(Resending with the correct date in the subject line!)
Test system results from the build of R2017a with TESS updates for the STK propagator.
Note: These 2: EphemPropagator_STK_VelocityDiscontinuity [pos err 4.03717, tol 1e-06] EphemPropagator_STK_VelocityDiscontinuity [pos err 4.03717, tol 1e-06] test cases now show the much improved results:EphemPropagator_STK_VelocityDiscontinuity [pos err 0.00639492, tol 1e-06] EphemPropagator_STK_VelocityDiscontinuity [pos err 0.00639492, tol 1e-06]
- DJC -- Darrel J. Conway, Ph.D. Thinking Systems, Inc. Senior Scientist and CEO 6441 N Camino Libby Phone: (623) 298-4530 Tucson, AZ 85718 FAX: (520) 232-2533 www.thinksysinc.com Cell: (520) 425-3626 d...@thinksysinc.com
----------------------------------------------------------------- Summary ----------------------------------------------------------------- System configuration: RHEL_7.2 Tested build: RHEL_GMAT_Console Regression build: RHELBaseline Total number of scripts: 13848 (+133 deferred) Percent Passed: 99.94% New issues: 6 Output changes: 0 New truth failures: 6 New crashes: 0 New script errors: 0 New comparator errors: 0 Fixed issues: 13 Total issues: 9 Test system warnings: 55 New deferred issues: 17 Fixed deferred issues: 2 Total deferred issues: 86 Run Time: 06 hours, 52 minutes, 13 seconds ----------------------------------------------------------------- New Issues ----------------------------------------------------------------- New truth failures: EphemPropagator_PropStressTest_DifferentPropsDifferentOrigin [pos err 0.000130949, tol 0.0001] EphemPropagator_PropStressTest_DifferentPropsSameOrigin [pos err 0.000130949, tol 0.0001] EphemPropagator_PropStressTest_EpochFromProp [pos err 0.000130949, tol 0.0001] EphemPropagator_PropStressTest_EpochFromSat [pos err 0.000130949, tol 0.0001] EphemPropagator_STK_EphemCompare_LeapSecond [Output field 333.230000 failed tolerance in record 3602] SpacecraftNavigation_SolveFors_CartesianState_Cd_Cr_RangeRate [The test run failed to converge] [GMT-5417] 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: BatchEstimator_ReportFile_CovarianceCorrelationMatrix BatchEstimator_ReportFile_StateInformation SpacecraftNavigation_SolveFors_CartesianState_Cd_Cr_GN [GMT-5417] TrackingFileSet_UseAllCorrections_DsnTcp_Est TrackingFileSet_UseAllCorrections_DsnTcp_Sim TrackingFileSet_UseETminusTAI_Range_Est TrackingFileSet_UseETminusTAI_RangeRate_Est TrackingFileSet_UseLightTime_DsnSeqRange_Est TrackingFileSet_UseLightTime_DsnTcp_Est TrackingFileSet_UseLightTime_Range_Est TrackingFileSet_UseLightTime_Range_RangeRate_Est TrackingFileSet_UseLightTime_RangeRate_Est TrackingFileSet_UseRelativityCorrection_DsnSeqRange_Est Fixed crashes/hangs/etc.: None Fixed script errors: None Fixed comparator errors: None ----------------------------------------------------------------- All Known Issues ----------------------------------------------------------------- Crashes/hangs/etc.: None Script errors: None Comparator errors: None Truth failures: EphemPropagator_PropStressTest_DifferentPropsDifferentOrigin [pos err 0.000130949, tol 0.0001] EphemPropagator_PropStressTest_DifferentPropsSameOrigin [pos err 0.000130949, tol 0.0001] EphemPropagator_PropStressTest_EpochFromProp [pos err 0.000130949, tol 0.0001] EphemPropagator_PropStressTest_EpochFromSat [pos err 0.000130949, tol 0.0001] EphemPropagator_STK_EphemCompare_LeapSecond [Output field 333.230000 failed tolerance in record 3602] EphemPropagator_STK_VelocityDiscontinuity [pos err 0.00639492, tol 1e-06] EphemPropagator_STK_VelocityDiscontinuity [pos err 0.00639492, tol 1e-06] Integrator_LEO_PD853_Accuracy [] SpacecraftNavigation_SolveFors_CartesianState_Cd_Cr_RangeRate [The test run failed to converge] [GMT-5417] ----------------------------------------------------------------- New Issues (Deferred) ----------------------------------------------------------------- New truth failures (deferred): GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_BS [pos err 0.00236009, tol 0.0023] GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Max_Reduction_BS [pos err 0.00236009, tol 0.0023] GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Minimum_Reduction_BS [pos err 0.00236009, tol 0.0023] THF_Accel_CSA_None_NA [] [GMT-5701] THF_Accel_ECI_None_NA_3minutes_UnitZ [] [GMT-5701] THF_Accel_ECI_None_NA_3minutes_UnitZ_TSF [] [GMT-5701] THF_Accel_ECI_None_NA_3minutes_UnitZ_TSF_2 [] [GMT-5701] THF_Accel_ECI_None_NA_3minutes_UnitZ_TSF_3 [] [GMT-5701] THF_AccelMass_CSA_None_None [] [GMT-5701] THF_AccelMass_ECI_None_None_3minutes_UnitZ [] [GMT-5701] THF_AccelMass_ECI_None_None_3minutes_UnitZ_TSF [] [GMT-5701] THF_AccelMass_ECI_None_None_3minutes_UnitZ_TSF_2 [] [GMT-5701] THF_AccelMass_ECI_None_None_3minutes_UnitZ_TSF_3 [] [GMT-5701] THF_ThrustMass_CSA_None_None [] [GMT-5701] THF_ThrustMass_ECI_None_None_3minutes_UnitZ [] [GMT-5701] THF_ThrustMass_ECI_None_None_3minutes_UnitZ_TSF_2 [] [GMT-5701] THF_ThrustMass_ECI_None_None_3minutes_UnitZ_TSF_3 [] [GMT-5701] 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): GMAT_LunarTran_PropSynchronization_BS THF_Sim_Accel_ConfigD_None_NA [GMT-5986] 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, GMT-5701] Math_Shadowed_Builtins [GMT-3043] OLDBatchEstimator_EstimationEpoch [GMT-5708, GMT-5701] OLDTransmitter_Frequency_DSN_Doppler_DeepSpace_2 [GMT-5701] OLDTransmitter_Frequency_DSN_Doppler_DeepSpace [GMT-5701] OLDTransmitter_Frequency_DSN_Range_DeepSpace_2 [GMT-5701] OLDTransmitter_Frequency_DSN_Range_DeepSpace [GMT-5701] OLDTrkFile_SimEst_DSN_DS_Range_Solve_Bias_apriori [GMT-5709] Python_IO_String [5317] ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522] Transmitter_Frequency_DSN_Doppler_DeepSpace_2 [GMT-5701] Transmitter_Frequency_DSN_Doppler_DeepSpace [GMT-5701] Transmitter_Frequency_DSN_Range_DeepSpace_2 [GMT-5701] Transmitter_Frequency_DSN_Range_DeepSpace [GMT-5701] TrkFile_SimEst_DSN_DS_Range_Solve_Bias_apriori [GMT-5709] TrkFile_SimEst_GN_RangeRate_Solve_Cd [GMT-5701] TrkFile_SimEst_GN_RangeRate_Solve_Cr [GMT-5701] TrkFile_SimEst_GN_range_Solve_Cd [GMT-5701] TrkFile_SimEst_GN_range_Solve_Cr [GMT-5701] 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] 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 15.2471, 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 14.3801, tol 1e-12] [GMT-4077] EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection [pos err 0.000230256, tol 1e-12] [GMT-4112] EphemStressTests_PD78_ABM_Prop_Code500_60Sec_Step_ForwardDirection [pos err 21.5627, 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 0.000810884, tol 1e-06] [GMT-2567] GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_BS [pos err 0.00236009, tol 0.0023] GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Max_Reduction_BS [pos err 0.00236009, tol 0.0023] GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Minimum_Reduction_BS [pos err 0.00236009, tol 0.0023] GMAT_LEO_PropSynchronization_BS [] GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS [pos err 0.0757314, tol 0.002] 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] OLDSimulator_Propagator_EarthPointMass_Drag/Simulator_Propagator_EarthPointMass_Drag_PosErr.report [diff 0.0207037, tol 4e-05] [GMT-5417] OLDSimulator_Propagator_EarthPointMass_SRP_Drag/Simulator_Propagator_EarthPointMass_SRP_Drag_PosErr.report [diff 0.0299541, tol 5e-05] [GMT-5417] OLDWrite_Multiple_ReportFile_Concise_2 [] [GMT-5801] OLDWrite_Multiple_ReportFile_Verbose_2 [#24 failed] [GMT-5801] 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] Simulator_Propagator_EarthPointMass_Drag/Simulator_Propagator_EarthPointMass_Drag_PosErr.report [diff 0.0207037, tol 4e-05] [GMT-5417] Simulator_Propagator_EarthPointMass_SRP_Drag/Simulator_Propagator_EarthPointMass_SRP_Drag_PosErr.report [diff 0.0299541, tol 5e-05] [GMT-5417] SpacecraftNavigation_SolveFors_CartesianState_LeapSec_Range [Parameter TDRS10.EarthTODEq.X value -11597.438317 exceeds tolerance 0.010000] [GMT-5954] SpacecraftNavigation_SolveFors_CartesianState_LeapSec_RangeRate [Parameter Aura.EarthMJ2000Eq.X value -4277.420356 exceeds tolerance 0.010000] [GMT-5954] SpacecraftNavigation_Validation_Mode [#1 failed] [GMT-5841] String_AssignNumericParam [] [GMT-2888] THF_Accel_CSA_None_NA [] [GMT-5701] THF_Accel_ECI_None_NA_3minutes_UnitZ [] [GMT-5701] THF_Accel_ECI_None_NA_3minutes_UnitZ_TSF [] [GMT-5701] THF_Accel_ECI_None_NA_3minutes_UnitZ_TSF_2 [] [GMT-5701] THF_Accel_ECI_None_NA_3minutes_UnitZ_TSF_3 [] [GMT-5701] THF_AccelMass_CSA_None_None [] [GMT-5701] THF_AccelMass_ECI_None_None_3minutes_UnitZ [] [GMT-5701] THF_AccelMass_ECI_None_None_3minutes_UnitZ_TSF [] [GMT-5701] THF_AccelMass_ECI_None_None_3minutes_UnitZ_TSF_2 [] [GMT-5701] THF_AccelMass_ECI_None_None_3minutes_UnitZ_TSF_3 [] [GMT-5701] THF_Sim_Accel_ConfigD_None_NA_2 [ Observable Error: 739.3 m.] [GMT-5986] THF_ThrustMass_CSA_None_None [] [GMT-5701] THF_ThrustMass_ECI_None_None_3minutes_UnitZ [] [GMT-5701] THF_ThrustMass_ECI_None_None_3minutes_UnitZ_TSF_2 [] [GMT-5701] THF_ThrustMass_ECI_None_None_3minutes_UnitZ_TSF_3 [] [GMT-5701] TrkFile_SimEst_TDRS_range_Solve_Cr [] [GMT-5416, GMT-5701] 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_STK_CentralBody_Moon_Meters [GMT-6093] 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_Code500_ACE_OpsPrototype_v13 [GMT-4112] 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] ErrorModel_NoiseSigma_RangeRate2 [GMT-5417] 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] OLDBatchEstimator_Nominal_Heliocentric_RangeDoppler [GMT-5417] OLDBatchEstimator_Nominal_L1_Range [GMT-5417] OLDWrite_Spacecraft_LogFile_Script [GMT-5802] ScriptLanguage_Validation_DataTypes_ReferenceArray_Formation_5 [GMT-6064] SpacePointParams_CelestialBody_EpochOutput [3939] SpacecraftNavigation_SolveFors_CartesianState_Cd_Cr_GN [GMT-5417] SpacecraftNavigation_SolveFors_CartesianState_Cd_RangeRate [GMT-5417] THF_AccelMass_CSB_None_None [GMT-5701] THF_AccelMass_CSC_None_None [GMT-5701, GMT-5981] THF_AccelMass_CSC_None_None_2 [GMT-5701] THF_Accel_CSB_None_NA [GMT-5701] THF_Accel_CSC_None_None [GMT-5701, GMT-5981] THF_Accel_CSC_None_None_2 [GMT-5701] THF_Sim_Accel_ConfigD_None_NA [GMT-5986] THF_ThrustMass_CSB_None_None [GMT-5701] THF_ThrustMass_CSC_None_None [GMT-5701, GMT-5981] THF_ThrustMass_CSC_None_None_2 [GMT-5701] THF_ThrustMass_ECI_None_None_3minutes_UnitZ_TSF [GMT-5701] THF_Thrust_CSA_None_NA [GMT-5701] THF_Thrust_CSB_None_NA [GMT-5701] THF_Thrust_CSC_None_None [GMT-5701, GMT-5981] THF_Thrust_CSC_None_None_2 [GMT-5981] THF_Thrust_ECI_None_NA_3minutes_UnitZ [GMT-5701] THF_Thrust_ECI_None_NA_3minutes_UnitZ_TSF [GMT-5701] THF_Thrust_ECI_None_NA_3minutes_UnitZ_TSF_2 [GMT-5701] THF_Thrust_ECI_None_NA_3minutes_UnitZ_TSF_3 [GMT-5701] Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
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