I agree. On 10/15/2015 02:18 PM, Jun, Linda O. (GSFC-5830) wrote: > I think we still need to run nightly test since we are committing changes. > > Linda > > -----Original Message----- > From: Parker, Joel J. K. (GSFC-5950) [mailto:[email protected]] > Sent: Thursday, October 15, 2015 5:10 PM > To: Parker, Joel J. K. (GSFC-5950); [email protected] > Subject: Re: [Gmat-buildtest] Test results: 2015-10-13 > (GS580W-GMAT-T4/Win7-64/GMAT-32/M2014a/VS2013) > > Sorry folks, ignore this. I didn't get in and disable the nightly test runs. > Doing it now... > > JP > > -----Original Message----- > From: [email protected] [mailto:[email protected]] > Sent: Thursday, October 15, 2015 4:23 PM > To: [email protected] > Subject: [Gmat-buildtest] Test results: 2015-10-13 > (GS580W-GMAT-T4/Win7-64/GMAT-32/M2014a/VS2013) > > ----------------------------------------------------------------- > Summary > ----------------------------------------------------------------- > System configuration: GS580W-GMAT-T4/Win7-64/GMAT-32/M2014a/VS2013 > Tested build: 2015-10-13 > Regression build: 2015-10-10 > > Total number of scripts: 12512 (+81 deferred) > Percent Passed: 99.76% > New issues: 1 > Output changes: 0 > New truth failures: 0 > New crashes: 1 > New script errors: 0 > New comparator errors: 0 > Fixed issues: 0 > Total issues: 30 > > Test system warnings: 17 > New deferred issues: 35 > Fixed deferred issues: 2 > Total deferred issues: 74 > > Run Time: 00 hours, 16 minutes, 14 seconds > > ----------------------------------------------------------------- > New Issues > ----------------------------------------------------------------- > New truth failures: > None > > Output changes (but still pass): > None > > Output changes (but still fail): > None > > New crashes/hangs/etc.: > XYPlotStressTests_PD78_ABM_Prop_CCSDS_60Sec_Step_ForwardDirection > > 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.: > CommandMode_GroundTrackPlot_Field_Tests_Maximized > FindEvents_ControlFlow_While [GMT-5361] > Thruster_Finite_Burn_Permutations_Separate_Propagators_VNB_2 > XYPlotStressTests_PD78_ABM_Prop_CCSDS_60Sec_Step_ForwardDirection > > Script errors: > CommandMode_GroundTrackPlot_FieldTests_TestingRelativeZOrder > Events_TESS_Optimize_TwoStage_FromLaunch_master_03b4b32 > > GMATFunction_ACE_impulsive_493_Global_Subscribers_User_Defined_Parameters > Python_IO_String [5317] > > Comparator errors: > None > > Truth failures: > DensityParam_Validation_Disabled_AtmosDensity [no error or exception] > Ephem_GMAT_SPK_60sec_backward [failed reading state 1/15 from SPK] > [GMT-5286] > Ephem_GMAT_SPK_60sec_target [vel err 0.900016, tol 1e-06] > Ephem_GMAT_SPK_DefaultIntegrationStep_User_Defined_LagrangeOrder > [failed reading state 1/19 from SPK] [GMT-5286] > Events_ContactLocator_EarthTransit [diff # events] > Events_ContactLocator_OccultingBodies_Multiple [diff # events] > Events_EclipseLocator_MarsLong [start diff = 0.001006s (mars/9)] > FindEvents_ControlFlow_For [diff occ bodies] [GMT-5360] > FindEvents_ControlFlow_Target [diff # events for earth] > FMParams_Validation_Disabled_Acceleration [no error or exception] > FMParams_Validation_Disabled_AccelerationX [no error or exception] > FMParams_Validation_Disabled_AccelerationY [no error or exception] > FMParams_Validation_Disabled_AccelerationZ [no error or exception] > GMAT_ISS_Earth_0_JR_0_CSSI [pos err 2.73498, tol 0.002] > GMAT_ISS_Earth_0_MSISE86_0_CSSI [pos err 0.0463992, tol 0.002] > GMAT_ISS_Earth_0_MSISE90_0_CSSI [pos err 0.0125291, tol 0.002] > GMAT_ISS_Earth_0_MSISE90_0_CSSI_AssignmentOperator [pos err 0.0125291, > tol 0.002] > GMAT_ISS_Earth_0_NRLMSISE00_0_CSSI [pos err 0.0123784, tol 0.002] > GMAT_UserMoon-Titan_AllPlanets_SRP_AboutAsteroid [pos err 5569.14, tol > 0.002] [GMT-5262] > GMAT_UserMoon-Titan_AllPlanets_SRP_AboutComet [pos err 5569.14, tol > 0.002] [GMT-5262] > ScriptLanguage_Validation_FilePaths_3 [no error or exception] > SolarSystem_Bug2437 [max diff 2.09863e-12 > tol 1e-12max diff 1e-12 > > tol ] > > ----------------------------------------------------------------- > 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): > Ex_Integrators > GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_BS > > GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Max_Reduction_BS > > GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Minimum_Reduction_BS > GMAT_LEO_PropSynchronization_BS > GMAT_LunarTran_PropSynchronization_BS > GMAT_LunarTransfer_AllPlanets_DE421_BS > GMAT_MarsTransfer_4_BS > GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS > Integrator_BS_InitialStep > Integrator_GEO_BS_2Body > Integrator_ISS_BS_2Body > Integrator_LEO_BS_Accuracy > Integrator_LEO_BS_ErrorControl > Integrator_Max_Step_BS > STM_GMAT_BLSTR > Save_Barycenter > Save_DifferentialCorrector > Save_FiniteBurn > Save_Formation > Save_GroundStation_Cartesian > Save_GroundStation_Spherical > Save_ImpulsiveBurn_EarthFixed_Decrement_Tank1 > Save_ImpulsiveBurn_EarthFixed_~Decrement > Save_ImpulsiveBurn_Local_Decrement_Tank1 > Save_ImpulsiveBurn_Local_~Decrement > Save_LibrationPoint > Save_SQP > Save_Simulator > ScriptEvent_SmokeTests_Save_GroundStation_Spherical > Target_DC_Command_Save > Thruster_FBurn_Earth_ScA_ThrusterB_CS2_TankA_BS > Thruster_FBurn_Earth_ScA_ThrusterB_CS3_TankL_BS > Thruster_FBurn_Earth_ScA_ThrusterB_CS3_TankL_Max_Reduction_BS > Thruster_FBurn_Earth_ScA_ThrusterB_CS3_TankL_Minimum_Reduction_BS > > New comparator errors (deferred): > None > > ----------------------------------------------------------------- > Fixed Issues (Deferred) > ----------------------------------------------------------------- > Fixed truth failures (deferred): > None > > Fixed crashes/hangs/etc. (deferred): > GMAT_LunarTransfer_AllPlanets_DE421_BS > GMAT_MarsTransfer_4_BS > > Fixed script errors (deferred): > None > > Fixed comparator errors (deferred): > None > > ----------------------------------------------------------------- > All Known Issues (Deferred) > ----------------------------------------------------------------- > Crashes/hangs/etc. (deferred): > None > > Script errors (deferred): > Ex_Integrators > GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_BS > > GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Max_Reduction_BS > > GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Minimum_Reduction_BS > GMAT_LEO_PropSynchronization_BS > GMAT_LunarTran_PropSynchronization_BS > GMAT_LunarTransfer_AllPlanets_DE421_BS > GMAT_MarsTransfer_4_BS > GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS > GS_Nav_DeepSpace_DSN_Media > Integrator_BS_InitialStep > Integrator_GEO_BS_2Body > Integrator_ISS_BS_2Body > Integrator_LEO_BS_Accuracy > Integrator_LEO_BS_ErrorControl > Integrator_Max_Step_BS > Math_Shadowed_Builtins [GMT-3043] > STM_GMAT_BLSTR > Save_Barycenter > Save_DifferentialCorrector > Save_FiniteBurn > Save_Formation > Save_GroundStation_Cartesian > Save_GroundStation_Spherical > Save_ImpulsiveBurn_EarthFixed_Decrement_Tank1 > Save_ImpulsiveBurn_EarthFixed_Decrement_~Tank > Save_ImpulsiveBurn_EarthFixed_~Decrement > Save_ImpulsiveBurn_Local_Decrement_Tank1 > Save_ImpulsiveBurn_Local_Decrement_~Tank > Save_ImpulsiveBurn_Local_~Decrement > Save_LibrationPoint > Save_SQP > Save_Simulator > Save_Thruster_EarthFixed_Decrement_NoTank > Save_Thruster_EarthFixed_Decrement_Tank1 > Save_Thruster_EarthFixed_NoDecrement > Save_Thruster_Local_Decrement_NoTank > Save_Thruster_Local_Decrement_Tank1 > Save_Thruster_Local_NoDecrement > ScriptEvent_SmokeTests_Save_GroundStation_Spherical > ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522] > Target_DC_Command_Save > Thruster_FBurn_Earth_ScA_ThrusterB_CS2_TankA_BS > Thruster_FBurn_Earth_ScA_ThrusterB_CS3_TankL_BS > Thruster_FBurn_Earth_ScA_ThrusterB_CS3_TankL_Max_Reduction_BS > Thruster_FBurn_Earth_ScA_ThrusterB_CS3_TankL_Minimum_Reduction_BS > > Comparator errors (deferred): > None > > Truth failures (deferred): > Achieve_Validation_LHS_Field [ptrn 1 failed] [GMT-3687] > Achieve_Validation_RHS_Field [no error or exception] [GMT-3687] > Ephem_GMAT_Code500_ACE_OpsPrototype_v13 [pos err 1.36904, tol 1] > [GMT-4112] > > Ephem_GMAT_Code500_InterpolationOrder/Ephem_GMAT_Code500_InterpolationOrder_1.eph > [pos err 0.0177967, 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 15.2522, 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 14.1473, tol 1e-12] [GMT-4077] > > EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection > [pos err 0.000224514, 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 mjd diff 1.000111s > 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 0.00081427, tol > 1e-06] [GMT-2567] > 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] > 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] > String_AssignNumericParam [] [GMT-2888] > Vary_Validation_RHS_Field [no error or exception] [GMT-3687] > > ----------------------------------------------------------------- > 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_SatAssigmentToNewSatThenProp [GMT-3434] > 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] > SpacePointParams_CelestialBody_EpochOutput [3939] > Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455] > > > ------------------------------------------------------------------------------ > 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