Permutations_VNB
KalmanFilter_InputWarmStartFile_GN_Moon_MoonFixed
OrbitState_CoordSysChangeDoesntChangeState
OrbitState_EpochAndCoordSysChange_Cartesian
OrbitState_EpochAndCoordSysChange_MixedReps
OrbitState_EpochFormat
Orbit_CoordinateSystemConversions
RejectFilter_FileNames_1
RejectFilter_Level2_ObservedObjects_All
RejectFilter_ObservedObjects_1
SNOPT_Ex_MarsLaunchWindowAnalysis
SNOPT_Problem_MarsPatchConic
SNOPT_Problem_OptimalLCROSSTrajectory_Monitored
SNOPT_Problem_OptimalLCROSSTrajectory
ScriptEvent_SmokeTests_EphemTest_DE405_Earth_Neptune
ScriptEvent_SmokeTests_Thruster_FullPoly_EarthSat_EarthProp_3EarthThrusters_3CS_2
ScriptLanguage_DataTypes_Enumeration
SolarSystem_EphemUpdateInterval_0
SolarSystem_EphemUpdateInterval_120
SolarSystem_EphemUpdateInterval_60
SpacecraftNavigation_IOD_Gibbs_GEO_SDO
SpacecraftNavigation_IOD_Gibbs_LEO_ISS
SpacecraftNavigation_IOD_HerrickGibbs_GEO_SDO
SpacecraftNavigation_IOD_HerrickGibbs_LEO_ISS
SpacecraftNavigation_Multisat_AquaTD6_Cd_Crosslink
SpacecraftNavigation_SolveFors_CartesianState_DSN_GEO
Spacecraft_AttitudeProp_ChangeModeinCMD_ToCommandableNadirPointing
Spacecraft_AttitudeProp_ChangeModeinCMD_ToCoordSysFixed
Spacecraft_AttitudeProp_ChangeModeinCMD_ToNadirPointing
Spacecraft_AttitudeProp_ChangeModeinCMD_ToPrecessingSpinner
Spacecraft_AttitudeProp_ChangeModeinCMD_ToSPICE
Spacecraft_AttitudeProp_ChangeModeinCMD_ToSpinner
Spacecraft_AttitudeProp_ChangeModeinCMD_ToThreeAxisKinematic
Spacecraft_CommandMode_Ballistic
StopCond_GMAT_EarthPM_FirstStepAlgorithm_MultiProps
StopCond_GMAT_EarthPM_FirstStepAlgorithm_MultiSats
StopCond_GMAT_EarthPM_FirstStepAlgorithm
StopCond_GMAT_EarthSPK_FirstStepAlgorithm
StopCond_GMAT_Earth_Synchronization
StopCond_GMAT_LunaPM_FirstStepAlgorithm
StopCond_GMAT_MoonPM_FirstStepAlgorithm_MultiProps
StopCond_GMAT_MoonPM_FirstStepAlgorithm_MultiSats
StopCond_GMAT_MoonPM_FirstStepAlgorithm
StopCond_GMAT_MoonSPK_FirstStepAlgorithm
Thruster_Finite_Burn_Permutations_Separate_Propagators_LVLH_2
Thruster_Finite_Burn_Permutations_Separate_Propagators_VNB_2
Thruster_FullPoly_EarthSat_EarthProp_3EarthThrusters_3CS_2
Thruster_O2O_Assignment_2
TrkFile_Est_DSN_DS_Range_Ramp
TrkFile_Est_DSN_DS_Range
VF13AD_Ex_MarsLaunchWindowAnalysis
VF13AD_Problem_MarsPatchConic
VF13AD_Problem_OptimalLCROSSTrajectory_Monitered
VF13AD_Problem_OptimalLCROSSTrajectory
Yukon_Problem_MarsPatchConic
Yukon_Problem_OptimalLCROSSTrajectory
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
*For_PiC_Parameter
*SPICESGP4Propagator_300sec_Propagation
Script errors:
*API_Command_MatlabFunction: (Python)
EKFS_SpacecraftNavigation_MultiHarmGrav_EarthMoonNRHO_CAPSTONE:
[GMT-8282]
ForceModel_External_SphericalSRP_FiniteBurn_RSSStep: [GMT-8022]
*MatAPI_Command_PythonFunction: (Matlab)
SpacecraftNavigation_MultiHarmGrav_EarthMoonNRHO_CAPSTONE: [GMT-8282]
Comparator errors:
*EphemerisFile_CCSDS-OEM_ReduceOrder: (truth)
*EphemerisFile_CCSDS-OEM_ReduceOrder_FiniteBurn: (truth)
Truth failures:
CoordSysTest_GMAT_EarthICRF_To_SPICE_MoonICRF [Output field
1668364.391677 failed tolerance in record 1] [GMT-5211]
CoordSysTest_GMAT_EarthMJ2000Eq_To_SPICE_IAUMars [Output field
-70724894.702716 failed tolerance in record 1] [GMT-5211]
CoordSysTest_GMAT_EarthMJ2000Eq_To_SPICE_MoonICRF [Output field
1668364.391674 failed tolerance in record 1] [GMT-5211]
CoordSysTest_GMAT_EarthMJ2000Eq_To_SPICE_MoonME [Output field
849565.610922 failed tolerance in record 1] [GMT-5211]
CoordSysTest_GMAT_SunICRF_To_SPICE_IAUMars [Output field
-70724894.702716 failed tolerance in record 1] [GMT-5211]
CoordSysTest_GMAT_SunMJ2000Eq_To_SPICE_IAUEnceladus [Output field
1294727045.068408 failed tolerance in record 1] [GMT-5211]
CoordSysTest_SPICE_EarthICRF_To_SPICE_MoonICRF [Output field
1668364.391677 failed tolerance in record 1] [GMT-5211]
CoordSysTest_SPICE_MoonPA_To_GMAT_EarthMJ2000Eq [Output field
384621.861424 failed tolerance in record 1] [GMT-5211]
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] [GMT-8282]
DynamicsModels_MultiHarmGrav_Validation_MissingPrimaryBody [#1 failed]
[GMT-8282]
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]
*EphemerisFile_CCSDS-OEM_ReduceOrder_MultipleSegments []
*EphemerisFile_ReduceOrder_WarningMessage [#1 failed]
*EphemerisFile_STK_ReduceOrder [Test ScenarioEpoch does not match truth
ScenarioEpoch]
*EphemerisFile_STK_ReduceOrder_FiniteBurn [Unable to read STK ephemeris
/home/buildbot/gmattest/output/RedHatEnterprise8-GMAT_Console/Resources/FRR-31_EphemerisFile/script/EphemerisFile_STK_ReduceOrder_FiniteBurn.e]
*EphemerisFile_STK_ReduceOrder_MultipleSegments [Unable to read STK
ephemeris
/home/buildbot/gmattest/output/RedHatEnterprise8-GMAT_Console/Resources/FRR-31_EphemerisFile/script/EphemerisFile_STK_ReduceOrder_MultipleSegments.e]
*EphemerisFile_Validation_ReduceOrder_OnePoint [#1 failed]
ForceModel_External_SphericalSRP [Output field 35783.451450 failed
tolerance in record 3] [GMT-8022]
ForceModel_Validation_Drag_DragModel_Mode [#1 failed] [GMT-8317]
ForceModel_Validation_SRP_SRPModel_Mode [#1 failed] [GMT-8317]
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]
*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]
[GMT-8318]
Simulator_EarthFixedInitialState [Residual failed at 01 Mar 2005
00:19:00.000] [GMT-7923]
*SNOPT_LEOtoGEO_Monitored []
*SNOPT_LEOtoGEO_Monitored_Noopt []
*SNOPT_Problem_OptimalLCROSSTrajectory_Monitored []
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]
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 []
*Write_EphemerisFile_OEMV2 []
*Write_Plate_ReportFile_Script []
-----------------------------------------------------------------
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):
EKFS_SpacecraftNavigation_SolveFors_CartesianState_SN_OEM_SPK_RK
Fixed crashes/hangs/etc. (deferred):
None
Fixed script errors (deferred):
Epoch_LeapSecond_G2MJD [2561]
Epoch_LeapSecond_In [2561]
Epoch_LeapSecond_Out [2561]
Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
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]
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]
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 0.010043 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]
KalmanFilter_ReportFile [#58 failed]
KalmanFilter_ReportFile_DSN_Moon [#59 failed]
KalmanFilter_ReportFile_DSN_Sun [#61 failed]
KalmanFilter_ReportFile_GpsPosVec [#58 failed]
KalmanFilter_ReportStyle_Verbose [#58 failed]
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-8293]
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]
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]
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