Test system results from last night.We'll need to look at adjusting tolerances/fixing truth data for the STK propagator now that it uses Hermite interpolation (vs the cubic spline it was using).
- 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: 13538 (+89 deferred) Percent Passed: 99.56% New issues: 36 Output changes: 0 New truth failures: 35 New crashes: 0 New script errors: 0 New comparator errors: 1 Fixed issues: 21 Total issues: 61 Test system warnings: 42 New deferred issues: 0 Fixed deferred issues: 0 Total deferred issues: 62 Run Time: 07 hours, 57 minutes, 08 seconds ----------------------------------------------------------------- New Issues ----------------------------------------------------------------- New truth failures: BatchEstimator_ReportFile_Range [#488 failed] EphemPropagator_STK_CentralBody_Jupiter [vel err 2.80476e-06, tol 3e-08] EphemPropagator_STK_CentralBody_Mars [vel err 3.49495e-06, tol 3e-08] EphemPropagator_STK_CentralBody_Moon [vel err 1.10099e-05, tol 3e-09] EphemPropagator_STK_CentralBody_Moon_Meters [vel err 1.10099e-05, tol 3e-09] [GMT-6093] EphemPropagator_STK_CentralBody_Saturn [vel err 1.49341e-06, tol 3e-08] EphemPropagator_STK_CentralBody_Sun [vel err 4.95649e-05, tol 3e-09] EphemPropagator_STK_CentralBody_Venus [vel err 2.55247e-06, tol 3e-08] EphemPropagator_STK_EphemCompare_LeapSecond [Output field 333.230000 failed tolerance in record 3602] EphemPropagator_STK_EphemCompare_Moon [Output field 53.769000 failed tolerance in record 432] EphemPropagator_STK_EphemCompare_Sun [Output field 241.664000 failed tolerance in record 416] EphemPropagator_STK_StepSize_1min [vel err 3.23542e-07, tol 6e-09] EphemPropagator_STK_StepSize_10min [vel err 2.14477e-07, tol 6e-09] EphemPropagator_STK_StepSize_60min [vel err 6.28231e-08, tol 6e-09] EphemPropagator_STK_TessEphemerisCheck [vel err 1.64485e-07, tol 6e-09] ErrorModel_BiasSigma_DsnSeqRange_DsnTcp [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_DSN [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_DsnTcp [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_GN [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_Range [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_Range_RangeRate [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_RangeRate [#1 failed] SpacecraftNavigation_SolveFors_CartesianState_EarthFixed [The test run failed to converge] [GMT-6408] SpacecraftNavigation_Validation_EstimationStateType [#1 failed] Write_Mode_Function [] Write_Spacecraft_LogFile_Concise [] Write_Spacecraft_LogFile_Script [#21 failed] Write_Spacecraft_LogFile_Verbose [] Write_Spacecraft_ReportFile_Concise [] Write_Spacecraft_ReportFile_LogFile_Script [] Write_Spacecraft_ReportFile_LogFile_Script [] Write_Spacecraft_ReportFile_Script [] Write_Spacecraft_ReportFile_Script_Include [] Write_Spacecraft_ReportFile_Script_RunEstimator [] Write_Spacecraft_ReportFile_Verbose [] Output changes (but still pass): None Output changes (but still fail): None New crashes/hangs/etc.: None New script errors: None New comparator errors: EphemTest_DE405_Moon_Neptune (truth) ----------------------------------------------------------------- Fixed Issues ----------------------------------------------------------------- Fixed truth failures: BatchEstimator_ReportFile_CovarianceCorrelationMatrix ForceModel_Validation_TideFile ForceModel_Validation_TideFile_ZeroTideModel ForceModel_Validation_TideModel SpacecraftNavigation_SolveFors_CartesianState_Cd_Cr_GN 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: Transmitter_Frequency_DSN_Doppler_DeepSpace_2 Transmitter_Frequency_DSN_Doppler_DeepSpace Transmitter_Frequency_DSN_Range_DeepSpace_2 Transmitter_Frequency_DSN_Range_DeepSpace TrkFile_SimEst_DSN_DS_Range_Solve_Inc_RAAN_apriori TrkFile_SimEst_DSN_DS_Range_Solve_RAAN_apriori Fixed comparator errors: None ----------------------------------------------------------------- All Known Issues ----------------------------------------------------------------- Crashes/hangs/etc.: None Script errors: ForceModel_GravityField_ZeroTide_Luna_TideModel_Solid: ERROR MESSAGE: Output file /home/buildbot/gsfcgmat/GmatDevelopment/GMAT-R2017a-Linux-x64/output/ForceModel_GravityField_ZeroTide_Luna_TideModel_Solid.txt does not exist Comparator errors: EphemTest_DE405_Moon_Neptune: (truth) ERROR MESSAGE: Comparator PVComparator failed: Error using fileread (line 26) Could not open file /home/buildbot/jazz/test/script/input/Resources/FRR-16_SolarSystem/truth/RotationDataSource_Deprecation_Warning.txtEphemTest_DE405_Moon_Neptune.truth. No such file or directory. Truth failures: BatchEstimator_ReportFile_Range [#488 failed] BatchEstimator_ReportFile_StateInformation [#4 failed] EphemPropagator_STK_CentralBody_Jupiter [vel err 2.80476e-06, tol 3e-08] EphemPropagator_STK_CentralBody_Mars [vel err 3.49495e-06, tol 3e-08] EphemPropagator_STK_CentralBody_Moon [vel err 1.10099e-05, tol 3e-09] EphemPropagator_STK_CentralBody_Moon_Meters [vel err 1.10099e-05, tol 3e-09] [GMT-6093] EphemPropagator_STK_CentralBody_Saturn [vel err 1.49341e-06, tol 3e-08] EphemPropagator_STK_CentralBody_Sun [vel err 4.95649e-05, tol 3e-09] EphemPropagator_STK_CentralBody_Venus [vel err 2.55247e-06, tol 3e-08] EphemPropagator_STK_EphemCompare_LeapSecond [Output field 333.230000 failed tolerance in record 3602] EphemPropagator_STK_EphemCompare_Moon [Output field 53.769000 failed tolerance in record 432] EphemPropagator_STK_EphemCompare_Sun [Output field 241.664000 failed tolerance in record 416] EphemPropagator_STK_Filter_Mnvr [pos err 0.00123461, tol 3e-06] EphemPropagator_STK_PositionAndVelocityDiscontinuity [] EphemPropagator_STK_PropTimeJump [vel err 1.08339e-09, tol 1e-09] EphemPropagator_STK_SmoothFile_4_0 [vel err 8.27125e-08, tol 6e-08] EphemPropagator_STK_SmoothFile_4_2 [vel err 8.27125e-08, tol 6e-08] EphemPropagator_STK_SmoothFile_4_3 [vel err 8.27125e-08, tol 6e-08] EphemPropagator_STK_SmoothFile_6_2 [vel err 8.27125e-08, tol 6e-08] EphemPropagator_STK_SmoothFile_8_0 [vel err 8.28961e-08, tol 6e-08] EphemPropagator_STK_StepSize_1min [vel err 3.23542e-07, tol 6e-09] EphemPropagator_STK_StepSize_10min [vel err 2.14477e-07, tol 6e-09] EphemPropagator_STK_StepSize_60min [vel err 6.28231e-08, tol 6e-09] EphemPropagator_STK_TessEphemerisCheck [vel err 1.64485e-07, tol 6e-09] EphemPropagator_STK_Validation_CentralBody_NoEffect [vel err 1.05079e-07, tol 1e-09] EphemPropagator_STK_VelocityDiscontinuity [pos err 0.00639492, tol 1e-06] ErrorModel_BiasSigma_DsnSeqRange_DsnTcp [#1 failed] Integrator_LEO_PD853_Accuracy [] Integrator_NoErrorControl_Warning [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_DSN [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_DsnTcp [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_GN [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_Keplerian_DSN [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_Keplerian_DsnSeqRange [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_Keplerian_RangeRate [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_Range [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_Range_RangeRate [#1 failed] SpacecraftNavigation_OrbitErrorCovariance_RangeRate [#1 failed] SpacecraftNavigation_SolveFors_CartesianState_EarthFixed [The test run failed to converge] [GMT-6408] SpacecraftNavigation_SolveFors_KeplerianState_Cd_Cr_Range [Parameter EstSat.EarthMJ2000Eq.AOP error 0.013477 exceeds tolerance 0.005000] SpacecraftNavigation_SolveFors_KeplerianState_EarthFixed [The test run failed to converge] SpacecraftNavigation_SolveFors_KeplerianState_LeapSec_Range [Parameter TDRS10.EarthTODEq.X error 2.248139 exceeds tolerance 0.010000] [GMT-5954] SpacecraftNavigation_SolveFors_KeplerianState_LeapSec_RangeRate [The test run failed to converge] [GMT-5954] SpacecraftNavigation_Validation_EstimationStateType [#1 failed] TrackingFileSet_ChebyshevDEBoundary_1day [ Observable Error: 0.0002995 Hz] TrackingFileSet_ChebyshevDEBoundary_1hour [ Observable Error: 0.8751 Hz] Write_Mode_Function [] Write_Spacecraft_LogFile_Concise [] Write_Spacecraft_LogFile_Script [#21 failed] Write_Spacecraft_LogFile_Verbose [] Write_Spacecraft_MultipleObjects [#12 failed] Write_Spacecraft_ReportFile_Concise [] Write_Spacecraft_ReportFile_LogFile_Script [] Write_Spacecraft_ReportFile_LogFile_Script [] Write_Spacecraft_ReportFile_Script [] Write_Spacecraft_ReportFile_Script_Include [] Write_Spacecraft_ReportFile_Script_RunEstimator [] Write_Spacecraft_ReportFile_Verbose [] Write_Spacecraft_Thruster [#10 failed] ----------------------------------------------------------------- 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): GMAT_LunarTransfer_AllPlanets_DE421_BS GMAT_MarsTransfer_4_BS Script errors (deferred): BatchEstimator_EstimationEpoch [GMT-5708, GMT-5701] Math_Shadowed_Builtins [GMT-3043] Python_IO_String [5317] ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522] 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 15.2507, tol 1e-12] [GMT-4077] EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection [pos err 9.57663, tol 1e-12] [GMT-4077] EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect [pos err 14.3819, tol 1e-12] [GMT-4077] EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection [pos err 0.000200011, 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 0.00081572, tol 1e-06] [GMT-2567] GMAT_LEO_PropSynchronization_BS [] GMAT_LunarTran_PropSynchronization_BS [max diff 5.74844e-08 > tol 5e-08] GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS [pos err 0.0748552, 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] 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_MoonOccultation [GMAT: 11299 lines, Truth: 11306 lines] [GMT-6134] Simulator_Propagator_EarthPointMass_Drag/Simulator_Propagator_EarthPointMass_Drag_PosErr.report [diff 0.0310455, tol 4e-05] [GMT-5417] Simulator_Propagator_EarthPointMass_SRP_Drag/Simulator_Propagator_EarthPointMass_SRP_Drag_PosErr.report [diff 0.0437413, tol 5e-05] [GMT-5417] SpacecraftNavigation_SolveFors_CartesianState_LeapSec_Range [Parameter TDRS10.EarthTODEq.X error 2.248239 exceeds tolerance 0.010000] [GMT-5954] SpacecraftNavigation_SolveFors_CartesianState_LeapSec_Range [Parameter TDRS10.EarthTODEq.X error 2.248239 exceeds tolerance 0.010000] [GMT-5954] SpacecraftNavigation_SolveFors_CartesianState_LeapSec_RangeRate [Parameter Aura.EarthMJ2000Eq.X error 1.965657 exceeds tolerance 0.010000] [GMT-5954] SpacecraftNavigation_SolveFors_CartesianState_LeapSec_RangeRate [Parameter Aura.EarthMJ2000Eq.X error 1.965657 exceeds tolerance 0.010000] [GMT-5954] SpacecraftNavigation_Validation_Mode [#1 failed] [GMT-5841] String_AssignNumericParam [] [GMT-2888] THF_Sim_Accel_ConfigD_None_NA [ Observable Error: 0.3426 m.] [GMT-5986] THF_Sim_Accel_ConfigD_None_NA_2 [ Observable Error: 739.3 m.] [GMT-5986] THF_Sim_Accel_ConfigD_None_NA_3 [ Observable Error: 0.2607 m.] [GMT-5986] THF_Sim_Accel_ConfigD_None_NA_4 [ Observable Error: 0.04548 m.] [GMT-5986] 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_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] ScriptLanguage_Validation_DataTypes_ReferenceArray_Formation_5 [GMT-6064] 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] SpacecraftNavigation_L1_DsnSeqRange_SOHO_AncillaryElements [GMT-6040] SpacecraftNavigation_L1_DsnSeqRange_SOHO_CovarianceCorrelationMatrix [GMT-6040] SpacecraftNavigation_L1_DsnSeqRange_SOHO_EstimatedState [GMT-6040] THF_AccelMass_CSC_None_None [GMT-5981] THF_Accel_CSC_None_None [GMT-5981] THF_ThrustMass_CSC_None_None [GMT-5981] THF_Thrust_CSC_None_None [GMT-5981] THF_Thrust_CSC_None_None_2 [GMT-5981] Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
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