-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: GS580W-GMAT-T4/Win7-64/GMAT-32/M2013a/VS2010
Tested build: 2015-04-08
Regression build: 2015-04-06
Total number of scripts: 12072 (+129 deferred)
Percent Passed: 98.88%
New issues: 2
Output changes: 2
New truth failures: 0
New crashes: 0
New script errors: 0
New comparator errors: 0
Fixed issues: 1
Total issues: 135
Test system warnings: 15
New deferred issues: 2
Fixed deferred issues: 0
Total deferred issues: 120
Run Time: 16 hours, 07 minutes, 51 seconds
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
None
Output changes (but still pass):
Ephem_GMAT_Code500_60sec
Ephem_GMAT_Code500_WriteEphemeris
Output changes (but still fail):
None
New crashes/hangs/etc.:
None
New script errors:
None
New comparator errors:
None
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
None
Fixed crashes/hangs/etc.:
ReportFileStressTests_Default_and_ABM_Integrator_CCSDS_60Sec_MultipleSCs_ForwardDirection
Fixed script errors:
None
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
None
Script errors:
All_in_One_STEREO
BatchEstimator_InversionAlgorithm_2
BatchEstimator_InversionAlgorithm_3
BatchEstimator_InversionAlgorithm
BatchEstimator_Nominal_Geosynchronous_RangeDoppler
BatchEstimator_Nominal_Heliocentric_RangeDoppler
BatchEstimator_Nominal_L1_Range
BatchEstimator_Nominal_L2_Range
BatchEstimator_Nominal_Lunar_RangeDoppler
BatchEstimator_OLSEInitialRMSSigma_Doppler
BatchEstimator_OLSEInitialRMSSigma_Range
BatchEstimator_Propagator_Simulate_Earth8x8
BatchEstimator_Propagator_Simulate_EarthFull
BatchEstimator_Propagator_Simulate_EarthPtMass_Drag
BatchEstimator_Propagator_Simulate_EarthPtMass_SRP_Drag
BatchEstimator_Propagator_Simulate_EarthPtMass_SRP
BatchEstimator_Propagator_Simulate_EarthPtMass
BatchEstimator_Propagator_Simulate_Sun_EM_AllPlanets_SRP_GR
BatchEstimator_Propagator_Simulate_Sun_EM_AllPlanets
BatchEstimator_Propagator_Simulate_Sun_EM_GR
BatchEstimator_Propagator_Simulate_Sun_EM
BatchEstimator_Propagator_Simulate_Sun_SRP
BatchEstimator_Propagator_Simulate_Sun
BatchEstimator_Propagator
BatchEstimator_ReportStyle_Concise
BatchEstimator_ReportStyle_Debug
BatchEstimator_ReportStyle_Normal
BatchEstimator_ReportStyle_Verbose
Estimate_LEO_PointMass_USNTwoWayRange_LightTimeOnly_NonPerturbedIC
Estimate_LEO_PointMass_USNTwoWayRange_LightTimeOnly_PerturbedIC
Events_ContactLocator_Simple
Events_EclipseLocator_Simple
GS_Nav_DeepSpace_DSN_Media
Old_All_in_One_STEREO
Old_All_in_One
Old_Estimate_DeepSpace_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC_Ramp
Old_Estimate_DeepSpace_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC
Old_Estimate_LEO_PointMass_DSNTwoWayDoppler_LightTimeOnly_NonPerturbedIC
Old_Estimate_LEO_PointMass_DSNTwoWayRangeDoppler_LightTimeOnly_NonPerturbedIC_Ramp
Old_Estimate_LEO_PointMass_DSNTwoWayRangeDoppler_LightTimeOnly_NonPerturbedIC
Old_Estimate_LEO_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC
Old_Simulate_DeepSpace_DSNTwoWayDoppler_LightTimeOnly_RampTable
Old_Simulate_DeepSpace_DSNTwoWayRange_LT_GR_Transponder_RampTable
Old_Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_GR_RampTable
Old_Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable_2
Old_Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable
Old_Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly
Old_Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly_Ramp
Old_Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly_Zero_Ramp
Old_Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly
Old_Simulate_LEO_DSNTwoWayRange_LightTimeOnly_RampTable
Old_Simulate_LEO_DSNTwoWayRange_LightTimeOnly
ScriptEvent_SmokeTests_Events_Eclipse_Simple
Simulate_DeepSpace_DSNTwoWayRange_LT_GR_Transponder_RampTable
Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_GR_RampTable
Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable_2
Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly
Thruster_OtherNumericProperties_Cmd
TrkFile_Est_DSN_DS_Range_Ramp
TrkFile_Est_DSN_DS_Range
TrkFile_Est_DSN_LEO_Doppler
TrkFile_Est_DSN_LEO_RangeDoppler_Ramp
TrkFile_Est_DSN_LEO_RangeDoppler
TrkFile_Est_DSN_LEO_Range
TrkFile_SimEst_DSN_DS
TrkFile_SimEst_DSN_LEO
TrkFile_Sim_DSN_DeepSpace_Doppler_Ramp
TrkFile_Sim_DSN_DeepSpace_Range_GR_Ramp
TrkFile_Sim_DSN_DeepSpace_Range_GR_Transpon_Ramp
TrkFile_Sim_DSN_DeepSpace_Range_Ramp_2
TrkFile_Sim_DSN_DeepSpace_Range_Ramp
TrkFile_Sim_DSN_DeepSpace_Range
TrkFile_Sim_DSN_LEO_Doppler_Ramp_2
TrkFile_Sim_DSN_LEO_Doppler_Ramp
TrkFile_Sim_DSN_LEO_Doppler
TrkFile_Sim_DSN_LEO_Range_Ramp
TrkFile_Sim_DSN_LEO_Range
Comparator errors:
None
Truth failures:
BatchEstimator_AddSolveFor_CartesianState [#1 failed]
BatchEstimator_AddSolveFor_CartesianState_DopplerBias [#1 failed]
BatchEstimator_AddSolveFor_CartesianState_DopplerBias2 [#1 failed]
BatchEstimator_AddSolveFor_CartesianState_DopplerBias3 [#1 failed]
BatchEstimator_AddSolveFor_CartesianState_RangeBias [#1 failed]
BatchEstimator_AddSolveFor_CartesianState_RangeBias2 [#1 failed]
BatchEstimator_AddSolveFor_CartesianState_RangeBias2_DopplerBias2 [#1
failed]
BatchEstimator_AddSolveFor_CartesianState_RangeBias3 [#1 failed]
BatchEstimator_AddSolveFor_CartesianState_RangeBias3_DopplerBias3 [#1
failed]
BatchEstimator_AddSolveFor_CartesianState_RangeBias_DopplerBias [#1
failed]
BatchEstimator_InversionAlgorithm_NotEnoughData [ptrn 1,2 failed]
BatchEstimator_InversionAlgorithm_NotEnoughData_2 [ptrn 1,2 failed]
BatchEstimator_InversionAlgorithm_NotEnoughData_3 [ptrn 1,2 failed]
BatchEstimator_InversionAlgorithm_Singular [#1 failed]
BatchEstimator_InversionAlgorithm_Singular_2 [#1 failed]
BatchEstimator_InversionAlgorithm_Singular_3 [#1 failed]
BatchEstimator_MaxConsecutiveDivergences [ptrn 1,2 failed]
BatchEstimator_Measurements [#1 failed]
BatchEstimator_Measurements2 [#1 failed]
BatchEstimator_Measurements3 [#1 failed]
BatchEstimator_OLSE_NoDataEdited_AllIterations [#1 failed]
BatchEstimator_OLSE_NoDataEdited_FirstIteration [#1 failed]
BatchEstimator_OLSEAdditiveConstant_Doppler [#1 failed]
BatchEstimator_OLSEAdditiveConstant_Range [#1 failed]
BatchEstimator_OLSEMultiplicativeConstant_Doppler [#1 failed]
BatchEstimator_OLSEMultiplicativeConstant_Range [#1 failed]
BatchEstimator_Validation_AddSolveFor [#1 failed]
BatchEstimator_Validation_Measurements [#1 failed]
BatchEstimator_Validation_Mode [#1 failed]
BatchEstimator_Validation_ReportFile [#1 failed]
EphemPropagator_Origin_Earth_HST_5MinStepSize [pos err 0.517881, tol
0.01]
EphemPropagator_Origin_Earth_HST_TestExtraStep [pos err 0.515198, tol
0.01]
EphemPropagator_PropAssigmentToNewPropThenProp [pos err 0.517881, tol
0.01]
EphemPropagator_PropDifferentSpacecraft [pos err 0.454003, tol 1e-07]
EphemPropagator_SatAssigmentToNewSatThenProp [pos err 0.517881, tol
0.01] [GMT-3434]
EphemPropagator_StartEpoch_A1Gregorian [pos err 81.8951, tol 0.001]
EphemPropagator_StartEpoch_A1ModJulian [pos err 81.8952, tol 0.001]
EphemPropagator_StartEpoch_FromSpacecraft [pos err 81.8952, tol 0.001]
EphemPropagator_StartEpoch_TAIGregorian [pos err 81.8952, tol 0.001]
EphemPropagator_StartEpoch_TAIModJulian [pos err 81.8952, tol 0.001]
EphemPropagator_StartEpoch_TDBGregorian [pos err 81.8954, tol 0.001]
EphemPropagator_StartEpoch_TDBModJulian [pos err 81.8952, tol 0.001]
EphemPropagator_StartEpoch_TTGregorian [pos err 81.8952, tol 0.001]
EphemPropagator_StartEpoch_TTModJulian [pos err 81.8952, tol 0.001]
EphemPropagator_StartEpoch_UTCGregorian [pos err 81.8952, tol 0.001]
EphemPropagator_StartEpoch_UTCModJulian [pos err 81.8952, tol 0.001]
EphemPropagator_StepSize_1day [pos err 0.504113, tol 0.001]
EphemPropagator_StepSize_1day_ForLoop [pos err 0.504113, tol 0.001]
EphemPropagator_StepSize_1hour [pos err 0.492245, tol 0.001]
EphemPropagator_StepSize_1hour_ForLoop [pos err 0.492245, tol 0.001]
EphemPropagator_StepSize_2minutes [pos err 0.491893, tol 0.001]
EphemPropagator_StepSize_2minutes_ForLoop [pos err 0.491893, tol 0.001]
GMAT_UserMoon-Titan_AllPlanets_SRP_AboutAsteroid [pos err 5569.14, tol
0.002]
GMAT_UserMoon-Titan_AllPlanets_SRP_AboutComet [pos err 5569.14, tol
0.002]
Maneuver_BackProp [] [4774]
Maneuver_BackProp_2 [] [4774]
ScriptLanguage_Validation_FilePaths_3 [no error or exception]
TargeterNesting [max diff 2.26405e-07 > tol 1e-07]
-----------------------------------------------------------------
New Issues (Deferred)
-----------------------------------------------------------------
New truth failures (deferred):
None
Output changes (but still pass) (deferred):
None
Output changes (but still fail) (deferred):
Ephem_GMAT_Code500_ACE_OpsPrototype_v13 [pos err 1.36904, tol 1]
[GMT-4112]
EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection
[pos err 15.2522, tol 1e-12] [GMT-4077]
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):
All_in_One
Estimate_DeepSpace_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC_Ramp
Estimate_DeepSpace_PointMass_DSNTwoWayRange_LightTimeOnly_NonPerturbedIC
Estimate_LEO_4x4_USNTwoWayRange_LightTimeOnly_NonPerturbedIC
Estimate_LEO_4x4_USNTwoWayRange_LightTimeOnly_PerturbedIC
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
Ex_GmatFunction [GMT-3604]
Ex_Integrators
GMATFunction_ArrayIO
GMATFunction_EarthFixedPropFun_Periapsis
GMATFunction_EarthFixedPropFun
GMATFunction_FunInFun_Global
GMATFunction_FunInFun
GMATFunction_GlobalSC
GMATFunction_LiteralInput
GMATFunction_MJ2000EcPropFun_Apoapsis
GMATFunction_MJ2000EcProp
GMATFunction_MJ2000EqPropFun_Apoapsis
GMATFunction_MJ2000EqProp
GMATFunction_NoFunOutput
GMATFunction_NoIO_EditSC
GMATFunction_NoInput
GMATFunction_PassAndPropSC
GMATFunction_PassSC_NoFunOutput
GMATFunction_PlotFun
GMATFunction_Recursive
GMATFunction_SCIO_wprop
GMATFunction_SCIO
GMATFunction_SearchFunPath
GMATFunction_StringIO
GMATFunction_TwoFunOneFile
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
Math_Math_GmatFunction
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]
Simulate_DeepSpace_DSNTwoWayDoppler_LightTimeOnly_RampTable
Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable
Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly_Ramp
Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly_Zero_Ramp
Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly
Simulate_LEO_DSNTwoWayRange_LightTimeOnly_RampTable
Simulate_LEO_DSNTwoWayRange_LightTimeOnly
Simulate_LEO_USNTwoWayRange_LightTime-Bias
Simulate_LEO_USNTwoWayRange_LightTimeOnly
Target_DC_Command_GMATFunction
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]
BatchEstimator_AbsoluteTol [ptrn 1 failed]
BatchEstimator_MaximumIterations [ptrn 1,2 failed]
BatchEstimator_RelativeTol [ptrn 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_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]
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]
Maneuver_BackProp_3 [4774]
Maneuver_BackProp_4 [4774]
Maneuver_BackProp_5 [4774]
Maneuver_BackProp_6 [4774]
SpacePointParams_CelestialBody_EpochOutput [3939]
Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
------------------------------------------------------------------------------
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