Updates pushed. This should move the Drag tests back to passing, starting with tomorrow's build.
- DJC On 09/09/2015 08:47 AM, Darrel J. Conway wrote: > Found the issue. It comes from setting the defaults for the file name > -- the code isn't handling a case where you use constants when a file > name is specified. It'll be fixed today, but likely this afternoon/evening. > > - DJC > > On 09/09/2015 08:34 AM, Darrel J. Conway wrote: >> The toggle between using constant values and using file based values was >> broken somewhere, and we now are using file values all the time. Sigh. >> I'll get it fixed today, but probably not in time for the build that >> starts in half an hour! >> >> - DJC >> >> On 09/09/2015 07:58 AM, Hughes, Steven P. (GSFC-5950) wrote: >>> We had a major regression related to density in this build. Darrel is >>> investigating. Many propagation tests and density params failed in this >>> build. >>> >>> -----Original Message----- >>> From: [email protected] [mailto:[email protected]] >>> Sent: Wednesday, September 09, 2015 9:55 AM >>> To: [email protected] >>> Subject: [Gmat-buildtest] Test results: 2015-09-08 >>> (GS580W-GMAT-T4/Win7-64/GMAT-32/M2014a/VS2013) >>> >>> ----------------------------------------------------------------- >>> Summary >>> ----------------------------------------------------------------- >>> System configuration: GS580W-GMAT-T4/Win7-64/GMAT-32/M2014a/VS2013 >>> Tested build: 2015-09-08 >>> Regression build: 2015-09-04 >>> >>> Total number of scripts: 12280 (+81 deferred) >>> Percent Passed: 98.09% >>> New issues: 2 >>> Output changes: 0 >>> New truth failures: 0 >>> New crashes: 1 >>> New script errors: 1 >>> New comparator errors: 0 >>> Fixed issues: 1 >>> Total issues: 237 >>> >>> Test system warnings: 19 >>> New deferred issues: 0 >>> Fixed deferred issues: 0 >>> Total deferred issues: 74 >>> >>> Run Time: 18 hours, 47 minutes, 06 seconds >>> >>> ----------------------------------------------------------------- >>> New Issues >>> ----------------------------------------------------------------- >>> New truth failures: >>> None >>> >>> Output changes (but still pass): >>> None >>> >>> Output changes (but still fail): >>> None >>> >>> New crashes/hangs/etc.: >>> Optimize_fmincon_cvg_status >>> >>> New script errors: >>> scriptEvent_optimizer_fmincon__InitialValue_Array >>> >>> New comparator errors: >>> None >>> >>> ----------------------------------------------------------------- >>> Fixed Issues >>> ----------------------------------------------------------------- >>> Fixed truth failures: >>> None >>> >>> Fixed crashes/hangs/etc.: >>> None >>> >>> Fixed script errors: >>> Optimize_fmincon_ExitMode_DiscardAndContinue_3 >>> >>> Fixed comparator errors: >>> None >>> >>> ----------------------------------------------------------------- >>> All Known Issues >>> ----------------------------------------------------------------- >>> Crashes/hangs/etc.: >>> Optimize_fmincon_cvg_status >>> >>> Script errors: >>> Events_ContactLocator_DiscontinuousEphem_EpochOnly [GMT-5232] >>> Events_ContactLocator_DiscontinuousEphem_UseEntireInterval_False >>> [GMT-5232] >>> Events_ContactLocator_DiscontinuousEphem_UseEntireInterval_True >>> Events_ContactLocator_EarthTransit >>> Events_EclipseLocator_OccultingBodies_UserDefined [GMT-5254] >>> Events_TESS_Optimize_TwoStage_FromLaunch_master_03b4b32 >>> Math_Math_GmatFunction [GMT-5262] >>> PythonFunction_Builtin >>> PythonFunction_Custom_DegToRad_Assignment >>> PythonFunction_Custom_DegToRad >>> PythonFunction_Custom_magic >>> PythonFunction_Custom >>> PythonFunction_FunctionPath_Relative >>> Python_IO_Array >>> Python_IO_Real >>> Python_IO_String >>> Python_NoInputs >>> Python_VariableInputs >>> ScriptEvent_SmokeTests_Events_Eclipse_Simple >>> Thruster_OtherNumericProperties_Cmd [GMT-5261] >>> scriptEvent_optimizer_fmincon__InitialValue_Array >>> >>> Comparator errors: >>> Events_ContactLocator_StepSize_TooLarge (truth) >>> Events_ContactLocator_Target_Propagated_NoPropagate (truth) >>> >>> Truth failures: >>> Ballistic_and_Mass_Case01_GTO [pos err 215.36, tol 0.0025] >>> Ballistic_and_Mass_Case01_LEO [pos err 10.196, tol 0.001] >>> Ballistic_and_Mass_Case01_LEO_Cmd [pos err 10.196, tol 0.001] >>> Ballistic_and_Mass_Case02_GTO [pos err 316.081, tol 0.0025] >>> Ballistic_and_Mass_Case02_LEO [pos err 14.9831, tol 0.001] >>> Ballistic_and_Mass_Case03_GTO [pos err 198.436, tol 0.0025] >>> Ballistic_and_Mass_Case03_LEO [pos err 9.3788, tol 0.001] >>> Ballistic_and_Mass_Case04_GTO [pos err 9.00029, tol 0.0025] >>> Ballistic_and_Mass_Case04_LEO [pos err 0.846407, tol 0.001] >>> DensityParam_ISS_JR [max diff 0.00505267 > tol 1e-07] >>> DensityParam_ISS_MSISE86 [max diff 0.00351689 > tol 1e-07] >>> DensityParam_ISS_MSISE90 [max diff 0.00356521 > tol 1e-07] >>> DensityParam_ISS_NRLMSISE00 [max diff 0.00197445 > tol 5e-05] >>> Ephem_GMAT_SPK_60sec_backward [failed reading state 1/15 from >>> SPK] >>> Ephem_GMAT_SPK_60sec_for_loop [failed reading state 10/10 from >>> SPK] >>> Ephem_GMAT_SPK_60sec_if_loop [failed reading state 121/121 from >>> SPK] >>> Ephem_GMAT_SPK_60sec_ifelse1_loop [failed reading state 121/121 >>> from SPK] >>> Ephem_GMAT_SPK_60sec_ifelse2_loop [failed reading state 121/121 >>> from SPK] >>> Ephem_GMAT_SPK_60sec_target [failed reading state 1/162 from >>> SPK] >>> Ephem_GMAT_SPK_60sec_while_loop [failed reading state 721/721 >>> from SPK] >>> Ephem_GMAT_SPK_60sec_with_600secFB [failed reading state >>> 1010/1010 from SPK] >>> >>> Ephem_GMAT_SPK_DefaultIntegrationStep_User_Defined_LagrangeOrder [failed >>> reading state 1/21 from SPK] >>> >>> Ephem_GMAT_SPK_DifferentTimeFormats_OptionallyDisplayEphemData/Ephem_GMAT_SPK_DifferentTimeFormats_OptionallyDisplayEphemData_UTCGregorian.bsp >>> [failed reading state 1/123 from SPK] >>> >>> Ephem_GMAT_SPK_DifferentTimeFormats_OptionallyDisplayEphemData/Ephem_GMAT_SPK_DifferentTimeFormats_OptionallyDisplayEphemData_TAIGregorian.bsp >>> [failed reading state 1/123 from SPK] >>> >>> Ephem_GMAT_SPK_DifferentTimeFormats_OptionallyDisplayEphemData/Ephem_GMAT_SPK_DifferentTimeFormats_OptionallyDisplayEphemData_TTGregorian.bsp >>> [failed reading state 1/123 from SPK] >>> >>> Ephem_GMAT_SPK_DifferentTimeFormats_OptionallyDisplayEphemData/Ephem_GMAT_SPK_DifferentTimeFormats_OptionallyDisplayEphemData_A1Gregorian.bsp >>> [failed reading state 1/123 from SPK] >>> Events_ContactLocator_Antumbra [start diff = 0.100010s (event >>> 5)] [GMT-5209] >>> Events_ContactLocator_CBSizeShape [incorr. metadata] [GMT-5209] >>> Events_ContactLocator_DiscontinuousEphem_InitialEpochInGap >>> [start diff = 119.399996s (event 1)] [GMT-5232] >>> Events_ContactLocator_Ephemeris_DE405 [diff # events] [GMT-5209] >>> Events_ContactLocator_Filename_RelativePath [incorr. metadata] >>> [GMT-5209] >>> Events_ContactLocator_Filename_SetInMissionSequence [incorr. >>> metadata] [GMT-5209] >>> Events_ContactLocator_FinalEpoch_EphemBound [incorr. metadata] >>> [GMT-5209] >>> Events_ContactLocator_FinalEpoch_EventBoundary_Stop [dur diff = >>> 5.060870s (event 2)] [GMT-5209] >>> Events_ContactLocator_FinalEpoch_Exact [end diff = 54.599996s >>> (event 2)] [GMT-5209] >>> Events_ContactLocator_FinalEpoch_LessThanStepSize [end diff = >>> 0.399998s (event 1)] >>> Events_ContactLocator_FinalEpoch_SetInMissionSequence [end diff >>> = 54.599996s (event 2)] [GMT-5171] >>> Events_ContactLocator_Geo [end diff = 54.599996s (event 1)] >>> [GMT-5209] >>> Events_ContactLocator_Heo1 [dur diff = 0.482993s (event 2)] >>> [GMT-5209] >>> Events_ContactLocator_Heo2 [start diff = 0.900005s (event 2)] >>> [GMT-5209] >>> Events_ContactLocator_InitialEpoch_EphemBound [incorr. >>> metadata] [GMT-5209] >>> Events_ContactLocator_InitialEpoch_EventBoundary_Start [incorr. >>> metadata] [GMT-5209] >>> Events_ContactLocator_InitialEpoch_EventBoundary_Stop [diff # >>> events] >>> Events_ContactLocator_InputEpochFormat_A1ModJulian [dur diff = >>> 0.008184s (event 2)] >>> Events_ContactLocator_InputEpochFormat_Default [dur diff = >>> 0.008184s (event 2)] >>> Events_ContactLocator_InputEpochFormat_TAIGregorian [dur diff = >>> 0.008184s (event 2)] >>> Events_ContactLocator_Interplanetary [start diff = 54.099998s >>> (event 216)] [GMT-5254] >>> Events_ContactLocator_Leo [diff # events] [GMT-5209] >>> Events_ContactLocator_LightTimeDirection_Receive [diff # >>> events] [GMT-5209] >>> Events_ContactLocator_LightTimeDirection_Transmit [start diff = >>> 57.200002s (event 4)] [GMT-5209] >>> Events_ContactLocator_Lunar [diff # events] [GMT-5209] >>> Events_ContactLocator_MarsLong [diff # events] [GMT-5209] >>> Events_ContactLocator_Martian [diff # events] [GMT-5254] >>> Events_ContactLocator_NoEvent [diff # events] >>> Events_ContactLocator_Observers_GSCartesian [incorr. metadata] >>> [GMT-5209] >>> Events_ContactLocator_Observers_GSMinEl85 [dur diff = 0.003744s >>> (event 2)] [GMT-5209] >>> Events_ContactLocator_Observers_Multiple [diff # events] >>> [GMT-5209] >>> Events_ContactLocator_Observers_Repeated [incorr. metadata] >>> [GMT-5172] >>> Events_ContactLocator_Observers_Single [incorr. metadata] >>> [GMT-5209] >>> Events_ContactLocator_Observers_Single_NoBrackets [incorr. >>> metadata] [GMT-5209] >>> Events_ContactLocator_OccultingBodies_Duplicate [diff # events] >>> [GMT-5205] >>> Events_ContactLocator_OccultingBodies_GSCentralBody [incorr. >>> metadata] [GMT-5209] >>> Events_ContactLocator_OccultingBodies_NoEvent [incorr. >>> metadata] [GMT-5209] >>> Events_ContactLocator_OccultingBodies_Single [diff # events] >>> [GMT-5209] >>> Events_ContactLocator_OccultingBodies_Single_NoBrackets [diff # >>> events] [GMT-5209] >>> Events_ContactLocator_OccultingBodies_UserDefined [diff # >>> events] [GMT-5254] >>> Events_ContactLocator_Pluto [start diff = 57.200002s (event 4)] >>> [GMT-5209] >>> Events_ContactLocator_RunMode_Automatic [incorr. metadata] >>> [GMT-5209] >>> Events_ContactLocator_RunMode_Automatic_WithFindEvents [incorr. >>> metadata] [GMT-5209] >>> Events_ContactLocator_RunMode_Manual [incorr. metadata] >>> [GMT-5209] >>> Events_ContactLocator_Simple [incorr. metadata] [GMT-5209] >>> Events_ContactLocator_StepSize_Default [incorr. metadata] >>> [GMT-5209] >>> Events_ContactLocator_StepSize_NonDefault [incorr. metadata] >>> [GMT-5209] >>> Events_ContactLocator_Target_Propagated [incorr. metadata] >>> [GMT-5209] >>> Events_ContactLocator_Target_SPKPropagation [dur diff = >>> 0.008184s (event 2)] >>> Events_ContactLocator_Target_SPKPropagation_NoPropagate [incorr. >>> metadata] [GMT-5209] >>> Events_ContactLocator_UseEntireInterval_Default [incorr. >>> metadata] [GMT-5209] >>> Events_ContactLocator_UseEntireInterval_False [end diff = >>> 54.599996s (event 2)] [GMT-5209] >>> Events_ContactLocator_UseEntireInterval_True [incorr. metadata] >>> [GMT-5209] >>> Events_ContactLocator_UseLightTimeDelay_Default [start diff = >>> 57.200002s (event 4)] [GMT-5209] >>> Events_ContactLocator_UseLightTimeDelay_False [start diff = >>> 7440.800005s (event 8)] >>> Events_ContactLocator_UseLightTimeDelay_True [start diff = >>> 57.200002s (event 4)] [GMT-5209] >>> Events_ContactLocator_UseStellarAberration_Default [start diff >>> = 57.200002s (event 4)] [GMT-5209] >>> Events_ContactLocator_UseStellarAberration_False [diff # >>> events] [GMT-5209] >>> Events_ContactLocator_UseStellarAberration_True [start diff = >>> 57.200002s (event 4)] [GMT-5209] >>> Events_ContactLocator_Validation_FinalEpoch_BeyondEnd [no error >>> or exception] >>> Events_ContactLocator_Validation_InitialEpoch_BeforeStart [no >>> error or exception] >>> Events_ContactLocator_WriteReport_Default [incorr. metadata] >>> [GMT-5209] >>> Events_ContactLocator_WriteReport_SetInMissionSequence [incorr. >>> metadata] [GMT-5209] >>> Events_ContactLocator_WriteReport_True [incorr. metadata] >>> [GMT-5209] >>> Events_EclipseLocator_Antumbra [end diff = 1.100004s (earth/1)] >>> Events_EclipseLocator_CBSizeShape [start diff = 175.300005s >>> (earth/5)] >>> Events_EclipseLocator_DiscontinuousEphem_EpochOnly [start diff >>> = 1799.199998s (earth/5)] [GMT-5232] >>> Events_EclipseLocator_DiscontinuousEphem_FinalEpochInGap [diff >>> # events for earth] >>> >>> Events_EclipseLocator_DiscontinuousEphem_UseEntireInterval_False [diff # >>> events for earth] >>> Events_EclipseLocator_DiscontinuousEphem_UseEntireInterval_True >>> [diff # events for earth] >>> Events_EclipseLocator_EarthTransit [diff occ bodies] [GMT-5254] >>> Events_EclipseLocator_EclipseTypes_Antumbra [diff occ bodies] >>> Events_EclipseLocator_Ephemeris_DE405 [diff occ bodies] >>> [GMT-5075] >>> Events_EclipseLocator_FinalEpoch_EventBoundary_Start [diff # >>> events for earth] >>> Events_EclipseLocator_FinalEpoch_Exact [diff # events for earth] >>> Events_EclipseLocator_InitialEpoch_EventBoundary_Start [diff # >>> events for earth] >>> Events_EclipseLocator_InitialEpoch_EventBoundary_Stop [diff # >>> events for earth] >>> Events_EclipseLocator_InitialEpoch_SetInMissionSequence [start >>> diff = 0.100010s (earth/2)] [GMT-5171] >>> Events_EclipseLocator_Interplanetary [start diff = 0.299998s >>> (mars/2)] [GMT-5254] >>> Events_EclipseLocator_Leo [diff # events for earth] >>> Events_EclipseLocator_Lunar [start diff = 0.199999s (earth/2)] >>> Events_EclipseLocator_MarsLong [diff occ bodies] >>> Events_EclipseLocator_Martian [diff # events for mars] >>> [GMT-5254] >>> Events_EclipseLocator_OccultingBodies_Duplicate [diff occ >>> bodies] [GMT-5205] >>> Events_EclipseLocator_OccultingBodies_Multiple [diff # events >>> for earth] >>> Events_EclipseLocator_OccultingBodies_Single [start diff = >>> 54.099998s (luna/4)] >>> Events_EclipseLocator_OccultingBodies_Single_NoBrackets [start >>> diff = 54.099998s (luna/4)] >>> Events_EclipseLocator_Pluto [diff # events for pluto] >>> Events_EclipseLocator_Spacecraft_SPKPropagation [start diff = >>> 0.100010s (earth/3)] >>> Events_EclipseLocator_UseLightTimeDelay_Default [diff # events >>> for pluto] >>> Events_EclipseLocator_UseLightTimeDelay_True [diff # events for >>> pluto] >>> Events_EclipseLocator_UseStellarAberration_Default [diff # >>> events for pluto] >>> Events_EclipseLocator_UseStellarAberration_True [diff # events >>> for pluto] >>> >>> Events_EclipseLocator_Validation_DiscontinuousEphemeris_InitialFinalEpochs >>> [no error or exception] >>> >>> Events_EclipseLocator_Validation_DiscontinuousEphemeris_UseEntireInterval >>> [no error or exception] >>> FindEvents_Append_True [diff # events for earth] [GMT-5256] >>> FindEvents_ControlFlow_For [diff occ bodies] [GMT-5452] >>> FindEvents_ControlFlow_While [diff occ bodies] [GMT-5219] >>> FindEvents_Locator_ContactLocator [incorr. metadata] [GMT-5209] >>> FMParams_GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP [max diff >>> 0.00487103 > tol 1e-09] >>> ForceModel_DeprecatedDragFlux_JR [max diff 0.0167806 > tol >>> 1e-07] >>> ForceModel_DeprecatedDragFlux_MSISE00 [max diff 0.0151116 > tol >>> 1e-07] >>> ForceModel_DeprecatedDragFlux_MSISE86 [max diff 0.0174618 > tol >>> 1e-07] >>> ForceModel_DeprecatedDragFlux_MSISE90 [max diff 0.0173753 > tol >>> 1e-07] >>> ForceModel_MultipleLinesSettingDragBug2939 [pos err 345.77, tol >>> 0.001] >>> GMAT_ISS_Earth_0_JR_0 [pos err 27.9777, tol 0.002] >>> GMAT_ISS_Earth_0_JR_0_NonDefaultEarthRadiusFlattening [GMAT: >>> 720 lines, >>> Truth: 1441 lines] >>> GMAT_ISS_Earth_0_JR_ModifiedFluxAndGeoMag [pos err 55.73, tol >>> 0.005] >>> GMAT_ISS_Earth_0_MSISE86_0 [pos err 26.2686, tol 0.002] >>> GMAT_ISS_Earth_0_MSISE86_0_NonDefaultEarthRadiusFlattening [pos >>> err 45.6227, tol 0.002] >>> GMAT_ISS_Earth_0_MSISE86_ModifiedFluxAndGeoMag [pos err >>> 53.9063, tol 0.002] >>> GMAT_ISS_Earth_0_MSISE90_0 [pos err 46.834, tol 0.002] >>> GMAT_ISS_Earth_0_MSISE90_0_NonDefaultEarthRadiusFlattening [pos >>> err 45.8953, tol 0.002] >>> GMAT_ISS_Earth_0_MSISE90_ModifiedFluxAndGeoMag [pos err >>> 54.2245, tol 0.002] >>> GMAT_ISS_Earth_0_NRLMSISE00_0 [pos err 46.8817, tol 0.002] >>> GMAT_ISS_Earth_0_NRLMSISE00_0_NonDefaultEarthRadiusFlattening >>> [pos err 45.932, tol 0.002] >>> GMAT_ISS_Earth_0_NRLMSISE00_ModifiedFluxAndGeoMag [pos err >>> 54.1819, tol 0.002] >>> GMAT_ISS_EarthSunLuna_EGM96_JR_SRP [pos err 51.3189, tol 0.002] >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP [pos err 52.1236, tol >>> 0.002] >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_EControl_LargestState >>> [pos err 52.1233, tol 0.002] >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_EControl_LargestStep >>> [pos err 52.1233, tol 0.002] >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_EControl_None [pos err >>> 52.1232, tol 0.002] >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_EControl_RSSState [pos >>> err 52.1232, tol 0.002] >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_EControl_RSSStep [pos >>> err 52.1233, tol 0.002] >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide [pos >>> err 52.1215, tol 0.002] >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_ABM >>> [pos err 52.1215, tol 0.002] >>> >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_LargeMaxStep >>> [pos err 0.949464, tol 0.002] >>> >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Lower_Error_ABM >>> [pos err 52.1215, tol 0.002] >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_PD45 >>> [pos err 52.1216, tol 0.002] >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_PD78 >>> [pos err 52.1215, tol 0.002] >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_PD853 >>> [pos err 29.2801, tol 0.0025] >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_RK56 >>> [pos err 52.1215, tol 0.002] >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_RKN68 >>> [pos err 52.1257, tol 0.07] >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_RKV89 >>> [pos err 52.1215, tol 0.002] >>> >>> GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Target_Error_ABM >>> [pos err 52.1215, tol 0.002] >>> GMAT_ISS_EarthSunLuna_JGM2_JR_SRP [pos err 51.3188, tol 0.002] >>> GMAT_ISS_EarthSunLuna_JGM2_MSISE86_SRP [pos err 51.8257, tol >>> 0.002] >>> GMAT_ISS_EarthSunLuna_JGM2_MSISE90_SRP [pos err 52.1238, tol >>> 0.002] >>> GMAT_ISS_EarthSunLuna_JGM2_NRLMSISE00_SRP [pos err 52.2121, tol >>> 0.002] >>> GMAT_ISS_EarthSunLuna_JGM3_JR_SRP [pos err 51.3161, tol 0.005] >>> GMAT_ISS_EarthSunLuna_JGM3_MSISE90_SRP [pos err 29.2825, tol >>> 0.002] >>> GMAT_ISS_EarthSunLuna_JGM3_MSISE90_SRP_Cmd [pos err 29.2823, >>> tol 0.002] >>> GMAT_LEO_PropSynchronization_ForwardProp [diff 19.4817, tol >>> 0.0002] >>> GMAT_Molniya_Earth_0_JR_0 [pos err 2.79744, tol 0.002] >>> GMAT_Molniya_Earth_0_MSISE86_0 [pos err 2.23691, tol 0.002] >>> GMAT_Molniya_Earth_0_MSISE90_0 [pos err 2.20992, tol 0.002] >>> GMAT_Molniya_Earth_0_NRLMSISE00_0 [pos err 2.4621, tol 0.0055] >>> GMAT_Molniya_EarthSunLuna_EGM96_JR_SRP [pos err 2.3348, tol >>> 0.002] >>> GMAT_Molniya_EarthSunLuna_EGM96_MSISE90_SRP [pos err 1.82522, >>> tol 0.002] >>> GMAT_Molniya_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide >>> [pos err 1.81953, tol 0.0075] >>> GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP [pos err 2.3348, tol >>> 0.002] >>> GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_ABM [pos err 2.15782, tol >>> 1] >>> GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_Lower_Error_ABM [pos err >>> 2.33475, tol 0.002] >>> GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_PD45 [pos err 2.33481, >>> tol 0.002] >>> GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_PD78 [pos err 2.33478, >>> tol 0.002] >>> GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_PD853 [pos err 2.33479, >>> tol 0.002] >>> GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_RK56 [pos err 2.3349, tol >>> 0.002] >>> GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_RKN68 [pos err 2.33483, >>> tol 0.002] >>> GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_RKV89 [pos err 2.33481, >>> tol 0.002] >>> GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_Target_Error_ABM [pos err >>> 1.47544, tol 0.002] >>> GMAT_Molniya_EarthSunLuna_JGM2_MSISE86_SRP [pos err 1.84755, >>> tol 0.002] >>> GMAT_Molniya_EarthSunLuna_JGM2_MSISE90_SRP [pos err 1.82521, >>> tol 0.002] >>> GMAT_Molniya_EarthSunLuna_JGM2_NRLMSISE00_SRP [pos err 2.02756, >>> tol 0.012] >>> GMAT_Molniya_EarthSunLuna_JGM3_JR_SRP [pos err 2.3348, tol >>> 0.002] >>> GMAT_Molniya_EarthSunLuna_JGM3_MSISE90_SRP [pos err 1.82521, >>> tol 0.002] >>> GMAT_SunSync_Earth_0_JR_0 [GMAT: 720 lines, Truth: 1441 lines] >>> GMAT_SunSync_Earth_0_MSISE86_0 [pos err 30.7809, tol 0.002] >>> GMAT_SunSync_Earth_0_MSISE90_0 [pos err 30.8405, tol 0.002] >>> GMAT_SunSync_Earth_0_NRLMSISE00_0 [pos err 30.9494, tol 0.0065] >>> GMAT_SunSync_EarthSunLuna_EGM96_JR_SRP [pos err 34.0944, tol >>> 0.005] >>> GMAT_SunSync_EarthSunLuna_EGM96_MSISE90_SRP [pos err 33.3515, >>> tol 0.002] >>> GMAT_SunSync_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide >>> [pos err 33.3495, tol 0.002] >>> GMAT_SunSync_EarthSunLuna_JGM2_JR_SRP [pos err 34.0942, tol >>> 0.005] >>> GMAT_SunSync_EarthSunLuna_JGM2_MSISE86_SRP [pos err 33.2939, >>> tol 0.002] >>> GMAT_SunSync_EarthSunLuna_JGM2_MSISE90_SRP [pos err 33.3514, >>> tol 0.002] >>> GMAT_SunSync_EarthSunLuna_JGM2_NRLMSISE00_SRP [pos err 33.4888, >>> tol 0.0065] >>> GMAT_SunSync_EarthSunLuna_JGM3_JR_SRP [pos err 34.0944, tol >>> 0.005] >>> GMAT_SunSync_EarthSunLuna_JGM3_MSISE90_SRP [pos err 33.3516, >>> tol 0.002] >>> GMAT_UserMoon-Titan_AllPlanets_SRP_AboutAsteroid [pos err >>> 0.0135384, tol 0.002] [GMT-5262] >>> Maneuver_BackProp [] [4774] >>> Maneuver_BackProp_5 [] [4774] >>> Mars_B_Plane_Targeting [diff 0.000166714, tol 0.0001] >>> Python_NoInputsOutputs [] >>> Python_NoOutputs [] >>> ScriptEvent_SmokeTests_Ballistic_and_Mass_Case04_LEO [pos err >>> 0.846407, tol 0.001] >>> >>> ScriptEvent_SmokeTests_GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_LargeMaxStep >>> [pos err 0.949464, tol 0.002] >>> ScriptLanguage_Validation_FilePaths_3 [no error or exception] >>> >>> ----------------------------------------------------------------- >>> 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): >>> 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_EclipseLocator_FinalEpoch_SetInMissionSequence [GMT-5171] >>> 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] >>> GMAT_UserMoon-Titan_AllPlanets_SRP_AboutComet [GMT-5262] >>> Maneuver_BackProp_2 [4774] >>> Maneuver_BackProp_3 [4774] >>> Maneuver_BackProp_4 [4774] >>> Maneuver_BackProp_6 [4774] >>> SpacePointParams_CelestialBody_EpochOutput [3939] >>> Thruster_Finite_Burn_Permutations_Separate_Propagators_2 >>> [GMT-3455] >>> >>> >>> 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