The most recent test system results (Red Hat). Run made with MATLAB R2019a.
- DJC -- Darrel J. Conway, Ph.D. Thinking Systems, Inc. Senior Scientist and CEO 437 W Thurber Road, Suite 6 Phone: (623) 298-4530 Tucson, AZ 85705 FAX: (520) 232-2533 www.thinksysinc.com Cell: (520) 425-3626 darrel.con...@thinksysinc.com
----------------------------------------------------------------- Summary ----------------------------------------------------------------- System configuration: RedHatEnterpriseWorkstation7.6 Tested build: RedHatEnterpriseWorkstation7.6-GMAT_Console Regression build: RedHatEnterpriseWorkstation7.6Baseline Total number of scripts: 14124 (+50 deferred) Percent Passed: 99.93% New issues: 2 Output changes: 0 New truth failures: 2 New crashes: 0 New script errors: 0 New comparator errors: 0 Fixed issues: 0 Total issues: 10 Test system warnings: 34 New deferred issues: 0 Fixed deferred issues: 0 Total deferred issues: 45 Run Time: 14 hours, 13 minutes, 57 seconds ----------------------------------------------------------------- New Issues ----------------------------------------------------------------- New truth failures: ErrorModel_Type_AzimuthElevation [#19 failed] SpacecraftNavigation_SolveFors_CartesianState_SPADDragScaleFactor_GN_MSISE86 [The test run failed to converge] Output changes (but still pass): None Output changes (but still fail): None New crashes/hangs/etc.: None New script errors: None 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: ForceModel_SPAD_Drag_1deg_Bicubic_Mars: ERROR MESSAGE: Output file ~/gsfcgmat/GmatDevelopment/GMAT-R2018a-Linux-x64/output/ForceModel_SPAD_Drag_1deg_Bicubic_Mars.report does not exist ForceModel_SPAD_Drag_1deg_Bilinear_Mars: ERROR MESSAGE: Output file ~/gsfcgmat/GmatDevelopment/GMAT-R2018a-Linux-x64/output/ForceModel_SPAD_Drag_1deg_Bilinear_Mars.report does not exist Comparator errors: None Truth failures: EKF_AcceptFilter_Level2_FileNames_GpsPosVec [#1 failed] [GMT-6762] EKF_RejectFilter_Level2_FileNames_GpsPosVec [#457 failed] [GMT-6762] EKF_TrackingFileSet_AddTrackingConfig_All [#15 failed] [GMT-6785] ErrorModel_Type_AzimuthElevation [#19 failed] ForceModel_Drag_SpaceWeatherFile_LineEndings [pos err 0.0154116, tol 2e-06] [GMT-6673] KalmanFilter_Validation_MatlabFile [#1 failed] [GMT-6784] SpacecraftNavigation_CdSigma_Range_MSISE86 [#1 failed] SpacecraftNavigation_SolveFors_CartesianState_SPADDragScaleFactor_GN_MSISE86 [The test run failed to converge] ----------------------------------------------------------------- New Issues (Deferred) ----------------------------------------------------------------- New truth failures (deferred): None Output changes (but still pass) (deferred): None Output changes (but still fail) (deferred): None 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): None Script errors (deferred): BatchEstimator_EstimationEpoch [GMT-5708] Math_Shadowed_Builtins [GMT-3043] Python_IO_String [5317] ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522] 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 0.0200021, 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 305.166, tol 0.002] [GMT-4112] EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection [pos err 15.2507, 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 14.3939, tol 1e-12] [GMT-4077] EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection [pos err 0.000219563, 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 0.000808928, tol 1e-06] [GMT-2567] Math_Inf [GMAT: 53 lines, Truth: 69 lines] [GMT-3195] Minimize_Validation_Field [ptrn 1 failed] [GMT-3687] Nonlinear_Validation_LHS_Field [ptrn 1 failed] [GMT-3687] Nonlinear_Validation_RHS_Field [ptrn 1 failed] [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] 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] 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] Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
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