----------------------------------------------------------------- Summary ----------------------------------------------------------------- System configuration: Windows 10/MATLAB R2017a/VS 2013 Tested build: 2020-08-06 Regression build: 2020-08-05
Total number of scripts: 15207 (+94 deferred) Percent Passed: 99.64% New issues: 145 Output changes: 137 New truth failures: 3 New crashes: 0 New script errors: 5 New comparator errors: 0 Fixed issues: 4 Total issues: 56 Test system warnings: 52 New deferred issues: 9 Fixed deferred issues: 1 Total deferred issues: 66 Run Time: 19 hours, 16 minutes, 26 seconds ----------------------------------------------------------------- New Issues ----------------------------------------------------------------- New truth failures: Matlab_NoInputsOutputs [] Optimize_fmincon_CostFunction_and_ConvergedStatus_Display_2 [ptrn 1,2,3 failed] Optimize_fmincon_Max_Iterations_Display [ptrn 1,2 failed] Output changes (but still pass): CelestialBodyRendezvous_Mars CelestialBodyRendezvous_Venus CustomLinkageConstraint_AbsoluteMode_FinalPhase CustomLinkageConstraint_AbsoluteMode_GregorianEpochFormat CustomLinkageConstraint_DifferenceMode_Mass CustomLinkageConstraint_DifferenceMode_Position CustomLinkageConstraint_DifferenceMode_Time CustomLinkageConstraint_DifferenceMode_Velocity CustomLinkageConstraint_SeparatedLinkages_TwoPhases_NoRefinement_Local_WithMass CustomLinkageConstraint_TwoPhases_ConstraintMode_FinalPhase CustomLinkageConstraint_TwoPhases_ConstraintMode_InitialPhase CustomLinkageConstraint_TwoPhases_NoRefinement_Local_WithMass DynamicsConfiguration_ChemicalTankMass DynamicsConfiguration_ElectricTankMass DynamicsConfiguration_MultipleFuelTanks DynamicsConfiguration_TwoElementsInFiniteBurnsList DynamicsConfiguration_TwoElementsInForceModelsList DynamicsConfiguration_TwoElementsInList DynamicsConfiguration_TwoElementsInSpacecraftList DynamicsConfiguration_TwoPhasesWithUniqueDynConfigs DynamicsConfiguration_Typical EMTGSpacecraft_SCOpt_BusPowerType0 EMTGSpacecraft_SCOpt_BusPowerType1 EMTGSpacecraft_SCOpt_PowerSupplyCurve1 EMTGSpacecraft_SCOpt_ThrottleTable_Empty_Prop_Mode_ConstThrustIsp EMTGSpacecraft_SCOpt_ThrottleTable_File_Prop_Mode_ConstThrustIsp EMTGSpacecraft_SCOpt_ThrottleTable_None_Prop_Mode_ConstThrustIsp EMTGSpacecraft_SCOpt_ThrottleTable_None_Prop_Mode_Poly1D EMTGSpacecraft_SCOpt_ThrottleTableEmpty EMTGSpacecraft_SCOpt_ThrustType0 EMTGSpacecraft_SCOpt_ThrustType1 EMTGSpacecraft_SCOpt_ThrustType3 EMTGSpacecraft_SCOpt_ThrustType4 EMTGSpacecraft_SCOpt_ThrustType5 EMTGSpacecraft_StageListTooLong EMTGSpacecraft_StageListTooShort IntegratedFlyby_MarsFlyby [GMT-7169] IntegratedFlyby_VenusFlyby OCPropTest_DeepSpace_Relativity OCPropTest_DEEPSPACE_Relativity_Cmd OCPropTest_ESL2_SRP OCPropTest_GEO_4x4 OCPropTest_GEO_20x20 OCPropTest_GEO_20x20_SRP OCPropTest_GEO_20x20_SRP_MSISE00 OCPropTest_GEOPointMass OCPropTest_Jupiter_AllPlanets_SRP OCPropTest_Jupiter_Relativity OCPropTest_LEOJGM2_4x4 OCPropTest_LEOJGM2_4x4_JR OCPropTest_LEOJGM2_4x4_JR_SRP OCPropTest_LEOJGM2_4x4_SRP OCPropTest_LEOJGM2_20x20 OCPropTest_LEOPointMass OCPropTest_LUNA OCPropTest_LUNA_AllPlanets OCPropTest_LUNA_CentralBody_Cmd OCPropTest_LUNA_LP165 OCPropTest_LUNA_LP165P_SRP OCPropTest_LUNA_Relativity OCPropTest_LUNA_SRP OCPropTest_MARS OCPropTest_MARS_AllPlanets OCPropTest_MARS_Mars50c_MarsGRAM2005 OCPropTest_MARS_MarsGRAM2005 OCPropTest_MARS_SRP OCPropTest_MARS_SRP_Cmd OCPropTest_Mercury OCPropTest_Mercury_AllPlanets OCPropTest_Mercury_SRP OCPropTest_Mercury_SRP_Flux_Cmd OCPropTest_Neptune OCPropTest_Neptune_AllPlanets OCPropTest_Neptune_SRP OCPropTest_Pluto OCPropTest_Pluto_AllPlanets OCPropTest_Pluto_SRP OCPropTest_Saturn OCPropTest_Saturn_AllPlanets OCPropTest_Saturn_SRP OCPropTest_SPAD_SRP_1deg_Bilinear_Moon OCPropTest_Uranus OCPropTest_Uranus_AllPlanets OCPropTest_Uranus_SRP OCPropTest_Venus OCPropTest_Venus_AllPlanets OCPropTest_Venus_MGNP180U OCPropTest_Venus_MGNP180U_SRP OCPropTest_Venus_SRP OptimalControlGuess_System_Type_CollocationGuessFile OptimalControlGuess_System_Type_CollocationGuessFile_EarthCentralBody OptimalControlGuess_System_Type_CollocationGuessFile_MJ2000RefFrame OptimalControlGuess_System_Type_GMATArray OptimalControlGuess_System_Type_GMATArray_DefaultTimeSystem OptimalControlGuess_System_Type_GMATArray_EarthCenteredGuess OptimalControlGuess_System_Type_GMATArray_TDBGuess PCLaunch_ConstrainedC3AndDLA_EarthLaunch_EarthOrigin PCLaunch_ConstrainedC3AndDLA_EarthLaunch_SunOrigin PCLaunch_ConstrainedC3AndDLA_Venus Phase_Bound_EpochLowerBound Phase_Bound_Epochs Phase_Bound_EpochUpperBound Phase_Bounds_ControlMagLower Phase_Bounds_ControlMagUpper Phase_Bounds_ControlVector Phase_Bounds_StateLowerBound Phase_Bounds_StateUpperBound Phase_BuiltInCost_MaxTotalMass Phase_BuiltInCost_MinAbsoluteFinalTime Phase_Epoch_EpochGuesses Phase_EpochFormat_TAIGregorian [GMT-7168] Phase_MaxRelativeErrorTolerance_IRK_Loose Phase_MaxRelativeErrorTolerance_IRK_Tight Phase_MaxRelativeErrorTolerance_Radau_Loose Phase_MaxRelativeErrorTolerance_Radau_Tight Phase_PointsPerSubPhase_ImplicitRKOrder6 Phase_PointsPerSubPhase_IRK Phase_PointsPerSubPhase_Radau Phase_Type_HermiteSimpson Phase_Type_ImplicitRKOrder4 Phase_Type_ImplicitRKOrder6 Phase_Type_ImplicitRKOrder8 Phase_Type_Radau [GMT-7168] RHS_System_RHS_In_CommandMode RHS_System_RHS_In_ObjectMode RHS_System_StandAloneNumber Trajectory_System_GuessSource Trajectory_System_GuessSource_PhaseNoTraj Trajectory_System_GuessSource_TrajNoPhase Trajectory_System_MassScaleFactor Trajectory_System_MeshGuessMode_Curr Trajectory_System_OptimizationMode Trajectory_System_OutputCoordSys Trajectory_System_SolnFname_Undeclared Trajectory_System_StateScaleMode Trajectory_System_TotalIterationsLimits_Long Trajectory_System_TotItLim Output changes (but still fail): None New crashes/hangs/etc.: None New script errors: Matlab_IO_Array Matlab_VariableInputs Optimize_fmincon_ExitMode_SaveAndContinue_2 Optimize_fmincon_Minimize_Height_on_circle_2 Trajectory_System_MeshGuessMode_Best New comparator errors: None ----------------------------------------------------------------- Fixed Issues ----------------------------------------------------------------- Fixed truth failures: Formation_MultiRegime_MultiSat_MultiProp2 TrkFile_Est_DSN_DS_Range Fixed crashes/hangs/etc.: None Fixed script errors: Optimize_fmincon_ExitMode_DiscardAndContinue Optimize_fmincon_ExitMode_SaveAndContinue_3 Fixed comparator errors: None ----------------------------------------------------------------- All Known Issues ----------------------------------------------------------------- Crashes/hangs/etc.: None Script errors: Matlab_IO_Array: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Matlab_IO_Array.report does not exist Matlab_IO_String: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Matlab_IO_String.report does not exist Matlab_VariableInputs: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Matlab_VariableInputs.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_Minimize_Height_on_circle_2: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_Minimize_Height_on_circle_2.report does not exist Trajectory_System_MeshGuessMode_Best: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Trajectory_System_MeshGuessMode_Best.och does not exist Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2.report does not exist Vary_optimizer_fmincon_InitialGuess_ForLoopVariable: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_InitialGuess_ForLoopVariable.report does not exist Vary_optimizer_fmincon_Perturbation_ArrayElement: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_Perturbation_ArrayElement.report does not exist Vary_optimizer_fmincon_Perturbation_RealNumber: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_Perturbation_RealNumber.report does not exist Vary_optimizer_fmincon_Perturbation_Variable: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_Perturbation_Variable.report does not exist Vary_optimizer_fmincon_UpperBound_ArrayElement: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_UpperBound_ArrayElement.report does not exist Vary_optimizer_fmincon_UpperBound_Variable: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_UpperBound_Variable.report does not exist Vary_optimizer_fmincon__InitialValue_Array: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__InitialValue_Array.report does not exist Vary_optimizer_fmincon__InitialValue_RealNumber: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__InitialValue_RealNumber.report does not exist Vary_optimizer_fmincon__InitialValue_Variable: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__InitialValue_Variable.report does not exist Vary_optimizer_fmincon__LowerBound_Array: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__LowerBound_Array.report does not exist Vary_optimizer_fmincon__LowerBound_RealNumber: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__LowerBound_RealNumber.report does not exist Vary_optimizer_fmincon__LowerBound_Variable: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__LowerBound_Variable.report does not exist completed_steps_1_thru_10_of_FRC_1_using_fmincon_Optimizer: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\completed_steps_1_thru_10_of_FRC_1_using_fmincon_Optimizer.report does not exist fmincon_ConstraintTolerance: ERROR MESSAGE: Output file C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\fmincon_ConstraintTolerance.report does not exist Comparator errors: None Truth failures: API_PD45PropagationE8x8SMPM (API) [pos err 0.000753381, tol 1e-07] BatchEstimator_NormalMatrixReduction_UseInitialCovariance [#1 failed] [GMT-7274] fmincon_Report [#3 failed] fmincon_ShowProgress [#1 failed] GroundStation_Iono_Range_DeepSpace [Found 13688 output records and 13695 truth records] [GMD-7061] KalmanFilter_InputWarmStartFile_DSN_Sun_SPADSRP [Output field -133536564.419617 failed tolerance in record 1] [GMT-7282, GMT-7278] KalmanFilter_InputWarmStartFile_GpsPosVec_ThrustScaleFactor [Output field -947.631290 failed tolerance in record 1] [GMT-7292] KalmanFilter_Smoother_PredictTimeSpan_Both_OEM/KalmanFilter_Smoother_PredictTimeSpan_Both_OEM_filter.oem [#1 failed] [GMT-6949] Matlab_NoInputsOutputs [] Optimize_fmincon_CostFunction_and_ConvergedStatus_Display_2 [ptrn 1,2,3 failed] Optimize_fmincon_cvg_status/Optimize_fmincon_cvg_status_Report1.report [] Optimize_fmincon_cvg_status/Optimize_fmincon_cvg_status_Report2.report [#2 failed] Optimize_fmincon_Max_Iterations_Display [ptrn 1,2 failed] Plate_Validation_PlateNormalHistoryFile [#1 failed] [GMT-7022] ProcessNoiseModel_AccelNoiseSigma_GN [Sigma-V failed at 10 Jun 2010 22:15:00.000] [GMT-6958] ProcessNoiseModel_AccelNoiseSigma_GpsPosVec [Variable Filter.Covariance error 6.3756e-06 failed tolerance 1e-06 at linear index 13940] [GMT-6958] ProcessNoiseModel_AccelNoiseSigma_Zero_GpsPosVec [Variable Filter.Covariance error 3.78248e-06 failed tolerance 1e-06 at linear index 16064] [GMT-6958] RotationMatrixTest_MercuryMJ2000Ec [max diff 1.09735e-09 > tol 1e-12] [GMT-7223] Spacecraft_Validation_AddPlates [#1 failed] [GMT-7022] TrackingFileSet_AddTrackingConfig_DsnSeqRange [#1 failed] [GMR-7061] TrackingFileSet_AddTrackingConfig_DsnTcp [#1 failed] [GMR-7061] TrackingFileSet_AddTrackingConfig_Range [#1 failed] [GMR-7061] TrackingFileSet_AddTrackingConfig_RangeRate [#1 failed] [GMR-7061] TrackingFileSet_FileName2 [#2 failed] [GMR-7061] Transponder_HardwareDelay_Sim_Range [GMAT: 617 lines, Truth: 619 lines] [GMR-7061] Transponder_HardwareDelay_Sim_Range_RangeSkin [GMAT: 65 lines, Truth: 66 lines] [GMR-7061] Transponder_HardwareDelay_Sim_RangeSkin [GMAT: 65 lines, Truth: 66 lines] [GMR-7061] Tut_MultipleShootingTutorial_Step3 [] [GMT-7280] Vary_optimizer_fmincon__AdditiveScaleFactor_Variable [ptrn 1,2 failed] Vary_optimizer_fmincon_Additive_and_Multiplicative_ScaleFactor_RealNumber [ptrn 1,2 failed] Vary_optimizer_fmincon_AdditiveScaleFactor_ArrayElement [ptrn 1,2 failed] Vary_optimizer_fmincon_AdditiveScaleFactor_RealNumber [ptrn 1,2 failed] Vary_optimizer_fmincon_MultiplicativeScaleFactor_ArrayElement [ptrn 1,2 failed] Vary_optimizer_fmincon_MultiplicativeScaleFactor_RealNumber [ptrn 1,2 failed] Vary_optimizer_fmincon_MultiplicativeScaleFactor_Variable [ptrn 1,2 failed] ----------------------------------------------------------------- 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_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): TrkFile_SimEst_TDRS_range_Solve_Cr [GMT-5416] 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] EKF_SpacecraftNavigation_OrbitErrorCovariance_Keplerian_GpsPosVec EKF_SpacecraftNavigation_SolveFors_KeplerianState_Cd_RandomConstant_GN EKF_SpacecraftNavigation_SolveFors_KeplerianState_Cr_RandomConstant_DSN EKF_SpacecraftNavigation_SolveFors_KeplerianState_GN EKF_SpacecraftNavigation_SolveFors_KeplerianState_GpsPosVec KalmanFilter_InputWarmStartFile_GN_Moon_Keplerian [GMT-6801] KalmanFilter_InputWarmStartFile_GpsPosVec_KeplerianToCartesian [GMT-6801] KalmanFilter_OutputWarmStartFile_GpsPosVec_Keplerian [GMT-6801] Math_Shadowed_Builtins [GMT-3043] OCPropTest_SPAD_Drag_1deg_Bicubic_LEO [GMT-7147] OCPropTest_SPAD_Drag_SRP_1deg_Bicubic_LEO [GMT-7147] 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] EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond_Filter.e [EphemerisTimePosVel failed epoch tolerance at row 988] [GMT-7291] EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond_Smoother.e [EphemerisTimePosVel failed epoch tolerance at row 988] [GMT-7291] 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_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] 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] EKFS_ThrustSegment_SolveFors_ThrustScaleFactor [GMT-6949] 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_CCSDS_Forward_and_BackwardDirect [GMT-6840] 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] FMParams_GMAT_UserAsteroid(OSIRIS)_HarmonicGravity_SRP_PointMasses [GMT-6955] 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] IntegratedFlyby_MarsFlyby [GMT-7169] KalmanFilter_TimeUpdate_GpsPosVec [GMT-6801] Math_Validation_Cross_WrongDim2 [GMT-5676] Phase_EpochFormat_TAIGregorian [GMT-7168] Phase_Type_Radau [GMT-7168] Plate_Type_File [GMT-7022] Plate_Type_File_CoordinateSystem_Body [GMT-7022] Plate_Type_File_CoordinateSystem_EarthMJ2000Ec [GMT-7022] Plate_Type_File_CoordinateSystem_FixedInBody [GMT-7022] Plate_Type_File_StartEpoch [GMT-7022] ScriptLanguage_LineContinuation_BeginningOfLine [GMT-3756] ScriptLanguage_Validation_DataTypes_ReferenceArray_Formation_5 [GMT-6064] Simulator_Propagator_EarthPointMass_Drag [GMT-5417] Simulator_Propagator_EarthPointMass_SRP_Drag [GMT-5417] Smoother_Filter_FogmCd_GpsPosVec [GMT-7278] SpacePointParams_CelestialBody_EpochOutput [3939] SpacecraftNavigation_CdSigma_Range_MSISE86 [GMT-6829 Linux only] SpacecraftNavigation_SPADDragScaleFactorSigma_ConstrainInc [GMT-7078, Ubuntu only] SpacecraftNavigation_SPADDragScaleFactorSigma_GN_MSISE86 [GMT-6829 Linux only] SpacecraftNavigation_SPADSRPScaleFactorSigma_ConstrainInc [GMT-7078, Linux only] SpacecraftNavigation_SolveFors_CartesianState_SPADDragScaleFactor_GN_MSISE86 [GMT-6829 Linux only] Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455] TrkFile_SimEst_TDRS_range_Solve_Cr [GMT-5416] _______________________________________________ Gmat-buildtest mailing list Gmat-buildtest@lists.sourceforge.net https://lists.sourceforge.net/lists/listinfo/gmat-buildtest