-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Windows 10/MATLAB R2017a/VS 2013
Tested build: 2019-09-06
Regression build: 2019-09-03
Total number of scripts: 14397 (+82 deferred)
Percent Passed: 99.90%
New issues: 4
Output changes: 1
New truth failures: 1
New crashes: 0
New script errors: 2
New comparator errors: 0
Fixed issues: 1
Total issues: 16
Test system warnings: 35
New deferred issues: 6
Fixed deferred issues: 0
Total deferred issues: 57
Run Time: 15 hours, 28 minutes, 28 seconds
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
Formation_MultiRegime_LEOandGEOFormation_Synchronization2 []
Output changes (but still pass):
Ephem_GMAT_Code500_Toggle
Output changes (but still fail):
None
New crashes/hangs/etc.:
None
New script errors:
Optimize_fmincon_cvg_status
ThrustSegment_SolveFors_ThrustScaleFactor_EpochDuringBurn [GMT-6940]
New comparator errors:
None
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
KalmanFilter_TimeUpdate_GpsPosVec
Fixed crashes/hangs/etc.:
None
Fixed script errors:
None
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
None
Script errors:
Optimize_fmincon_cvg_status:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_cvg_status_Report2.report
does not exist
ThrustSegment_SolveFors_ThrustScaleFactor_EpochDuringBurn: [GMT-6940]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\ThrustSegment_SolveFors_ThrustScaleFactor_EpochDuringBurn.txt
does not exist
Comparator errors:
FMParams_GMAT_UserAsteroid(OSIRIS)_HarmonicGravity_SRP_PointMasses:
(truth) [GMT-6955]
ERROR MESSAGE: Comparator PercentDiffComparator failed: Error using
textscan
First input can not be empty. Expected a non-empty character vector or a
valid file-id.
FMParams_GMAT_UserAsteroid(OSIRIS)_HarmonicGravity_SRP_PointMasses:
(reg)
[GMT-6955]
ERROR MESSAGE: Subscript indices must either be real positive integers
or logicals.
Truth failures:
EKF_EphemerisFile_STK_L1 [Test NumberOfEphemerisPoints ~= truth
NumberOfEphemerisPoints] [GMT-6937]
EKF_ErrorModel_Bias_DSN_Est [Residual failed at 10 Jun 2012
01:12:00.000]
[GMT-6941]
EphemStressTests_Default_Prop_CCSDS_Forward_and_BackwardDirect []
[GMT-6840]
ForceModel_Drag_SpaceWeatherFile_LineEndings [pos err 1.22211, tol
2e-06]
[GMT-6673]
Formation_MultiRegime_LEOandGEOFormation_Synchronization2 []
Optimize_vf13ad_SolveMode_SaveAndContinue_GMT-4346 [] [GMT-6954]
ProcessNoiseModel_AccelNoiseSigma_GN [Sigma-V failed at 10 Jun 2010
22:15:00.000] [GMT-6958]
ProcessNoiseModel_CoordinateSystem_MoonMJ2000Eq [The test run failed to
complete] [GMT-6942]
ProcessNoiseModel_CoordinateSystem_SunMJ2000Eq [The test run failed to
complete] [GMT-6942]
ProcessNoiseModel_Validation_CoordinateSystem [#1 failed] [GMT-6801]
ProcessNoiseModel_Validation_Type [#1 failed] [GMT-6801]
Smoother_Validation_Filter [#1 failed] [GMT-6986]
-----------------------------------------------------------------
New Issues (Deferred)
-----------------------------------------------------------------
New truth failures (deferred):
None
Output changes (but still pass) (deferred):
None
Output changes (but still fail) (deferred):
Ephem_GMAT_Code500_InterpolationOrder [pos err 0.0173914, tol 0.002]
[GMT-4075, GMT-4112]
Ephem_GMAT_Code500_StepSize [pos err 305.165, tol 0.002] [GMT-4112]
EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection
[pos err 15.2508, 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 14.3834, tol 1e-12] [GMT-4077]
EphemStressTests_PD78_ABM_Prop_Code500_60Sec_Step_ForwardDirection [pos
err 21.5632, tol 1e-12] [GMT-4112]
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):
BatchEstimator_EstimationEpoch [GMT-5708]
Math_Shadowed_Builtins [GMT-3043]
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_ReportFile_InitialState [#5 failed] [GMT-6412]
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 15.2508, 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 14.3834, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
[pos err 0.000217107, 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_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]
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_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]
SpacecraftNavigation_Validation_Mode [#1 failed] [GMT-5841]
String_AssignNumericParam [] [GMT-2888]
TrkFile_SimEst_TDRS_range_Solve_Cr [] [GMT-5416]
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_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]
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]
Math_Validation_Cross_WrongDim2 [GMT-5676]
ScriptLanguage_Validation_DataTypes_ReferenceArray_Formation_5
[GMT-6064]
Simulator_Propagator_EarthPointMass_Drag [GMT-5417]
Simulator_Propagator_EarthPointMass_SRP_Drag [GMT-5417]
SpacePointParams_CelestialBody_EpochOutput [3939]
SpacecraftNavigation_CdSigma_Range_MSISE86 [GMT-6829 Linux 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]
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