Syeda, Below is log file message for the test Steve S mentions:
Please wait while MATLAB engine opens... Failed to open MATLAB engine ... Please wait while MATLAB engine opens... MATLAB engine successfully opened Interface Exception Thrown: "C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\bin\..\userfunctions\matlab\diff_gmd_files.m", Error using textscan Invalid file identifier. Use fopen to generate a valid file identifier. *** Mission run failed. ===> Total Run Time: 9.1 From: Slojkowski, Steven E. (GSFC-595.0)[OMITRON] <[email protected]> Sent: Monday, July 29, 2019 8:44 AM To: Cooley, D S. (GSFC-5950) <[email protected]>; [email protected] Cc: Kazmi, Syeda A. (GSFC-5830) <[email protected]> Subject: RE: Test results: 2019-07-26 (GS580W-GMAT-T6/Win7-64/GMAT-64/M2016a/VS2017) The GroundStation test is failing for MATLAB reasons. I checked in a update to hopefully fix the SpacecraftNavigation case. From: gmat-nav <[email protected]<mailto:[email protected]>> On Behalf Of Cooley, D S. (GSFC-5950) via gmat-nav Sent: Saturday, July 27, 2019 12:31 PM To: Cooley, D S. (GSFC-5950) <[email protected]<mailto:[email protected]>>; [email protected]<mailto:[email protected]>; '[email protected]' <[email protected]<mailto:[email protected]>> Cc: Kazmi, Syeda A. (GSFC-5830) <[email protected]<mailto:[email protected]>> Subject: Re: [gmat-nav] Test results: 2019-07-26 (GS580W-GMAT-T6/Win7-64/GMAT-64/M2016a/VS2017) Test results look pretty good. Most of the un-tagged failures appear to be false matlab related failures. For example, the log for test, Optimize_fmincon_cvg_status, shows: Please wait while MATLAB engine opens... Failed to open MATLAB engine ... Please wait while MATLAB engine opens... Failed to open MATLAB engine ... For tests needing matlab, I wonder if having the test script close all existing Matlab main window and command window processes first would help? Would allowing more attempts or more time to open Matlab engine help? Three Tests bolded in red below need attention. Thanks, Steve -----Original Message----- From: [email protected]<mailto:[email protected]> <[email protected]<mailto:[email protected]>> Sent: Saturday, July 27, 2019 4:02 AM To: Cooley, D S. (GSFC-5950) <[email protected]<mailto:[email protected]>>; [email protected]<mailto:[email protected]> Subject: Test results: 2019-07-26 (GS580W-GMAT-T6/Win7-64/GMAT-64/M2016a/VS2017) ----------------------------------------------------------------- Summary ----------------------------------------------------------------- System configuration: Windows 10/MATLAB R2017a/VS 2013 Tested build: 2019-07-26 Regression build: 2019-07-24 Total number of scripts: 14375 (+84 deferred) Percent Passed: 99.92% New issues: 9 Output changes: 4 New truth failures: 1 New crashes: 0 New script errors: 4 New comparator errors: 0 Fixed issues: 13 Total issues: 12 Test system warnings: 34 New deferred issues: 11 Fixed deferred issues: 0 Total deferred issues: 58 Run Time: 14 hours, 56 minutes, 51 seconds ----------------------------------------------------------------- New Issues ----------------------------------------------------------------- New truth failures: SpacecraftNavigation_SolveFors_KeplerianState_RangeSkin [Parameter EstSat.EarthMJ2000Eq.AOP error 0.001271 exceeds tolerance 0.001000] Output changes (but still pass): Ephem_GMAT_Code500_Toggle KalmanFilter_ScaledResidualThreshold KalmanFilter_ScaledResidualThreshold_DSN Simulator_LongTimeSpan Output changes (but still fail): None New crashes/hangs/etc.: None New script errors: GroundStation_Tropo_Marini_XSouthYEast_DeepSpace MatlabFunction_Custom_magic Optimize_fmincon_ExitMode_SaveAndContinue_2 Optimize_fmincon_cvg_status New comparator errors: None ----------------------------------------------------------------- Fixed Issues ----------------------------------------------------------------- Fixed truth failures: ErrorModel_SolveFors_Bias_RangeSkin3 GMATFunction_1stTarget_InFunction_2nd_In_Script_GlobalObjects_GlobalSC_As_Input_Output GMATFunction_Mars_B_Plane_Targeting_Global_Subscribers KalmanFilter_ReportFile_GpsPosVec Mars_B_Plane_Targeting_In_FunctionMode OREx_Outbound_Cruise_Optimization OREx_Outbound_Cruise_Optimization_In_FunctionMode OREx_Outbound_Cruise_Optimization_With_Global_Subscribers_And_Objects TrkFile_SimEst_DSN_DS Fixed crashes/hangs/etc.: None Fixed script errors: ErrorModel_Bias_Range GroundStation_Iono_XEastYNorth_DeepSpace Optimize_fmincon_SolveMode_Defaultscript Fixed comparator errors: EKF_ErrorModel_NoiseSigma_Range (truth) ----------------------------------------------------------------- All Known Issues ----------------------------------------------------------------- Crashes/hangs/etc.: None Script errors: GroundStation_Tropo_Marini_XSouthYEast_DeepSpace: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\GroundStation_Tropo_Marini_XSouthYEast_DeepSpace.diff does not exist MatlabFunction_Custom_magic: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\MatlabFunction_Custom_magic.report does not exist Optimize_fmincon_ExitMode_SaveAndContinue_2: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_ExitMode_SaveAndContinue_2.report does not exist Optimize_fmincon_cvg_status: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_cvg_status_Report2.report does not exist scriptEvent_optimizer_fmincon__InitialValue_RealNumber: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\scriptEvent_optimizer_fmincon__InitialValue_RealNumber.report does not exist Comparator errors: None Truth failures: EphemerisFile-STK-IncludeEventBoundariesFalse [ Too many blank lines.] EphemStressTests_Default_Prop_CCSDS_Forward_and_BackwardDirect [] [GMT-6840] ForceModel_Drag_SpaceWeatherFile_LineEndings [pos err 1.22211, tol 2e-06] [GMT-6673] Optimize_vf13ad_SolveMode_SaveAndContinue_GMT-4346 [] ProcessNoiseModel_Validation_CoordinateSystem [#1 failed] [GMT-6801] ProcessNoiseModel_Validation_Type [#1 failed] [GMT-6801] SpacecraftNavigation_SolveFors_KeplerianState_RangeSkin [Parameter EstSat.EarthMJ2000Eq.AOP error 0.001271 exceeds tolerance 0.001000] ----------------------------------------------------------------- New Issues (Deferred) ----------------------------------------------------------------- New truth failures (deferred): None Output changes (but still pass) (deferred): Ephem_GMAT_Code500_InterpolationOrder [GMT-4075, GMT-4112] Ephem_GMAT_Code500_InterpolationOrder [GMT-4075, GMT-4112] 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_InterpolationOrder [pos err 0.0463976, 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] THF_Sim_Accel_ConfigG_None_NA_FixedStep [ Observable Error: 0.413 m.] 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] 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] THF_Sim_Accel_ConfigD_None_NA_FixedStep [FixedStep 1 second, Sim, constant thrust over entire interval, should it pass] Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
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