----------------------------------------------------------------- Summary ----------------------------------------------------------------- System configuration: Windows 10/MATLAB R2017a/VS 2013 Tested build: 2019-08-29 Regression build: 2019-08-28
Total number of scripts: 14393 (+82 deferred) Percent Passed: 99.90% New issues: 3 Output changes: 2 New truth failures: 0 New crashes: 0 New script errors: 1 New comparator errors: 0 Fixed issues: 0 Total issues: 15 Test system warnings: 37 New deferred issues: 7 Fixed deferred issues: 0 Total deferred issues: 57 Run Time: 15 hours, 30 minutes, 41 seconds ----------------------------------------------------------------- New Issues ----------------------------------------------------------------- New truth failures: None Output changes (but still pass): Ephem_GMAT_Code500_60sec Ephem_GMAT_Code500_Toggle Output changes (but still fail): None New crashes/hangs/etc.: None New script errors: ThrustSegment_SolveFors_ThrustScaleFactor_EpochDuringBurn [GMT-6940] New comparator errors: None ----------------------------------------------------------------- Fixed Issues ----------------------------------------------------------------- Fixed truth failures: None Fixed crashes/hangs/etc.: None Fixed script errors: None Fixed comparator errors: None ----------------------------------------------------------------- All Known Issues ----------------------------------------------------------------- Crashes/hangs/etc.: None Script errors: 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] EKF_SpacecraftNavigation_GEO_Range_SDO [Parameter SDO.EarthMJ2000Eq.X error 513.703532 exceeds tolerance 0.010000] [GMT-6775] EphemStressTests_Default_Prop_CCSDS_Forward_and_BackwardDirect [] [GMT-6840] ForceModel_Drag_SpaceWeatherFile_LineEndings [pos err 1.22211, tol 2e-06] [GMT-6673] KalmanFilter_MeasurementUpdate_GpsPosVec [Test variable Filter.Covariance size does not match truth size] 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): 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_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] ProcessNoiseModel_AccelNoiseSigma_GpsPosVec [GMT-6959] ProcessNoiseModel_AccelNoiseSigma_Zero_GpsPosVec [GMT-6959] 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] _______________________________________________ Gmat-buildtest mailing list Gmat-buildtest@lists.sourceforge.net https://lists.sourceforge.net/lists/listinfo/gmat-buildtest