The two new failures appear to be spurious. They are a result of a qualitatively new type of failure.
The log files for the two failed cases are truncated. The file must have been closed before the write was finished. The Timeout variable is set to 600 seconds by default. Any ideas? -----Original Message----- From: [email protected] <[email protected]> Sent: Wednesday, August 21, 2019 6:34 AM To: Cooley, D S. (GSFC-5950) <[email protected]>; [email protected] Subject: Test results: 2019-08-20 (GS580W-GMAT-T6/Win7-64/GMAT-64/M2016a/VS2017) ----------------------------------------------------------------- Summary ----------------------------------------------------------------- System configuration: Windows 10/MATLAB R2017a/VS 2013 Tested build: 2019-08-20 Regression build: 2019-08-16 Total number of scripts: 14390 (+82 deferred) Percent Passed: 99.90% New issues: 4 Output changes: 2 New truth failures: 2 New crashes: 0 New script errors: 0 New comparator errors: 0 Fixed issues: 2 Total issues: 15 Test system warnings: 36 New deferred issues: 8 Fixed deferred issues: 0 Total deferred issues: 57 Run Time: 15 hours, 28 minutes, 19 seconds ----------------------------------------------------------------- New Issues ----------------------------------------------------------------- New truth failures: CallPythonFunction_Validation_InvalidOutputs_WrongSizeArray_4 [no error or exception] Formation_MultiRegime_LEOFormation_Synchronization [] Output changes (but still pass): Ephem_GMAT_Code500_Toggle KalmanFilter_ScaledResidualThreshold_AzimuthElevation Output changes (but still fail): None New crashes/hangs/etc.: None New script errors: None New comparator errors: None ----------------------------------------------------------------- Fixed Issues ----------------------------------------------------------------- Fixed truth failures: Formation_MultiRegime_MultiSat_MultiProp2 Fixed crashes/hangs/etc.: None Fixed script errors: None Fixed comparator errors: ProcessNoiseModel_Validation_AccelNoiseSigma (truth) ----------------------------------------------------------------- All Known Issues ----------------------------------------------------------------- Crashes/hangs/etc.: None Script errors: None 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: CallPythonFunction_Validation_InvalidOutputs_WrongSizeArray_4 [no error or exception] 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] EKF_SpacecraftNavigation_GEO_Range_SDO [The test run failed to complete] [GMT-6775] EphemStressTests_Default_Prop_CCSDS_Forward_and_BackwardDirect [] [GMT-6840] ForceModel_Drag_SpaceWeatherFile_LineEndings [pos err 1.22211, tol 2e-06] [GMT-6673] Formation_MultiRegime_LEOFormation_Synchronization [] KalmanFilter_TimeUpdate_GpsPosVec [Found extra field Computed] [GMT-6958] Optimize_vf13ad_SolveMode_SaveAndContinue_GMT-4346 [] [GMT-6954] 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] ----------------------------------------------------------------- New Issues (Deferred) ----------------------------------------------------------------- New truth failures (deferred): None Output changes (but still pass) (deferred): Ephem_GMAT_Code500_StepSize [GMT-4112] 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_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] 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] ThrustSegment_SolveFors_ThrustScaleFactor_EpochDuringBurn [GMT-6940] Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455] _______________________________________________ Gmat-buildtest mailing list [email protected] https://lists.sourceforge.net/lists/listinfo/gmat-buildtest
