Ubuntu test results. (Ubuntu panic averted -- My shell script that
collects data needed to be updated.)
- DJC
--
Darrel J. Conway, Ph.D. Thinking Systems, Inc.
Senior Scientist and CEO 6441 N Camino Libby
Phone: (623) 298-4530 Tucson, AZ 85718
FAX: (520) 232-2533 www.thinksysinc.com
Cell: (520) 425-3626 [email protected]
-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Ubuntu_16.04
Tested build: Ubuntu_GMAT_Console
Regression build: UbuntuBaseline
Total number of scripts: 13820 (+133 deferred)
Percent Passed: 99.96%
New issues: 2
Output changes: 0
New truth failures: 2
New crashes: 0
New script errors: 0
New comparator errors: 0
Fixed issues: 195
Total issues: 6
Test system warnings: 54
New deferred issues: 0
Fixed deferred issues: 4
Total deferred issues: 84
Run Time: 06 hours, 23 minutes, 14 seconds
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
Integrator_LEO_PD853_Accuracy []
Matlab_IO_String []
Output changes (but still pass):
None
Output changes (but still fail):
None
New crashes/hangs/etc.:
None
New script errors:
None
New comparator errors:
None
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
Antenna_Validation_Mode
BatchEstimator_Validation_Mode
Bug-GMT-5667
CelestialBody_Earth_EopFileName
CelestialBody_Earth_EopFileName_Default
CelestialBody_Earth_EopFileName_EmtpyString
CommandMode_ReportFile_Tests Delimiter and FixedWidth_Comma option
CommandMode_ReportFile_Tests Delimiter and FixedWidth_Semicolon option
CommandMode_ReportFile_Tests Delimiter and FixedWidth_Space option
CommandMode_ReportFile_Tests Delimiter and FixedWidth_Tab option
CoordinateSystem_VNBLocalvsBuiltIn
Ephem_GMAT_CCSDS_OEM_60sec
Ephem_GMAT_CCSDS_OEM_60sec_backward
Ephem_GMAT_CCSDS_OEM_60sec_backward
Ephem_GMAT_CCSDS_OEM_60sec_for_loop
Ephem_GMAT_CCSDS_OEM_60sec_if_loop
Ephem_GMAT_CCSDS_OEM_60sec_ifelse1_loop
Ephem_GMAT_CCSDS_OEM_60sec_ifelse2_loop
Ephem_GMAT_CCSDS_OEM_60sec_IterativeProcess_Optimizer
Ephem_GMAT_CCSDS_OEM_60sec_target
Ephem_GMAT_CCSDS_OEM_60sec_while_loop
Ephem_GMAT_CCSDS_OEM_60sec_with_1DV_IB
Ephem_GMAT_CCSDS_OEM_60sec_with_600secFB
Ephem_GMAT_CCSDS_OEM_3600sec
Ephem_GMAT_CCSDS_OEM_86400sec_IterativeProcess_Target_and_DynamicsChange
Ephem_GMAT_CCSDS_OEM_DefaultIntegrationStep_with_1DV_IB
Ephem_GMAT_CCSDS_OEM_ForwardProp_BackrProp_Monotonic_time
Ephem_GMAT_InitialEpoch_FinalEpoch_StepSize
EphemPropagator_Code500_CentralBody_Jupiter [GMT-5795]
EphemPropagator_Code500_CentralBody_Saturn [GMT-5795]
EphemPropagator_Code500_EphemCompare
EphemPropagator_Code500_EphemCompare_LeapSecond
EphemPropagator_Code500_EphemCompare_Moon
EphemPropagator_Code500_EphemCompare_Sun
EphemPropagator_Code500_ForwardProp_Interp [GMT-5760]
EphemPropagator_Code500_Validation_Mode
EphemStressTests_Default_and_ABM_Integrator_CCSDS_60Sec_MultipleSCs_ForwardDirection
EphemStressTests_Default_Prop_CCSDS_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection
EphemStressTests_Default_Prop_CCSDS_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect
EphemStressTests_Default_Prop_CCSDS_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
EphemStressTests_PD78_ABM_Prop_CCSDS_60Sec_Step_ForwardDirection
EphemStressTests_PD78_ABM_Prop_CCSDS_60Sec_Step_ForwardDirection
EphemStressTests_SPK_Integrator_CCSDS_60Sec_ForwardDirection
ErrorModel_NoiseSigma_TdrsDopplerHz
ErrorModel_NoiseSigma_TdrsDopplerHz2
ErrorModel_NoiseSigma_TdrsRangeKm
ErrorModel_NoiseSigma_TdrsRangeKm2
ErrorModel_SolveFors_Bias_All
ErrorModel_SolveFors_Bias_TdrsAll
ErrorModel_SolveFors_Bias_TdrsDopplerHz1
ErrorModel_SolveFors_Bias_TdrsDopplerHz2
ErrorModel_SolveFors_Bias_TdrsDopplerHzDopplerRangeRate
ErrorModel_SolveFors_Bias_TdrsDopplerHzTdrsRangeKm
ErrorModel_SolveFors_Bias_TdrsRangeKm1
ErrorModel_SolveFors_Bias_TdrsRangeKm2
ErrorModel_SolveFors_Bias_TdrsRangeKmGnRangeKm
ErrorModel_Type_All
ErrorModel_Validation_SolveFors
ErrorModel_Validation_Type
GMAT_IncludeMacro_IncludeFile_Inside_For_Loop
GMAT_IncludeMacro_MarsBPlaneTarget_All_ResourcesCommands_From_IncludeScript
GMAT_IncludeMacro_MarsBPlaneTarget_OnlyCommands_From_IncludeFile
GMAT_IncludeMacro_MarsBPlaneTarget_OnlyResourceObjects_From_IncludeFile
GMAT_IncludeMacro_Read_ThrusterAndFuelTank_From_IncludeFile
GMAT_IncludeMacro_ReadSpacecraft_Update_to_NewState
GMAT_STM_Truncation_20x20
GMAT_SunSync_EGM96_360x360
GMAT_ToggleEphemeris_MiddleOff
GMAT_ToggleEphemeris_StartOffToggleOn
GMAT_ToggleEphemeris_TwoEphemeris
GMATFunction_Function_Inside_While_If_Else_Loop_Global_SC_Subscribers_Other_Objects
GMATFunction_Global_EphemerisFile
GMATFunction_Global_EphemerisFile_With_Toggle
GMATFunction_Global_EphemerisFile_With_Toggle_2
GMATFunction_Hohmann_Targeter_Inside
Function_PassLocal_SC_In_Receive_LocalSC_Out_EphemerisFile
GMATFunction_LEOStationKeeping_Targeting_LocalSC_In_LocalSC_Out_Method_1
GMATFunction_LEOStationKeeping_Targeting_LocalSC_In_LocalSC_Out_Method_2
GMT-3371_ElapsedTimeContextBug
GroundStation_Validation_AddHardware
GroundStation_Validation_ErrorModels
GroundStation_Validation_Humidity
GroundStation_Validation_IonosphereModel
GroundStation_Validation_Mode
GroundStation_Validation_Pressure
GroundStation_Validation_Temperature
GroundStation_Validation_TroposphereModel
Receiver_Validation_Mode
Receiver_Validation_PrimaryAntenna
report_Spacecraft_Attached_hardware_Fuel_Tank_Properties_Impulsive_Burn
ReportFile_Delimiter_Comma
ReportFile_Delimiter_SemiColon
ReportFile_Delimiter_Space
ReportFile_Delimiter_Tab
ReportFile_Hardware_Thruster_parameters_ImpulsiveBurn
RunEstimator
SchattenFile_NominalCycle_Mean_JR
Simulator_Validation_AddData
Simulator_Validation_Mode
SNOPT_OverrideSpecsFile
SNOPT_SpecsFile
SpacecraftNavigation_Validation_AddHardware
SpacecraftNavigation_Validation_Cd
SpacecraftNavigation_Validation_CdSigma
SpacecraftNavigation_Validation_Cr
SpacecraftNavigation_Validation_CrSigma
SpacecraftNavigation_Validation_EstimationStateType
SpacecraftNavigation_Validation_OrbitErrorCovariance
SpacecraftNavigation_Validation_SolveFors
StatisticsAcceptFilter_DataTypes_All
StatisticsAcceptFilter_DataTypes_TdrsDopplerHz
StatisticsAcceptFilter_DataTypes_TdrsRangeKm
StatisticsAcceptFilter_DataTypes_TdrsRangeKmDopplerRangeRate
StatisticsAcceptFilter_Validation_DataTypes
StatisticsAcceptFilter_Validation_FileNames
StatisticsAcceptFilter_Validation_Trackers
StatisticsRejectFilter_Validation_DataTypes
StatisticsRejectFilter_Validation_FileNames
StatisticsRejectFilter_Validation_Trackers
StringFuncs_Sprintf_Flags_PlusSign
StringFuncs_Sprintf_InlineFormatSpec
StringFuncs_Sprintf_Length_L
Thruster_Validation_Tank_DifferentLengthThanMixtureRatio1
TrackingFileSet_AddTrackingConfig_All
TrackingFileSet_AddTrackingConfig_TdrsDopplerHz
TrackingFileSet_AddTrackingConfig_TdrsRangeKm
TrackingFileSet_RampTable_EOF
TrackingFileSet_Validation_AddTrackingConfig
TrackingFileSet_Validation_DataFilters
TrackingFileSet_Validation_FileName
Transmitter_Validation_Frequency
Transmitter_Validation_Mode
Transmitter_Validation_PrimaryAntenna
Transponder_Validation_Mode
Write_Array_LogFile_Script
Write_Array_ReportFile_Script
Write_ImpulsiveBurn_LogFile_Concise
Write_ImpulsiveBurn_LogFile_Script
Write_ImpulsiveBurn_LogFile_Verbose
Write_ImpulsiveBurn_ReportFile_Concise
Write_ImpulsiveBurn_ReportFile_Script
Write_ImpulsiveBurn_ReportFile_Verbose
Write_Mode_Function
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_Propagator_LogFile_Concise
Write_Propagator_LogFile_Script
Write_Propagator_LogFile_Verbose
Write_Propagator_ReportFile_Concise
Write_Propagator_ReportFile_Script
Write_Propagator_ReportFile_Verbose
Write_Spacecraft_LogFile_Concise
Write_Spacecraft_LogFile_Script
Write_Spacecraft_LogFile_Verbose
Write_Spacecraft_ReportFile_Concise
Write_Spacecraft_ReportFile_LogFile_Script
Write_Spacecraft_ReportFile_LogFile_Script
Write_Spacecraft_ReportFile_Script
Write_Spacecraft_ReportFile_Script_Include
Write_Spacecraft_ReportFile_Script_RunEstimator
Write_Spacecraft_ReportFile_Verbose
Fixed crashes/hangs/etc.:
None
Fixed script errors:
BatchEstimator_ReportFile_Format
BatchEstimator_ReportStyle_Concise
BatchEstimator_ReportStyle_Debug
BatchEstimator_ReportStyle_Verbose
ErrorModel_Bias_TdrsDopplerHz2
ErrorModel_Bias_TdrsDopplerHz
ErrorModel_Bias_TdrsRangeKm2
ErrorModel_Bias_TdrsRangeKm
ErrorModel_Type_TdrsDopplerHz
ErrorModel_Type_TdrsRangeKm
StatisticsRejectFilter_DataTypes_All
StatisticsRejectFilter_DataTypes_TdrsDopplerHz
StatisticsRejectFilter_DataTypes_TdrsRangeKmDopplerRangeRate
StatisticsRejectFilter_DataTypes_TdrsRangeKm
TrackingFileSet_SimTdrsDataFlag_STGT
TrackingFileSet_SimTdrsDataFlag_TDRSK
TrackingFileSet_SimTdrsNode4FrequencyBand_Kband
TrackingFileSet_SimTdrsNode4FrequencyBand_Sband
TrackingFileSet_SimTdrsNode4Frequency
TrackingFileSet_SimTdrsServiceAccessList_All
TrackingFileSet_SimTdrsServiceAccessList_MA
TrackingFileSet_SimTdrsServiceAccessList_SA1
TrackingFileSet_SimTdrsServiceAccessList_SA2
TrackingFileSet_SimTdrsSmarId_3
TrackingFileSet_SimTdrsSmarId_5
TrkFile_Est_UTDF_LEO_RangeRate
TrkFile_Est_UTDF_LEO_Range
TrkFile_SimEst_TDRS_range_Solve_Cd
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
None
Script errors:
None
Comparator errors:
None
Truth failures:
Integrator_LEO_PD853_Accuracy []
Matlab_IO_String []
OLDBatchEstimator_Nominal_Heliocentric_RangeDoppler [diff 46.0017, tol
30diff 5e-05, tol ] [GMT-5417]
SpacecraftNavigation_SolveFors_CartesianState_Cd_Cr_RangeRate [The test
run failed to converge] [GMT-5417]
SpacecraftNavigation_SolveFors_CartesianState_Cr_RangeRate [The test
run failed to converge]
TrkFile_Est_UTDF_LEO_Range [pos err 0.0105743, tol 0.01]
-----------------------------------------------------------------
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):
Simulator_Propagator_EarthPointMass_Drag [GMT-5417]
Simulator_Propagator_EarthPointMass_SRP_Drag [GMT-5417]
SpacecraftNavigation_AddHardware
Fixed crashes/hangs/etc. (deferred):
None
Fixed script errors (deferred):
TrkFile_SimEst_TDRS_range_Solve_Cr [GMT-5416, GMT-5701]
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, GMT-5701]
Math_Shadowed_Builtins [GMT-3043]
OLDBatchEstimator_EstimationEpoch [GMT-5708, GMT-5701]
OLDTransmitter_Frequency_DSN_Doppler_DeepSpace_2 [GMT-5701]
OLDTransmitter_Frequency_DSN_Doppler_DeepSpace [GMT-5701]
OLDTransmitter_Frequency_DSN_Range_DeepSpace_2 [GMT-5701]
OLDTransmitter_Frequency_DSN_Range_DeepSpace [GMT-5701]
OLDTrkFile_SimEst_DSN_DS_Range_Solve_Bias_apriori [GMT-5709]
Python_IO_String [5317]
ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522]
Transmitter_Frequency_DSN_Doppler_DeepSpace_2 [GMT-5701]
Transmitter_Frequency_DSN_Doppler_DeepSpace [GMT-5701]
Transmitter_Frequency_DSN_Range_DeepSpace_2 [GMT-5701]
Transmitter_Frequency_DSN_Range_DeepSpace [GMT-5701]
TrkFile_SimEst_DSN_DS_Range_Solve_Bias_apriori [GMT-5709]
TrkFile_SimEst_GN_RangeRate_Solve_Cd [GMT-5701]
TrkFile_SimEst_GN_RangeRate_Solve_Cr [GMT-5701]
TrkFile_SimEst_GN_range_Solve_Cd [GMT-5701]
TrkFile_SimEst_GN_range_Solve_Cr [GMT-5701]
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]
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]
EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection
[pos err 15.2471, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection
[pos err 9.57664, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect
[pos err 14.3801, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
[pos err 0.000230256, tol 1e-12] [GMT-4112]
EphemStressTests_PD78_ABM_Prop_Code500_60Sec_Step_ForwardDirection [pos
err 21.5627, 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 0.000810884,
tol 1e-06] [GMT-2567]
GMAT_LEO_PropSynchronization_BS []
GMAT_LunarTran_PropSynchronization_BS [max diff 3.39992e-07 > tol 5e-08]
GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS [pos err 0.0757314, tol 0.002]
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]
OLDSimulator_Propagator_EarthPointMass_Drag/Simulator_Propagator_EarthPointMass_Drag_PosErr.report
[diff 0.0207037, tol 4e-05] [GMT-5417]
OLDSimulator_Propagator_EarthPointMass_SRP_Drag/Simulator_Propagator_EarthPointMass_SRP_Drag_PosErr.report
[diff 0.0299541, tol 5e-05] [GMT-5417]
OLDWrite_Multiple_ReportFile_Concise_2 [] [GMT-5801]
OLDWrite_Multiple_ReportFile_Verbose_2 [#24 failed] [GMT-5801]
RejectFilter_Validation_RecordNumbers [#5 failed] [GMT-6034]
ScriptLanguage_Comments_AfterControlFlow [] [GMT-3332]
ScriptLanguage_LineContinuation_BeginningOfLine [] [GMT-3756]
ScriptLanguage_LiteralArrays_String [] [GMT-3680]
ScriptLanguage_ReferenceArrays_ForceModel_7 [] [GMT-3541]
ScriptLanguage_Validation_Semicolons_1 [no error or exception]
[GMT-3545]
Simulator_Propagator_EarthPointMass_Drag/Simulator_Propagator_EarthPointMass_Drag_PosErr.report
[diff 0.0207037, tol 4e-05] [GMT-5417]
Simulator_Propagator_EarthPointMass_SRP_Drag/Simulator_Propagator_EarthPointMass_SRP_Drag_PosErr.report
[diff 0.0299541, tol 5e-05] [GMT-5417]
SpacecraftNavigation_SolveFors_CartesianState_LeapSec_Range [Parameter
TDRS10.EarthTODEq.X value -11597.438317 exceeds tolerance 0.010000] [GMT-5954]
SpacecraftNavigation_SolveFors_CartesianState_LeapSec_RangeRate
[Parameter Aura.EarthMJ2000Eq.X value -4277.420356 exceeds tolerance 0.010000]
[GMT-5954]
SpacecraftNavigation_Validation_Mode [#1 failed] [GMT-5841]
String_AssignNumericParam [] [GMT-2888]
THF_Accel_CSA_None_NA [] [GMT-5701]
THF_Accel_ECI_None_NA_3minutes_UnitZ [] [GMT-5701]
THF_Accel_ECI_None_NA_3minutes_UnitZ_TSF [] [GMT-5701]
THF_Accel_ECI_None_NA_3minutes_UnitZ_TSF_2 [] [GMT-5701]
THF_Accel_ECI_None_NA_3minutes_UnitZ_TSF_3 [] [GMT-5701]
THF_AccelMass_CSA_None_None [] [GMT-5701]
THF_AccelMass_ECI_None_None_3minutes_UnitZ [] [GMT-5701]
THF_AccelMass_ECI_None_None_3minutes_UnitZ_TSF [] [GMT-5701]
THF_AccelMass_ECI_None_None_3minutes_UnitZ_TSF_2 [] [GMT-5701]
THF_AccelMass_ECI_None_None_3minutes_UnitZ_TSF_3 [] [GMT-5701]
THF_Sim_Accel_ConfigD_None_NA_2 [ Observable Error: 739.3 m.] [GMT-5986]
THF_ThrustMass_CSA_None_None [] [GMT-5701]
THF_ThrustMass_ECI_None_None_3minutes_UnitZ [] [GMT-5701]
THF_ThrustMass_ECI_None_None_3minutes_UnitZ_TSF_2 [] [GMT-5701]
THF_ThrustMass_ECI_None_None_3minutes_UnitZ_TSF_3 [] [GMT-5701]
TrkFile_SimEst_TDRS_range_Solve_Cr [] [GMT-5416, GMT-5701]
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_STK_CentralBody_Moon_Meters [GMT-6093]
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_Code500_ACE_OpsPrototype_v13 [GMT-4112]
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]
ErrorModel_NoiseSigma_RangeRate2 [GMT-5417]
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]
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]
Math_Validation_Cross_WrongDim2 [GMT-5676]
OLDBatchEstimator_Nominal_L1_Range [GMT-5417]
OLDWrite_Spacecraft_LogFile_Script [GMT-5802]
ScriptLanguage_Validation_DataTypes_ReferenceArray_Formation_5
[GMT-6064]
SpacePointParams_CelestialBody_EpochOutput [3939]
SpacecraftNavigation_SolveFors_CartesianState_Cd_Cr_GN [GMT-5417]
SpacecraftNavigation_SolveFors_CartesianState_Cd_RangeRate [GMT-5417]
THF_AccelMass_CSB_None_None [GMT-5701]
THF_AccelMass_CSC_None_None [GMT-5701, GMT-5981]
THF_AccelMass_CSC_None_None_2 [GMT-5701]
THF_Accel_CSB_None_NA [GMT-5701]
THF_Accel_CSC_None_None [GMT-5701, GMT-5981]
THF_Accel_CSC_None_None_2 [GMT-5701]
THF_Sim_Accel_ConfigD_None_NA [GMT-5986]
THF_ThrustMass_CSB_None_None [GMT-5701]
THF_ThrustMass_CSC_None_None [GMT-5701, GMT-5981]
THF_ThrustMass_CSC_None_None_2 [GMT-5701]
THF_ThrustMass_ECI_None_None_3minutes_UnitZ_TSF [GMT-5701]
THF_Thrust_CSA_None_NA [GMT-5701]
THF_Thrust_CSB_None_NA [GMT-5701]
THF_Thrust_CSC_None_None [GMT-5701, GMT-5981]
THF_Thrust_CSC_None_None_2 [GMT-5981]
THF_Thrust_ECI_None_NA_3minutes_UnitZ [GMT-5701]
THF_Thrust_ECI_None_NA_3minutes_UnitZ_TSF [GMT-5701]
THF_Thrust_ECI_None_NA_3minutes_UnitZ_TSF_2 [GMT-5701]
THF_Thrust_ECI_None_NA_3minutes_UnitZ_TSF_3 [GMT-5701]
Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
------------------------------------------------------------------------------
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