-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Windows 7/MATLAB R2017a/VS 2013
Tested build: 2018-01-16
Regression build: 2018-01-03
Total number of scripts: 13702 (+133 deferred)
Percent Passed: 99.63%
New issues: 66
Output changes: 27
New truth failures: 39
New crashes: 0
New script errors: 0
New comparator errors: 0
Fixed issues: 26
Total issues: 52
Test system warnings: 41
New deferred issues: 13
Fixed deferred issues: 0
Total deferred issues: 105
Run Time: 18 hours, 33 minutes, 10 seconds
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
BatchEstimator_ReportFile_Range [#488 failed]
BatchEstimator_ReportFile_StateInformation [#4 failed]
EphemPropagator_STK_CentralBody_Jupiter [vel err 2.80476e-06, tol 3e-08]
EphemPropagator_STK_CentralBody_Mars [vel err 3.49495e-06, tol 3e-08]
EphemPropagator_STK_CentralBody_Moon [vel err 1.10099e-05, tol 3e-09]
EphemPropagator_STK_CentralBody_Moon_Meters [vel err 1.10099e-05, tol
3e-09] [GMT-6093]
EphemPropagator_STK_CentralBody_Saturn [vel err 1.49341e-06, tol 3e-08]
EphemPropagator_STK_CentralBody_Sun [vel err 4.95649e-05, tol 3e-09]
EphemPropagator_STK_CentralBody_Venus [vel err 2.55247e-06, tol 3e-08]
EphemPropagator_STK_EphemCompare_LeapSecond [Output field 333.230000
failed tolerance in record 3602]
EphemPropagator_STK_EphemCompare_Moon [Output field 53.769000 failed
tolerance in record 432]
EphemPropagator_STK_EphemCompare_Sun [Output field 241.664000 failed
tolerance in record 416]
EphemPropagator_STK_StepSize_1min [vel err 3.23542e-07, tol 6e-09]
EphemPropagator_STK_StepSize_10min [vel err 2.14477e-07, tol 6e-09]
EphemPropagator_STK_StepSize_60min [vel err 6.28231e-08, tol 6e-09]
EphemPropagator_STK_TessEphemerisCheck [vel err 1.64485e-07, tol 6e-09]
ErrorModel_BiasSigma_DsnSeqRange_DsnTcp [#1 failed]
SpacecraftNavigation_OrbitErrorCovariance_DSN [#1 failed]
SpacecraftNavigation_OrbitErrorCovariance_DsnTcp [#1 failed]
SpacecraftNavigation_OrbitErrorCovariance_GN [#1 failed]
SpacecraftNavigation_OrbitErrorCovariance_Keplerian_DSN [#1 failed]
SpacecraftNavigation_OrbitErrorCovariance_Keplerian_DsnSeqRange [#1
failed]
SpacecraftNavigation_OrbitErrorCovariance_Keplerian_RangeRate [#1
failed]
SpacecraftNavigation_OrbitErrorCovariance_Range [#1 failed]
SpacecraftNavigation_OrbitErrorCovariance_Range_RangeRate [#1 failed]
SpacecraftNavigation_OrbitErrorCovariance_RangeRate [#1 failed]
SpacecraftNavigation_SolveFors_KeplerianState_DsnSeqRange_L2 [Parameter
EstSat.EarthMJ2000Eq.RAAN error 0.000123 exceeds tolerance 0.000100]
SpacecraftNavigation_Validation_EstimationStateType [#1 failed]
Write_Mode_Function []
Write_Spacecraft_LogFile_Concise []
Write_Spacecraft_LogFile_Script [#21 failed]
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 []
Output changes (but still pass):
BatchEstimator_OLSEUseRMSP_False_Range
DC_ReportFile_Debug
Ephem_GMAT_Code500_60sec
Ephem_GMAT_Code500_OutputFormat
Ephem_GMAT_Code500_OutputFormat
Ephem_GMAT_Code500_TimeInteractions
Ephem_GMAT_Code500_TimeInteractions
Ephem_GMAT_Code500_Toggle
EphemerisFile_Code500_EpochAdvance
EphemerisFile_Code500_LeapSecond_65d_60sec
EphemerisFile_Code500_LeapSecond_65d_600sec
EphemPropagator_STK_EphemCompare
EphemPropagator_STK_ForwardBackward
EphemPropagator_STK_ForwardProp
EphemPropagator_STK_ForwardProp_ElapsedSecs
EphemPropagator_STK_StartEpoch
EphemPropagator_STK_StartEpoch_Inherit
Ex_FirstVersionNumericSettings
GroundStation_Tropo_Marini_DsnSeqRange_Est
GroundStation_Tropo_Marini_DsnTcp_Est
GroundStation_Tropo_Marini_Range_Est
GroundStation_Tropo_Marini_RangeRate_Est
SNOPT_OverrideSpecsFile
Write_Multiple_ReportFile_Concise
Write_Multiple_ReportFile_Script
Write_Multiple_ReportFile_Script_2
Output changes (but still fail):
SpacecraftNavigation_SolveFors_KeplerianState_LeapSec_RangeRate [The
test
run failed to converge] [GMT-5954]
New crashes/hangs/etc.:
None
New script errors:
None
New comparator errors:
None
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
fmincon_Report
fmincon_ShowProgress
SpacecraftNavigation_SolveFors_CartesianState_EarthTODEq
Vary_optimizer_fmincon__AdditiveScaleFactor_Variable
Vary_optimizer_fmincon_Additive_and_Multiplicative_ScaleFactor_RealNumber
Vary_optimizer_fmincon_AdditiveScaleFactor_ArrayElement
Vary_optimizer_fmincon_AdditiveScaleFactor_RealNumber
Vary_optimizer_fmincon_MultiplicativeScaleFactor_ArrayElement
Vary_optimizer_fmincon_MultiplicativeScaleFactor_RealNumber
Vary_optimizer_fmincon_MultiplicativeScaleFactor_Variable
Fixed crashes/hangs/etc.:
Optimize_fmincon_cvg_status
Fixed script errors:
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable
Vary_optimizer_fmincon_Perturbation_ArrayElement
Vary_optimizer_fmincon_Perturbation_RealNumber
Vary_optimizer_fmincon_Perturbation_Variable
Vary_optimizer_fmincon_UpperBound_ArrayElement
Vary_optimizer_fmincon_UpperBound_Variable
Vary_optimizer_fmincon__InitialValue_Array
Vary_optimizer_fmincon__InitialValue_RealNumber
Vary_optimizer_fmincon__InitialValue_Variable
Vary_optimizer_fmincon__LowerBound_Array
Vary_optimizer_fmincon__LowerBound_RealNumber
Vary_optimizer_fmincon__LowerBound_Variable
completed_steps_1_thru_10_of_FRC_1_using_fmincon_Optimizer
fmincon_ConstraintTolerance
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
CallPythonFunction_Validation_InvalidOutputs_WrongSizeArray_4
Script errors:
ForceModel_GravityField_ZeroTide_Luna_TideModel_Solid:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\scriptTest\gmat\output\ForceModel_GravityField_ZeroTide_Luna_TideModel_Solid.txt
does not exist
Comparator errors:
EphemTest_DE405_Moon_Neptune: (truth)
ERROR MESSAGE: Comparator PVComparator failed: Error using fileread
(line 22)
Could not open file
C:\Users\gsfc580gmattest\Documents\scriptTest\input\Resources\FRR-16_SolarSystem\truth\RotationDataSource_Deprecation_Warning.txtEphemTest_DE405_Moon_Neptune.truth.
No such file or directory.
GMT-6055-GMATFunctionLargeArrayCrash: (reg)
ERROR MESSAGE: Undefined function
'comparator.FileDiffComparator.Compare' for input arguments of type
'char'.
Truth failures:
BatchEstimator_ReportFile_Range [#488 failed]
BatchEstimator_ReportFile_StateInformation [#4 failed]
EphemPropagator_STK_CentralBody_Jupiter [vel err 2.80476e-06, tol 3e-08]
EphemPropagator_STK_CentralBody_Mars [vel err 3.49495e-06, tol 3e-08]
EphemPropagator_STK_CentralBody_Moon [vel err 1.10099e-05, tol 3e-09]
EphemPropagator_STK_CentralBody_Moon_Meters [vel err 1.10099e-05, tol
3e-09] [GMT-6093]
EphemPropagator_STK_CentralBody_Saturn [vel err 1.49341e-06, tol 3e-08]
EphemPropagator_STK_CentralBody_Sun [vel err 4.95649e-05, tol 3e-09]
EphemPropagator_STK_CentralBody_Venus [vel err 2.55247e-06, tol 3e-08]
EphemPropagator_STK_EphemCompare_LeapSecond [Output field 333.230000
failed tolerance in record 3602]
EphemPropagator_STK_EphemCompare_Moon [Output field 53.769000 failed
tolerance in record 432]
EphemPropagator_STK_EphemCompare_Sun [Output field 241.664000 failed
tolerance in record 416]
EphemPropagator_STK_StepSize_1min [vel err 3.23542e-07, tol 6e-09]
EphemPropagator_STK_StepSize_10min [vel err 2.14477e-07, tol 6e-09]
EphemPropagator_STK_StepSize_60min [vel err 6.28231e-08, tol 6e-09]
EphemPropagator_STK_TessEphemerisCheck [vel err 1.64485e-07, tol 6e-09]
EphemStressTests_Default_Prop_CCSDS_Forward_and_BackwardDirect []
ErrorModel_BiasSigma_DsnSeqRange_DsnTcp [#1 failed]
Integrator_NoErrorControl_Warning [#1 failed]
OREx_Outbound_Cruise_Optimization_With_Global_Subscribers_And_Objects
[diff 0.000497931, tol 0.0004]
SpacecraftNavigation_OrbitErrorCovariance_DSN [#1 failed]
SpacecraftNavigation_OrbitErrorCovariance_DsnTcp [#1 failed]
SpacecraftNavigation_OrbitErrorCovariance_GN [#1 failed]
SpacecraftNavigation_OrbitErrorCovariance_Keplerian_DSN [#1 failed]
SpacecraftNavigation_OrbitErrorCovariance_Keplerian_DsnSeqRange [#1
failed]
SpacecraftNavigation_OrbitErrorCovariance_Keplerian_RangeRate [#1
failed]
SpacecraftNavigation_OrbitErrorCovariance_Range [#1 failed]
SpacecraftNavigation_OrbitErrorCovariance_Range_RangeRate [#1 failed]
SpacecraftNavigation_OrbitErrorCovariance_RangeRate [#1 failed]
SpacecraftNavigation_SolveFors_CartesianState_EarthFixed [The test run
failed to converge] [GMT-6408]
SpacecraftNavigation_SolveFors_KeplerianState_DsnSeqRange_L2 [Parameter
EstSat.EarthMJ2000Eq.RAAN error 0.000123 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_EarthFixed [The test run
failed to converge]
SpacecraftNavigation_SolveFors_KeplerianState_LeapSec_Range [Parameter
TDRS10.EarthTODEq.X error 2.248139 exceeds tolerance 0.010000] [GMT-5954]
SpacecraftNavigation_SolveFors_KeplerianState_LeapSec_RangeRate [The
test
run failed to converge] [GMT-5954]
SpacecraftNavigation_Validation_EstimationStateType [#1 failed]
TrackingFileSet_ChebyshevDEBoundary_1day [ Observable Error: 0.0002632
Hz]
TrackingFileSet_ChebyshevDEBoundary_1hour [ Observable Error: 0.8751 Hz]
Write_Mode_Function []
Write_Spacecraft_LogFile_Concise []
Write_Spacecraft_LogFile_Script [#21 failed]
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 []
-----------------------------------------------------------------
New Issues (Deferred)
-----------------------------------------------------------------
New truth failures (deferred):
None
Output changes (but still pass) (deferred):
ErrorModel_Bias_GpsPosVec2
StatisticsAcceptFilter_DataTypes_GpsPosVec
StatisticsRejectFilter_DataTypes_GpsPosVec
Write_Multiple_ReportFile_Verbose
Output changes (but still fail) (deferred):
Ephem_GMAT_Code500_ACE_OpsPrototype_v13 [pos err 2.31993, tol 1]
[GMT-4112]
Ephem_GMAT_Code500_InterpolationOrder [pos err 0.0463976, tol 0.002]
[GMT-4075, GMT-4112]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
[pos err 0.000200836, 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]
SpacecraftNavigation_SolveFors_CartesianState_LeapSec_Range [Parameter
TDRS10.EarthTODEq.X error 2.248239 exceeds tolerance 0.010000] [GMT-5954]
SpacecraftNavigation_SolveFors_CartesianState_LeapSec_RangeRate
[Parameter
Aura.EarthMJ2000Eq.X error 1.965657 exceeds tolerance 0.010000] [GMT-5954]
Write_Multiple_ReportFile_Concise_2 [#69 failed] [GMT-5801]
Write_Multiple_ReportFile_Verbose_2 [#69 failed] [GMT-5801]
New crashes/hangs/etc. (deferred):
None
New script errors (deferred):
None
New comparator errors (deferred):
None
-----------------------------------------------------------------
Fixed Issues (Deferred)
-----------------------------------------------------------------
Fixed truth failures (deferred):
None
Fixed crashes/hangs/etc. (deferred):
None
Fixed script errors (deferred):
None
Fixed comparator errors (deferred):
None
-----------------------------------------------------------------
All Known Issues (Deferred)
-----------------------------------------------------------------
Crashes/hangs/etc. (deferred):
GMAT_LunarTransfer_AllPlanets_DE421_BS
GMAT_MarsTransfer_4_BS
Script errors (deferred):
All_in_One_STEREO
All_in_One
BatchEstimator_EstimationEpoch [GMT-5708, GMT-5701]
Estimate_DeepSpace_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC_Ramp
Estimate_DeepSpace_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC
Estimate_LEO_4x4_USNTwoWayRange_LightTimeOnly_NonPerturbedIC
Estimate_LEO_4x4_USNTwoWayRange_LightTimeOnly_PerturbedIC
Estimate_LEO_PointMass_DSNTwoWayDoppler_LightTimeOnly_NonPerturbedIC
Estimate_LEO_PointMass_DSNTwoWayRangeDoppler_LightTimeOnly_NonPerturbedIC_Ramp
Estimate_LEO_PointMass_DSNTwoWayRangeDoppler_LightTimeOnly_NonPerturbedIC
Estimate_LEO_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC
Estimate_LEO_PointMass_USNTwoWayRange_LightTimeOnly_NonPerturbedIC
Estimate_LEO_PointMass_USNTwoWayRange_LightTimeOnly_PerturbedIC
Math_Shadowed_Builtins [GMT-3043]
Old_All_in_One_STEREO
Old_All_in_One
Old_Estimate_DeepSpace_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC_Ramp
Old_Estimate_DeepSpace_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC
Old_Estimate_LEO_PointMass_DSNTwoWayDoppler_LightTimeOnly_NonPerturbedIC
Old_Estimate_LEO_PointMass_DSNTwoWayRangeDoppler_LightTimeOnly_NonPerturbedIC_Ramp
Old_Estimate_LEO_PointMass_DSNTwoWayRangeDoppler_LightTimeOnly_NonPerturbedIC
Old_Estimate_LEO_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC
Old_Simulate_DeepSpace_DSNTwoWayDoppler_LightTimeOnly_RampTable
Old_Simulate_DeepSpace_DSNTwoWayRange_LT_GR_Transponder_RampTable
Old_Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_GR_RampTable
Old_Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable_2
Old_Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable
Old_Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly
Old_Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly_Ramp
Old_Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly_Zero_Ramp
Old_Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly
Old_Simulate_LEO_DSNTwoWayRange_LightTimeOnly_RampTable
Old_Simulate_LEO_DSNTwoWayRange_LightTimeOnly
Python_IO_String [5317]
ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522]
Simulate_DeepSpace_DSNTwoWayRange_LT_GR_Transponder_RampTable
Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_GR_RampTable
Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable_2
Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable
Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly_Ramp
Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly_Zero_Ramp
Simulate_LEO_DSNTwoWayRange_LightTimeOnly_RampTable
Simulate_LEO_USNTwoWayRange_LightTime-Bias
Simulate_LEO_USNTwoWayRange_LightTimeOnly
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_ACE_OpsPrototype_v13 [pos err 2.31993, tol 1]
[GMT-4112]
Ephem_GMAT_Code500_InterpolationOrder/Ephem_GMAT_Code500_InterpolationOrder_1.eph
[pos err 0.0173914, 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
305.165, tol 0.002] [GMT-4112]
EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection
[pos err 15.2466, 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 14.3796, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
[pos err 0.000200836, 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 0.00081496, tol
1e-06] [GMT-2567]
GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_BS [pos err
0.00234382, tol 0.0023]
GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Max_Reduction_BS
[pos err 0.00234382, tol 0.0023]
GMAT_LEO_PropSynchronization_BS []
GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS [pos err 0.0756285, tol 0.002]
Math_Inf [GMAT: 53 lines, Truth: 69 lines] [GMT-3195]
Minimize_Validation_Field [no warn or err] [GMT-3687]
Nonlinear_Validation_LHS_Field [no warn or err] [GMT-3687]
Nonlinear_Validation_RHS_Field [no warn or err] [GMT-3687]
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_MoonOccultation [GMAT: 11299 lines, Truth: 11306 lines]
[GMT-6134]
Simulator_Propagator_EarthPointMass_Drag/Simulator_Propagator_EarthPointMass_Drag_PosErr.report
[diff 0.0260902, tol 4e-05] [GMT-5417]
Simulator_Propagator_EarthPointMass_SRP_Drag/Simulator_Propagator_EarthPointMass_SRP_Drag_PosErr.report
[diff 0.0423286, tol 5e-05] [GMT-5417]
SpacecraftNavigation_SolveFors_CartesianState_LeapSec_Range [Parameter
TDRS10.EarthTODEq.X error 2.248239 exceeds tolerance 0.010000] [GMT-5954]
SpacecraftNavigation_SolveFors_CartesianState_LeapSec_RangeRate
[Parameter
Aura.EarthMJ2000Eq.X error 1.965657 exceeds tolerance 0.010000] [GMT-5954]
SpacecraftNavigation_Validation_Mode [#1 failed] [GMT-5841]
StatisticsRejectFilter_DataTypes_All [#1 failed]
StatisticsRejectFilter_DataTypes_DsnSeqRange [#2 failed]
StatisticsRejectFilter_DataTypes_DsnTcp [#1 failed]
StatisticsRejectFilter_ObservedObjects_All [#3 failed]
String_AssignNumericParam [] [GMT-2888]
THF_Sim_Accel_ConfigD_None_NA [ Observable Error: 0.3426 m.] [GMT-5986]
THF_Sim_Accel_ConfigD_None_NA_2 [ Observable Error: 739.3 m.] [GMT-5986]
THF_Sim_Accel_ConfigD_None_NA_3 [ Observable Error: 0.2607 m.]
[GMT-5986]
THF_Sim_Accel_ConfigD_None_NA_4 [ Observable Error: 0.04548 m.]
[GMT-5986]
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 [#69 failed] [GMT-5801]
Write_Multiple_ReportFile_Verbose_2 [#69 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_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]
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]
ScriptLanguage_Validation_DataTypes_ReferenceArray_Formation_5
[GMT-6064]
Simulator_Propagator_Sun_EM [GMT-6040]
Simulator_Propagator_Sun_EM_AllPlanets [GMT-6040]
Simulator_Propagator_Sun_EM_AllPlanets_SRP_GR [GMT-6040]
Simulator_Propagator_Sun_EM_GR [GMT-6040]
SpacePointParams_CelestialBody_EpochOutput [3939]
SpacecraftNavigation_L1_DsnSeqRange_SOHO_AncillaryElements [GMT-6040]
SpacecraftNavigation_L1_DsnSeqRange_SOHO_CovarianceCorrelationMatrix
[GMT-6040]
SpacecraftNavigation_L1_DsnSeqRange_SOHO_EstimatedState [GMT-6040]
THF_AccelMass_CSC_None_None [GMT-5981]
THF_Accel_CSC_None_None [GMT-5981]
THF_ThrustMass_CSC_None_None [GMT-5981]
THF_Thrust_CSC_None_None [GMT-5981]
THF_Thrust_CSC_None_None_2 [GMT-5981]
Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
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