The script OrbitView_Validation_UseInitialView works as expected when I load it individually. It correctly checks for error.
***** file: C:\Projects\JazzTestScript\input\Resources\FRR-28_OrbitView\scripts\OrbitView_Validation_UseInitialView.script 1: **** ERROR **** Interpreter Exception: The value of "'DoesNotExist'" for field "UseInitialView" on object "OrbitView1" is not an allowed value The allowed values are case insensitive: [On Off True False] in line: " 10: OrbitView1.UseInitialView = 'DoesNotExist';" Linda -----Original Message----- From: Jun, Linda O. (GSFC-5830) [mailto:[email protected]] Sent: Wednesday, March 26, 2014 10:31 AM To: Parker, Joel J. K. (GSFC-5950); [email protected] Subject: Re: [Gmat-buildtest] Test results: 2014-03-25 (GS580W-GMAT-T4/Win7-64/GMAT-32/M2013a/VS/R2013bInternal) I'll look into: New crashes/hangs/etc.: OrbitView_Validation_UseInitialView Linda -----Original Message----- From: [email protected] [mailto:[email protected]] Sent: Wednesday, March 26, 2014 5:23 AM To: [email protected] Subject: [Gmat-buildtest] Test results: 2014-03-25 (GS580W-GMAT-T4/Win7-64/GMAT-32/M2013a/VS/R2013bInternal) ----------------------------------------------------------------- Summary ----------------------------------------------------------------- System configuration: GS580W-GMAT-T4/Win7-64/GMAT-32/M2013a/VS/R2013bInternal Tested build: 2014-03-25 Regression build: 2014-03-24 Total number of scripts: 10975 (+16 deferred) Percent Passed: 99.48% New issues: 4 Output changes: 3 New truth failures: 0 New crashes: 1 New script errors: 0 New comparator errors: 0 Fixed issues: 1 Total issues: 58 Test system warnings: 14 New deferred issues: 0 Fixed deferred issues: 0 Total deferred issues: 15 Run Time: 14 hours, 09 minutes, 35 seconds ----------------------------------------------------------------- New Issues ----------------------------------------------------------------- New truth failures: None Output changes (but still pass): Ephem_GMAT_Code500_TimeFormats [GMT-4079] Ephem_GMAT_Code500_TimeInteractions Output changes (but still fail): EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection [pos err 15.2522, tol 1e-12] [GMT-4077] New crashes/hangs/etc.: OrbitView_Validation_UseInitialView New script errors: None New comparator errors: None ----------------------------------------------------------------- Fixed Issues ----------------------------------------------------------------- Fixed truth failures: None Fixed crashes/hangs/etc.: None Fixed script errors: MatlabFunction_FunctionPath_Relative Fixed comparator errors: None ----------------------------------------------------------------- All Known Issues ----------------------------------------------------------------- Crashes/hangs/etc.: Measurement_Validation_Disabled OrbitView_Validation_UseInitialView Thruster_Finite_Burn_Permutations_Separate_Propagators_VNB_2 Script errors: AttitudeProp_EulerFile_DOYFormat_EndOfYearLeap Estimate_DeepSpace_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC_Ramp Estimate_DeepSpace_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC Estimate_LEO_PointMass_DSNTwoWayDoppler_LightTimeOnly_NonPerturbedIC Estimate_LEO_PointMass_DSNTwoWayRangeDoppler_LightTimeOnly_NonPerturbedIC_Ramp Estimate_LEO_PointMass_DSNTwoWayRangeDoppler_LightTimeOnly_NonPerturbedIC Estimate_LEO_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC Simulate_DeepSpace_DSNTwoWayDoppler_LightTimeOnly_RampTable Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly Simulate_LEO_DSNTwoWayRange_LightTimeOnly_RampTable Simulate_LEO_DSNTwoWayRange_LightTimeOnly Comparator errors: None Truth failures: Antenna_Validation_Disabled [no error or exception] CInterface_Validation_Disabled [no error or exception] Ephem_GMAT_CCSDS_OEM_86400sec_IterativeProcess_Target_and_DynamicsChange [] Ephem_GMAT_CCSDS_OEM_ForwardProp_BackrProp_Monotonic_time [#1 failed] 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_CCSDS_Forward_and_BackwardDirect [] 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] Estimate_LEO_4x4_USNTwoWayRange_LightTimeOnly_NonPerturbedIC [pos err 0.464918, tol 1e-05] Estimate_LEO_4x4_USNTwoWayRange_LightTimeOnly_PerturbedIC [pos err 0.464698, tol 1e-05] Events_Eclipse_Validation_Disabled [no error or exception] ForceModel_Validation_MarsGRAM2005_F107_Zero [no error or exception] [GMT-4383] KalmanFilter_Validation_Disabled [no error or exception] OrbitRepConv_EarthFixed_Circular_EqPro_Cartesian [max diff 1.44963 > tol 1e-07] OrbitRepConv_EarthFixed_Circular_EqPro_Planetodetic [max diff 1.91272 > tol 1e-07] OrbitRepConv_EarthFixed_Circular_InPro_Cartesian [max diff 0.917615 > tol 1e-07] OrbitRepConv_EarthFixed_Circular_InPro_Planetodetic [max diff 0.432137 > tol 1e-07] OrbitRepConv_EarthFixed_Circular_Polar_Cartesian [max diff 1.07533 > tol 1e-07] OrbitRepConv_EarthFixed_Circular_Polar_Planetodetic [max diff 1.3937 > tol 1e-07] OrbitRepConv_EarthFixed_Elliptic_EqPro_Cartesian [max diff 1.95501 > tol 1e-07] OrbitRepConv_EarthFixed_Elliptic_EqPro_Planetodetic [max diff 0.704638 > tol 1e-07] OrbitRepConv_EarthFixed_Elliptic_InPro_Cartesian [max diff 1.92404 > tol 1e-07] OrbitRepConv_EarthFixed_Elliptic_InPro_Planetodetic [max diff 0.701797 > tol 1e-07] OrbitRepConv_EarthFixed_Elliptic_Polar_Cartesian [max diff 0.998027 > tol 1e-07] OrbitRepConv_EarthFixed_Elliptic_Polar_Planetodetic [max diff 0.518254 > tol 1e-07] OrbitRepConv_EarthFixed_Hyperbolic_EqPro_Cartesian [max diff 5.41837 > tol 1e-07] OrbitRepConv_EarthFixed_Hyperbolic_EqPro_Planetodetic [max diff 0.844197 > tol 1e-07] OrbitRepConv_EarthFixed_Hyperbolic_InPro_Cartesian [max diff 3.38428 > tol 1e-07] OrbitRepConv_EarthFixed_Hyperbolic_InPro_Planetodetic [max diff 0.265127 > tol 1e-07] OrbitRepConv_EarthFixed_Hyperbolic_Polar_Cartesian [max diff 1.03617 > tol 1e-07] OrbitRepConv_EarthFixed_Hyperbolic_Polar_Planetodetic [max diff 0.412936 > tol 1e-07] OrbitRepConv_MarsFixed_Elliptic_InPro_Cartesian [max diff 1.92404 > tol 1e-07] OrbitRepConv_MarsFixed_Elliptic_InPro_Planetodetic [max diff 0.701797 > tol 1e-07] Simulate_LEO_USNTwoWayRange_LightTime-Bias [ Observable Error: 0.02813 m.] Simulate_LEO_USNTwoWayRange_LightTimeOnly [ Observable Error: 0.02813 m.] TrackingSystem_Validation_Disabled [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): Math_Shadowed_Builtins [GMT-3043] ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522] Comparator errors (deferred): None Truth failures (deferred): EphemerisFile_Validation_Code500_FinalEpoch_BeyondEnd [no error or exception] [GMT-4108] 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] 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) CallMatlabFunction_Validation_InvalidInputs_ArrayParam [GMT-3526] Comet_Validation_OrientationEpoch_3 [GMT-3252] CoordSysTest_Luna_MJ2000Eq_To_ICRF [GMT-3227] CoordinateSystem_Validation_Axes_4 [GMT-3155] EphemPropagator_SatAssigmentToNewSatThenProp [GMT-3434] Ephem_GMAT_Code500_TimeFormats [GMT-4079] 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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Download your free book today! http://p.sf.net/sfu/13534_NeoTech _______________________________________________ Gmat-buildtest mailing list [email protected] https://lists.sourceforge.net/lists/listinfo/gmat-buildtest ------------------------------------------------------------------------------ Learn Graph Databases - Download FREE O'Reilly Book "Graph Databases" is the definitive new guide to graph databases and their applications. Written by three acclaimed leaders in the field, this first edition is now available. Download your free book today! http://p.sf.net/sfu/13534_NeoTech _______________________________________________ Gmat-buildtest mailing list [email protected] https://lists.sourceforge.net/lists/listinfo/gmat-buildtest
