Truth failure for CoordinateSystem_Validation_OriginAxesCoupling_BodyFixed:
I fixed GMT-3852 - so now Spacecraft are allowed as origin for BodyFixed CSs.
Wendy
On Nov 1, 2013, at 12:14 AM, [email protected] wrote:
> -----------------------------------------------------------------
> Summary
> -----------------------------------------------------------------
> System configuration:
> GS580W-GMAT-T4/Win7-64/GMAT-32/M2013a/VS/R2013bInternal
> Tested build: 2013-10-31
> Regression build: 2013-10-30
>
> Total number of scripts: 10744 (+17 deferred)
> Percent Passed: 99.74%
> New issues: 2
> Output changes: 1
> New truth failures: 1
> New crashes: 0
> New script errors: 0
> New comparator errors: 0
> Fixed issues: 4
> Total issues: 47
>
> Test system warnings: 11
> New deferred issues: 0
> Fixed deferred issues: 0
> Total deferred issues: 17
>
> Run Time: 09 hours, 07 minutes, 24 seconds
>
> -----------------------------------------------------------------
> New Issues
> -----------------------------------------------------------------
> New truth failures:
> CoordinateSystem_Validation_OriginAxesCoupling_BodyFixed [no error or
> exception]
>
> Output changes (but still pass):
> None
>
> Output changes (but still fail):
>
> EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection
> [pos err 9.57663, tol 1e-12] [GMT-4077]
>
> New crashes/hangs/etc.:
> None
>
> New script errors:
> None
>
> New comparator errors:
> None
>
> -----------------------------------------------------------------
> Fixed Issues
> -----------------------------------------------------------------
> Fixed truth failures:
> fmincon_ShowProgress
>
> Fixed crashes/hangs/etc.:
> None
>
> Fixed script errors:
> BurnParams_Local_SpacecraftBody
> Spacecraft_AttitudeProp_CoordSysFixed_ObjRef_Mars
> Spacecraft_AttitudeProp_CoordSysFixed_ObjRef_Moon
>
> Fixed comparator errors:
> None
>
> -----------------------------------------------------------------
> All Known Issues
> -----------------------------------------------------------------
> Crashes/hangs/etc.:
> None
>
> Script errors:
> OrbitRepConv_EarthMJ2000Eq_Circular_EqPro_Cartesian_MS [GMT-4172]
> Simulate_LEO_USNTwoWayRange_LightTime-Bias
> Simulate_LEO_USNTwoWayRange_LightTimeOnly
>
> Comparator errors:
> None
>
> Truth failures:
> CoordinateSystem_Validation_OriginAxesCoupling_BodyFixed [no error or
> exception]
>
> Ephem_GMAT_CCSDS_OEM_86400sec_IterativeProcess_Target_and_DynamicsChange []
> Ephem_GMAT_Code500_60sec [pos err 4.00875e-06, tol 1e-12] [GMT-4112]
> Ephem_GMAT_Code500_ACE_OpsPrototype_v13 [pos err 0.000112799, tol 1e-12]
> [GMT-4112]
>
> Ephem_GMAT_Code500_CoordinateSystem/Ephem_GMAT_Code500_CoordinateSystem_MarsMJ2000Eq.eph
> [pos err 0.00102592, tol 1e-12] [GMT-4112]
>
> Ephem_GMAT_Code500_CoordinateSystem/Ephem_GMAT_Code500_CoordinateSystem_LunaMJ2000Eq.eph
> [pos err 0.000165046, tol 1e-12] [GMT-4112]
>
> Ephem_GMAT_Code500_CoordinateSystem/Ephem_GMAT_Code500_CoordinateSystem_SunMJ2000Eq.eph
> [pos err 0.000747626, tol 1e-12] [GMT-4112]
>
> Ephem_GMAT_Code500_InterpolationOrder/Ephem_GMAT_Code500_InterpolationOrder_1.eph
> [pos err 0.0177967, tol 1e-12] [GMT-4075, GMT-4112]
>
> Ephem_GMAT_Code500_InterpolationOrder/Ephem_GMAT_Code500_InterpolationOrder_3.eph
> [pos err 0.0463976, tol 1e-12] [GMT-4075, GMT-4112]
>
> Ephem_GMAT_Code500_InterpolationOrder/Ephem_GMAT_Code500_InterpolationOrder_6.eph
> [pos err 0.000162117, tol 1e-12] [GMT-4075, GMT-4112]
>
> Ephem_GMAT_Code500_InterpolationOrder/Ephem_GMAT_Code500_InterpolationOrder_10.eph
> [pos err 0.000153289, tol 1e-12] [GMT-4075, GMT-4112]
> Ephem_GMAT_Code500_ManeuverAtEnd [pos err 1.21288e-05, tol 1e-12]
> [GMT-4112]
>
> Ephem_GMAT_Code500_OutputFormat/Ephem_GMAT_Code500_OutputFormat_Default.eph
> [pos err 0.000153203, tol 1e-12] [GMT-4112]
> Ephem_GMAT_Code500_OutputFormat/Ephem_GMAT_Code500_OutputFormat_PC.eph
> [pos err 0.000153203, tol 1e-12] [GMT-4112]
>
> Ephem_GMAT_Code500_OutputFormat/Ephem_GMAT_Code500_OutputFormat_UNIX.eph [pos
> err 0.000153203, tol 1e-12] [GMT-4112]
> Ephem_GMAT_Code500_StepSize/Ephem_GMAT_Code500_StepSize_1.eph [pos err
> 305.165, tol 1e-12] [GMT-4112]
> Ephem_GMAT_Code500_StepSize/Ephem_GMAT_Code500_StepSize_30.eph [pos err
> 0.000154166, tol 1e-12] [GMT-4112]
> Ephem_GMAT_Code500_StepSize/Ephem_GMAT_Code500_StepSize_1073.eph [pos
> err 0.00605499, tol 1e-12] [GMT-4112]
> Ephem_GMAT_Code500_StepSize/Ephem_GMAT_Code500_StepSize_14400.eph [pos
> err 0.00010996, tol 1e-12] [GMT-4112]
>
> Ephem_GMAT_Code500_TimeFormats/Ephem_GMAT_Code500_TimeFormats_UTCGregorian.eph
> [pos err 0.000153096, tol 1e-12] [GMT-4079, GMT-4112]
>
> Ephem_GMAT_Code500_TimeFormats/Ephem_GMAT_Code500_TimeFormats_UTCModJulian.eph
> [pos err 0.000153096, tol 1e-12] [GMT-4079, GMT-4112]
>
> Ephem_GMAT_Code500_TimeFormats/Ephem_GMAT_Code500_TimeFormats_TAIGregorian.eph
> [pos err 0.000153096, tol 1e-12] [GMT-4079, GMT-4112]
>
> Ephem_GMAT_Code500_TimeFormats/Ephem_GMAT_Code500_TimeFormats_TAIModJulian.eph
> [pos err 0.000153096, tol 1e-12] [GMT-4079, GMT-4112]
>
> Ephem_GMAT_Code500_TimeFormats/Ephem_GMAT_Code500_TimeFormats_TTGregorian.eph
> [pos err 0.000153096, tol 1e-12] [GMT-4079, GMT-4112]
>
> Ephem_GMAT_Code500_TimeFormats/Ephem_GMAT_Code500_TimeFormats_TTModJulian.eph
> [pos err 0.000153096, tol 1e-12] [GMT-4079, GMT-4112]
>
> Ephem_GMAT_Code500_TimeFormats/Ephem_GMAT_Code500_TimeFormats_A1Gregorian.eph
> [pos err 0.00306041, tol 1e-12] [GMT-4079, GMT-4112]
>
> Ephem_GMAT_Code500_TimeFormats/Ephem_GMAT_Code500_TimeFormats_A1ModJulian.eph
> [pos err 0.000153096, tol 1e-12] [GMT-4079, GMT-4112]
>
> Ephem_GMAT_Code500_TimeInteractions/Ephem_GMAT_Code500_TimeInteractions_FinalHigh_StepPos_PropFwd.eph
> [pos err 0.000153096, tol 1e-12] [GMT-4112]
>
> Ephem_GMAT_Code500_TimeInteractions/Ephem_GMAT_Code500_TimeInteractions_FinalAutoHigh_StepPos_PropFwd.eph
> [pos err 0.000153096, tol 1e-12] [GMT-4112]
>
> Ephem_GMAT_Code500_TimeInteractions/Ephem_GMAT_Code500_TimeInteractions_FinalHigh_InitialAuto_StepPos_PropFwd.eph
> [pos err 0.000153096, tol 1e-12] [GMT-4112]
> Ephem_GMAT_Code500_Toggle [pos err 0.000153096, tol 1e-12] [GMT-4112]
> Ephem_GMAT_Code500_WriteEphemeris [pos err 0.000153203, tol 1e-12]
> [GMT-4112]
> EphemerisFile_Validation_Code500_FinalEpoch_BeyondEnd [no error or
> exception] [GMT-4108]
>
> EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection
> [pos err 15.2475, 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 14.1908, tol 1e-12] [GMT-4077]
>
> EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
> [pos err 0.000195242, tol 1e-12] [GMT-4112]
> EphemStressTests_PD78_ABM_Prop_Code500_60Sec_Step_ForwardDirection [pos
> err 21.5633, tol 1e-12] [GMT-4112]
> EphemStressTests_SPK_Integrator_Code500_60Sec_ForwardDirection [pos err
> 0.000427977, tol 1e-12] [GMT-4112]
> GMAT_Mars1_Mars_0_MarsGRAM2005_0 [pos err 0.00125082, tol 1e-12]
> OrbitRepConv_MarsFixed_Elliptic_IncPro_ModifiedEquinoctial [max diff
> 0.836111 > tol 1e-08] [GMT-4175]
> Spacecraft_AttitudeProp_CoordSysFixed_ObjRef_Mars []
> Spacecraft_AttitudeProp_CoordSysFixed_ObjRef_Moon []
> Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [diff. num.
> lines] [GMT-3455]
>
> -----------------------------------------------------------------
> 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):
> Math_LHS_Param_Array [GMT-3944]
> Math_RHS_Param_Array [GMT-3944]
> Math_Shadowed_Builtins [GMT-3043]
> ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522]
>
> Comparator errors (deferred):
> None
>
> Truth failures (deferred):
> CallMatlabFunction_Validation_InvalidInputs_ArrayParam [no error or
> exception] [GMT-3526]
> 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 0.000813214, tol
> 1e-06] [GMT-2567]
> Math_Inf [GMAT: 53 lines, Truth: 69 lines] [GMT-3195]
> 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]
>
> -----------------------------------------------------------------
> 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]
> 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]
>
>
> ------------------------------------------------------------------------------
> Android is increasing in popularity, but the open development platform that
> developers love is also attractive to malware creators. Download this white
> paper to learn more about secure code signing practices that can help keep
> Android apps secure.
> http://pubads.g.doubleclick.net/gampad/clk?id=65839951&iu=/4140/ostg.clktrk
> _______________________________________________
> Gmat-buildtest mailing list
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> https://lists.sourceforge.net/lists/listinfo/gmat-buildtest
=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=
Until he extends his circle of compassion to
all living things, man himself will not find
peace. - Albert Schweitzer
=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=
Views expressed are my own and do not necessarily
reflect those of my employer, or anyone else.
=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=
Wendy C. Shoan 301.286.6263
NASA/GSFC/GSSB/583 Greenbelt MD 20771
[email protected]
=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=
------------------------------------------------------------------------------
Android is increasing in popularity, but the open development platform that
developers love is also attractive to malware creators. Download this white
paper to learn more about secure code signing practices that can help keep
Android apps secure.
http://pubads.g.doubleclick.net/gampad/clk?id=65839951&iu=/4140/ostg.clktrk
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