Attached is a full run with spacecraft precision time.
Was it built with the internal plugins (I see matlab and python errors)?
Anyway, lots of errors.
-----Original Message-----
From: Cooley, D S. (GSFC-5950)
Sent: Thursday, November 1, 2018 4:06 PM
To: 'John McGreevy' <[email protected]>
Subject: RE: Spacecraft precision time build
Thanks. Just kicked off a run
-----Original Message-----
From: John McGreevy <[email protected]>
Sent: Thursday, November 1, 2018 3:40 PM
To: Cooley, D S. (GSFC-5950) <[email protected]>
Subject: Spacecraft precision time build
The build is located here:
\\mesa-file\595\GMAT\Builds\DevSnapShots\GMAT-SpacecraftTime-x64
-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Windows 10/MATLAB R2017b/TestBuild
Tested build: GMAT_Time_11_01
Regression build: $prevbuild$
Total number of scripts: 13855 (+51 deferred)
Percent Passed: 98.50%
New issues: 0
Output changes: 0
New truth failures: 0
New crashes: 0
New script errors: 0
New comparator errors: 0
Fixed issues: 0
Total issues: 214
Test system warnings: 40
New deferred issues: 0
Fixed deferred issues: 0
Total deferred issues: 39
Run Time: 14 hours, 01 minutes, 59 seconds
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
None
Output changes (but still pass):
None
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.:
None
Fixed script errors:
None
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
Tut_MultipleShootingTutorial_Step4
Tut_MultipleShootingTutorial_Step5
Script errors:
GmatFunction_SystemTime_TimeAccuracy:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\GmatFunction_SystemTime_TimeAccuracy.report
does not exist
Optimize_fmincon_ExitMode_DiscardAndContinue_2:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_ExitMode_DiscardAndContinue_2.report
does not exist
Optimize_fmincon_ExitMode_DiscardAndContinue_3:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_ExitMode_DiscardAndContinue_3.report
does not exist
Optimize_fmincon_ExitMode_DiscardAndContinue:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_ExitMode_DiscardAndContinue.report
does not exist
Optimize_fmincon_ExitMode_SaveAndContinue_2:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_ExitMode_SaveAndContinue_2.report
does not exist
Optimize_fmincon_ExitMode_SaveAndContinue_3:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_ExitMode_SaveAndContinue_3.report
does not exist
Optimize_fmincon_ExitMode_SaveAndContinue:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_ExitMode_SaveAndContinue.report
does not exist
Optimize_fmincon_ExitMode_Stop:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_ExitMode_Stop.report
does not exist
Optimize_fmincon_Minimize_Height_on_circle_1:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_Minimize_Height_on_circle_1.report
does not exist
Optimize_fmincon_Minimize_Height_on_circle_2:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_Minimize_Height_on_circle_2.report
does not exist
Optimize_fmincon_Minimize_Height_on_circle_3:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_Minimize_Height_on_circle_3.report
does not exist
Optimize_fmincon_Minimize_Height_on_circle_4:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_Minimize_Height_on_circle_4.report
does not exist
Optimize_fmincon_Minimize_Height_on_circle:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_Minimize_Height_on_circle.report
does not exist
Optimize_fmincon_SolveMode_Defaultscript:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_SolveMode_Defaultscript.report
does not exist
Optimize_fmincon_SolveMode_RunInitialGuess:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_SolveMode_RunInitialGuess.report
does not exist
Optimize_fmincon_SolveMode_Solve:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_SolveMode_Solve.report
does not exist
Optimize_fmincon_cvg_status:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Optimize_fmincon_cvg_status_Report2.report
does not exist
PythonArray2dReturn:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\PythonArray2dReturn.report
does not exist
PythonArrayReal:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\PythonArrayReal.report
does not exist
PythonFunction_Builtin:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\PythonFunction_Builtin.report
does not exist
PythonFunction_Custom_DegToRad_Assignment:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\PythonFunction_Custom_DegToRad_Assignment.report
does not exist
PythonFunction_Custom_DegToRad:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\PythonFunction_Custom_DegToRad.report
does not exist
PythonFunction_Custom_magic:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\PythonFunction_Custom_magic.report
does not exist
PythonFunction_Custom:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\PythonFunction_Custom.report
does not exist
PythonRealArrayReal:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\PythonRealArrayReal.report
does not exist
PythonReal:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\PythonReal.report
does not exist
PythonStringArrayArrayOp:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\PythonStringArrayArrayOp.report
does not exist
PythonStringArrayArray:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\PythonStringArrayArray.report
does not exist
PythonStringRealRealOp:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\PythonStringRealRealOp.report
does not exist
PythonStringRealReal:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\PythonStringRealReal.report
does not exist
PythonStringToString:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\PythonStringToString.report
does not exist
Python_NoInputs:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Python_NoInputs.report
does not exist
ScriptEvent_SmokeTests_fmincon_ConstraintTolerance:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\ScriptEvent_SmokeTests_fmincon_ConstraintTolerance.report
does not exist
SpacePointParams_CelestialBody_CartesianParams_DefaultDependency:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\SpacePointParams_CelestialBody_CartesianParams_DefaultDependency.report
does not exist
SpacePointParams_CelestialBody_CartesianParams:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\SpacePointParams_CelestialBody_CartesianParams.report
does not exist
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2.report
does not exist
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Vary_optimizer_fmincon_InitialGuess_ForLoopVariable.report
does not exist
Vary_optimizer_fmincon_Perturbation_ArrayElement:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Vary_optimizer_fmincon_Perturbation_ArrayElement.report
does not exist
Vary_optimizer_fmincon_Perturbation_RealNumber:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Vary_optimizer_fmincon_Perturbation_RealNumber.report
does not exist
Vary_optimizer_fmincon_Perturbation_Variable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Vary_optimizer_fmincon_Perturbation_Variable.report
does not exist
Vary_optimizer_fmincon_UpperBound_ArrayElement:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Vary_optimizer_fmincon_UpperBound_ArrayElement.report
does not exist
Vary_optimizer_fmincon_UpperBound_Variable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Vary_optimizer_fmincon_UpperBound_Variable.report
does not exist
Vary_optimizer_fmincon__InitialValue_Array:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Vary_optimizer_fmincon__InitialValue_Array.report
does not exist
Vary_optimizer_fmincon__InitialValue_RealNumber:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Vary_optimizer_fmincon__InitialValue_RealNumber.report
does not exist
Vary_optimizer_fmincon__InitialValue_Variable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Vary_optimizer_fmincon__InitialValue_Variable.report
does not exist
Vary_optimizer_fmincon__LowerBound_Array:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Vary_optimizer_fmincon__LowerBound_Array.report
does not exist
Vary_optimizer_fmincon__LowerBound_RealNumber:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Vary_optimizer_fmincon__LowerBound_RealNumber.report
does not exist
Vary_optimizer_fmincon__LowerBound_Variable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\Vary_optimizer_fmincon__LowerBound_Variable.report
does not exist
completed_steps_1_thru_10_of_FRC_1_using_fmincon_Optimizer:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\completed_steps_1_thru_10_of_FRC_1_using_fmincon_Optimizer.report
does not exist
fmincon_ConstraintTolerance:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\fmincon_ConstraintTolerance.report
does not exist
fmincon_ShowProgress:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\FminconOptimizerSQPfmincon.data
does not exist
scriptEvent_optimizer_fmincon__InitialValue_Array:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\scriptEvent_optimizer_fmincon__InitialValue_Array.report
does not exist
scriptEvent_optimizer_fmincon__InitialValue_RealNumber:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\scriptEvent_optimizer_fmincon__InitialValue_RealNumber.report
does not exist
scriptEvent_optimizer_fmincon__InitialValue_Variable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-SpacecraftTime-x64\output\scriptEvent_optimizer_fmincon__InitialValue_Variable.report
does not exist
Comparator errors:
None
Truth failures:
Barycenter_DE405SSB_JupiterOrbit [vel err 1.85376e-08, tol 1e-08]
Barycenter_DE405SSB_MercuryOrbit [vel err 2.3067e-08, tol 1e-08]
Barycenter_DE405SSB_PlutoOrbit [vel err 1.33338e-08, tol 1e-08]
Barycenter_DE405SSB_UranusOrbit [vel err 1.21043e-08, tol 1e-08]
Barycenter_DE405SSB_VenusOrbit [vel err 1.89642e-08, tol 1e-08]
Barycenter_DE421_AllPlanets_Jupiter_Orbit [vel err 1.94844e-08, tol
1e-08]
Barycenter_DE421_AllPlanets_Mercury_Orbit [vel err 2.3324e-08, tol
1e-08]
Barycenter_DE421_AllPlanets_Pluto_Orbit [vel err 2.21294e-08, tol 1e-08]
Barycenter_DE421_AllPlanets_Uranus_Orbit [vel err 1.33484e-08, tol
1e-08]
Barycenter_DE421_AllPlanets_Venus_Orbit [vel err 1.92074e-08, tol 1e-08]
Barycenter_DE421SSB_JupiterOrbit [vel err 1.9485e-08, tol 1e-08]
Barycenter_DE421SSB_MercuryOrbit [vel err 2.33241e-08, tol 1e-08]
Barycenter_DE421SSB_PlutoOrbit [vel err 2.21286e-08, tol 1e-08]
Barycenter_DE421SSB_UranusOrbit [vel err 1.33489e-08, tol 1e-08]
Barycenter_DE421SSB_VenusOrbit [vel err 1.92065e-08, tol 1e-08]
Barycenter_DE424_AllPlanets_Jupiter_Orbit [vel err 1.90662e-08, tol
1e-08]
Barycenter_DE424_AllPlanets_Mercury_Orbit [vel err 2.28919e-08, tol
1e-08]
Barycenter_DE424_AllPlanets_Pluto_Orbit [vel err 1.86769e-08, tol 1e-08]
Barycenter_DE424_AllPlanets_Uranus_Orbit [vel err 1.3608e-08, tol 1e-08]
Barycenter_DE424_AllPlanets_Venus_Orbit [vel err 1.92036e-08, tol 1e-08]
Barycenter_DE424SSB_JupiterOrbit [vel err 1.90665e-08, tol 1e-08]
Barycenter_DE424SSB_MercuryOrbit [vel err 2.28914e-08, tol 1e-08]
Barycenter_DE424SSB_PlutoOrbit [vel err 1.86772e-08, tol 1e-08]
Barycenter_DE424SSB_UranusOrbit [vel err 1.36083e-08, tol 1e-08]
Barycenter_DE424SSB_VenusOrbit [vel err 1.92031e-08, tol 1e-08]
BatchEstimator_ReportFile_MeasurementStatistics [#15 failed]
BatchEstimator_ReportFile_MeasurementStatistics_UserEdit_AcceptFilter_TimeSpan
[#5 failed]
BatchEstimator_ReportFile_MeasurementStatistics_UserEdit_DataType [#5
failed]
BatchEstimator_ReportFile_MeasurementStatistics_UserEdit_TimeSpan [#5
failed]
BatchEstimator_ReportFile_MeasurementStatistics_UserEdit_Tracker [#6
failed]
BatchEstimator_ReportFile_MeasurementStatistics_UserEdit_TrackerDataType [#5
failed]
BatchEstimator_ReportFile_StateInformation [#4 failed]
CbParams_Mars1_2Body_Earth/CbParams_Mars1_2Body_Earth_BetaAngle.report
[max diff 5.24686e-06 > tol 1e-13]
CbParams_Mars1_2Body_Mars/CbParams_Mars1_2Body_Mars_BetaAngle.report
[max diff 9.85698e-10 > tol 1e-13]
CbParams_Mars1_2Body_Moon/CbParams_Mars1_2Body_Moon_BetaAngle.report
[max diff 4.5326e-06 > tol 1e-13]
CbParams_Moon_2Body_Earth/CbParams_Moon_2Body_Earth_BetaAngle.report
[max diff 1.52975e-06 > tol 1e-13]
CbParams_Moon_2Body_Mars/CbParams_Moon_2Body_Mars_BetaAngle.report [max
diff 3.01479e-09 > tol 1e-13]
CbParams_Moon_2Body_Moon/CbParams_Moon_2Body_Moon_BetaAngle.report [max
diff 1.10208e-12 > tol 1e-13]
CbParams_Moon_2Body_Moon/CbParams_Moon_2Body_Moon_Latitude.report [max
diff 8.1985e-07 > tol 1e-13]
CbParams_Moon_2Body_Moon/CbParams_Moon_2Body_Moon_Longitude.report [max
diff 2.07947e-07 > tol 1e-10]
CSParams_Mars1_2Body_EarthMJ2000Eq/CSParams_Mars1_2Body_EarthMJ2000Eq_RAAN.report
[max diff 1.57734e-05 > tol 1e-05]
CSParams_Mars1_2Body_MarsMJ2000Ec [max diff 5.93623e-05 > tol 1e-05]
CSParams_Mars1_2Body_MarsMJ2000Eq/CSParams_Mars1_2Body_MarsMJ2000Eq_RA.report
[max diff 1.11524e-05 > tol 1e-05]
CSParams_Mercury1_2Body_MercuryFixed [max diff 0.000137564 > tol 0.0001]
CSParams_Mercury1_2Body_MercuryMJ2000Ec [max diff 7.06381e-05 > tol
1e-05]
CSParams_Mercury1_2Body_MercuryMJ2000Eq [max diff 0.00017574 > tol
0.0001]
CSParams_Moon_2Body_EarthMJ2000Eq/CSParams_Moon_2Body_EarthMJ2000Eq_HX.report
[max diff 4.20635e-07 > tol 1e-13]
CSParams_Moon_2Body_EarthMJ2000Eq/CSParams_Moon_2Body_EarthMJ2000Eq_HY.report
[max diff 3.66291e-07 > tol 1e-13]
CSParams_Moon_2Body_EarthMJ2000Eq/CSParams_Moon_2Body_EarthMJ2000Eq_HZ.report
[max diff 3.03295e-06 > tol 1e-13]
CSParams_Moon_2Body_MoonMJ2000Eq/CSParams_Moon_2Body_MoonMJ2000Eq_HX.report
[max diff 5.5695e-12 > tol 1e-13]
CSParams_Moon_2Body_MoonMJ2000Eq/CSParams_Moon_2Body_MoonMJ2000Eq_HY.report
[max diff 1.23362e-09 > tol 1e-13]
CSParams_Moon_2Body_MoonMJ2000Eq/CSParams_Moon_2Body_MoonMJ2000Eq_HZ.report
[max diff 1.15308e-11 > tol 1e-13]
ElectricThruster_Propagation_CentralBodyStressTest [ vel err 0.000000]
EphemPropagator_EpochFormat_ChangeInMission [#1 failed]
EphemPropagator_StartEpoch_A1Gregorian [pos err 0.0409948, tol 0.0016]
EphemPropagator_StartEpoch_A1ModJulian [pos err 0.0420186, tol 0.0016]
EphemPropagator_StartEpoch_ChangeInMission [pos err 0.0420186, tol
0.0016]
EphemPropagator_StartEpoch_FromSpacecraft [pos err 0.0420186, tol
0.0016]
EphemPropagator_StartEpoch_TAIGregorian [pos err 0.0420186, tol 0.0016]
EphemPropagator_StartEpoch_TAIModJulian [pos err 0.0420177, tol 0.0016]
EphemPropagator_StartEpoch_TDBGregorian [pos err 0.0421713, tol 0.0019]
EphemPropagator_StartEpoch_TDBModJulian [pos err 0.0420169, tol 0.0016]
EphemPropagator_StartEpoch_TTGregorian [pos err 0.0420194, tol 0.0016]
EphemPropagator_StartEpoch_TTModJulian [pos err 0.0420177, tol 0.0016]
EphemPropagator_StartEpoch_UTCGregorian [pos err 0.0420186, tol 0.0016]
EphemPropagator_StartEpoch_UTCModJulian [pos err 0.0420186, tol 0.0016]
Events_ContactLocator_DiscontinuousEphem_UseEntireIntervalFalse_UseLightTimeDelayFalse
[diff # events]
Events_ContactLocator_DiscontinuousEphem_UseEntireIntervalTrue_UseLightTimeDelayFalse
[diff # events]
fmincon_Report [#1 failed]
fmincon_Validation_DuplicateNames [ptrn 1 failed]
FMParams_GMAT_Mars1_AllPlanets_0_0_0_Short [max diff 1.05524e-08 > tol
1e-09]
ForceModel_GravityField_Luna_TideModel_None [pos err 6.69323e-05, tol
5e-06]
ForceModel_GravityField_Luna_TideModel_None_STK [pos err 6.70242e-05,
tol 5e-06]
ForceModel_GravityField_Luna_TideModel_Solid [pos err 6.46044e-05, tol
3e-06]
ForceModel_GravityField_Luna_TideModel_Solid_STK [pos err 6.44268e-05,
tol 3e-06]
ForceModel_GravityField_Luna_ZeroTide_TideModel_None [pos err
6.80857e-05, tol 5e-06]
GMAT_Mars1_Mars_0_0_SRP [pos err 0.00135986, tol 0.001]
GMAT_Mars1_Mars_0_MarsGRAM2005_0 [vel err 3.70867e-07, tol 3e-07]
GMAT_Mars1_Mars_0_MarsGRAM2005_0_IgnoredInputVariables [vel err
3.70867e-07, tol 3e-07]
GMAT_Mars1_Mars_0_MarsGRAM2005_0_NonDefaultF107 [pos err 0.00047618,
tol 0.0003]
GMAT_Mars1_Mars_Mars50c_MarsGRAM2005_0 [pos err 0.00100484, tol 0.001]
GMAT_MarsLow_Mars_0_MarsGRAM2005_0_ModifiedRadFlat [pos err
0.000160603, tol 5e-05]
GMAT_Moon_AllPlanets_0_0_0 [pos err 1.18931e-05, tol 1e-06]
GMAT_Moon_Luna_0_0_0 [pos err 1.22912e-05, tol 1e-06]
GMAT_Moon_Luna_LP165P_0_0 [pos err 1.20846e-05, tol 1e-06]
GMAT_Moon_Luna_LP165P_0_SRP [pos err 1.22117e-05, tol 1e-06]
GMAT_Moon_Luna_LP165P_0_SRP_Short [pos err 1.14395e-06, tol 1e-06]
GMAT_MoonPM_Luna_0_0_0 [pos err 1.22912e-05, tol 1e-06]
GMAT_Pluto1_Pluto_0_0_SRP [pos err 0.00117338, tol 0.001]
MatlabFunction_FunctionPath_Relative [diff 0.141593, tol 1e-13]
Optimize_fmincon_CostFunction_and_ConvergedStatus_Display [ptrn 1,2,3
failed]
Optimize_fmincon_CostFunction_and_ConvergedStatus_Display_2 [ptrn 1,2,3
failed]
Optimize_fmincon_Max_Iterations_Display [ptrn 1,2 failed]
Optimize_Validation_fmincon_Disallowed_Sequences [ptrn 1 failed]
Optimize_Validation_fmincon_No_Vary_Command [ptrn 1 failed]
Orbit_RepresentationConversions_CircularEquatorial2 [max diff 1 > tol
1e-10]
Orbit_RepresentationConversions_EllipticEquatorial_Mars [diff
3.09628e-08, tol 1e-08]
Orbit_RepresentationConversions_MixedReps_Planetodetic [max diff
1.12971e-07 > tol 3e-08]
OrbitConv_Dela_MarsFixed_Elliptic_InPro_Cartesian [max diff 1.95693e-08
> tol 1e-08]
OrbitConv_Dela_MarsMJ2000Eq_Elliptic_InPro_Cartesian [max diff
1.72432e-08 > tol 1e-08]
OrbitRepConv_MarsFixed_Elliptic_IncPro_Cartesian [max diff 1.96093e-08
> tol 1e-08]
OrbitRepConv_MarsFixed_Elliptic_IncPro_ModifiedEquinoctial [max diff
1.57832e-08 > tol 1e-08]
OrbitRepConv_NeptuneMJ2000Eq_Circular_EqPro_Cartesian [max diff
1.19209e-07 > tol 1e-08]
OrbitRepConv_NeptuneMJ2000Eq_Elliptic_EqPro_Cartesian [max diff
1.19209e-07 > tol 1e-08]
OrbitRepConv_NeptuneMJ2000Eq_Hyperbolic_EqPro_Cartesian [max diff
1.19209e-07 > tol 1e-08]
OrbitRepConv_SunMJ2000Eq_Circular_Polar_SphericalAzEl [max diff 2 > tol
1e-08]
OrbitRepConv_SunMJ2000Eq_Elliptic_Polar_SphericalAzEl [max diff 2 > tol
1e-08]
OrbitState_EpochAndCoordSysChange_Cartesian [max diff 4.59725e-09 > tol
1e-09]
OrbitState_EpochFormat [max diff 3.01729 > tol 1e-10]
OREx_Outbound_Cruise_Optimization [diff 0.000904972, tol 0.0005]
OREx_Outbound_Cruise_Optimization_In_FunctionMode [diff 0.000904972,
tol 0.0005]
OREx_Outbound_Cruise_Optimization_With_Global_Subscribers_And_Objects
[diff 0.000798388, tol 0.0004]
Params_LhsDeps_Planetodetic_ImplicitFixed [max diff 3.40139e-09 > tol
2e-09]
Python_NoInputsOutputs []
Python_NoOutputs []
Receiver_ErrorModels [Output field -1988.527405 failed tolerance in
record 145]
Receiver_Id [Output field -1988.527405 failed tolerance in record 145]
Simulator_MeasurementTimeStep_1 [#2 failed]
SpacecraftNavigation_SolveFors_OrderOfParameters_Cd_Cr [Found 1 output
records and 6 truth records] [GMT-6658]
SpacePointParams_BaryCenter_CartesianParams []
SpacePointParams_Barycenter_TimeDependendCS []
SpacePointParams_Barycenter_TimeDependendCS2 []
SpacePointParams_GroundStation_CartesianParams []
SpacePointParams_LibrationPoint_CartesianParams []
SpacePointParams_LibrationPoint_TimeDependendCS []
SpacePointParams_SSB_CartesianParams []
StopCond_GMAT_MarsPM_Apoapsis [diff 1.20742e-06, tol 1e-06]
StopCond_GMAT_MarsPM_TA180 [diff 1.20742e-06, tol 1e-06]
Thruster_FBurn_Jupiter_ScA_ThrusterE_CS0_TankA [pos err 0.000012]
Thruster_FBurn_Jupiter_ScA_ThrusterE_CS2_TankA [pos err 0.000023]
Thruster_FBurn_Jupiter_ScA_ThrusterE_CS3_TankA [pos err 0.000012]
Thruster_FBurn_Neptune_ScA_ThrusterF_CS0_TankA [pos err 0.000027]
Thruster_FBurn_Neptune_ScA_ThrusterF_CS3_TankA [pos err 0.000027]
Thruster_FBurn_Neptune_ScA_ThrusterH_CS1_TankA [pos err 0.000012]
Thruster_FBurn_Neptune_ScA_ThrusterH_CS2_TankA [pos err 0.000021]
Thruster_FBurn_Saturn_ScA_ThrusterA_CS0_TankA [pos err 0.000019]
Thruster_FBurn_Saturn_ScA_ThrusterA_CS3_TankA [pos err 0.000019]
Thruster_FBurn_Saturn_ScA_ThrusterC_CS0_TankA [pos err 0.000019]
Thruster_FBurn_Saturn_ScA_ThrusterC_CS3_TankA [pos err 0.000019]
Thruster_FBurn_Uranus_ScA_ThrusterA_CS1_TankA [pos err 0.000012]
Thruster_FBurn_Uranus_ScA_ThrusterC_CS0_TankA [pos err 0.000011]
Thruster_FBurn_Uranus_ScA_ThrusterC_CS3_TankA [pos err 0.000011]
Thruster_FBurn_Uranus_ScA_ThrusterD_CS1_TankA [pos err 0.000011]
Thruster_FBurn_Uranus_ScA_ThrusterF_CS0_TankA [pos err 0.000015]
Thruster_FBurn_Uranus_ScA_ThrusterF_CS3_TankA [pos err 0.000015]
TrackingFileSet_ChebyshevDEBoundary_1day [ Observable Error: 7.439e-05
Hz]
TrackingFileSet_ChebyshevDEBoundary_1hour [ Observable Error: 9.441e-05
Hz]
Transmitter_Frequency_DSN_Doppler_DeepSpace []
Transmitter_Frequency_DSN_Doppler_DeepSpace_2 []
TrkFile_SimEst_DSN_DS_Range_Solve_Keplerian_Unconstrained []
Tut_MultipleShootingTutorial_Step3 []
Vary_optimizer_fmincon__AdditiveScaleFactor_Variable [ptrn 1,2 failed]
Vary_optimizer_fmincon_Additive_and_Multiplicative_ScaleFactor_RealNumber [ptrn
1,2 failed]
Vary_optimizer_fmincon_AdditiveScaleFactor_ArrayElement [ptrn 1,2
failed]
Vary_optimizer_fmincon_AdditiveScaleFactor_RealNumber [ptrn 1,2 failed]
Vary_optimizer_fmincon_MultiplicativeScaleFactor_ArrayElement [ptrn 1,2
failed]
Vary_optimizer_fmincon_MultiplicativeScaleFactor_RealNumber [ptrn 1,2
failed]
Vary_optimizer_fmincon_MultiplicativeScaleFactor_Variable [ptrn 1,2
failed]
-----------------------------------------------------------------
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):
BatchEstimator_EstimationEpoch [GMT-5708]
Math_Shadowed_Builtins [GMT-3043]
Python_IO_String [5317]
ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522]
TrkFile_SimEst_DSN_DS_Range_Solve_Bias_apriori [GMT-5709]
Comparator errors (deferred):
GroundStation_Iono_Range_Kband (truth) [GMT-5644]
GroundStation_Iono_RangeRate_Kband (truth) [GMT-5644]
GroundStation_TropoIono_Range_Kband (truth) [GMT-5644]
Truth failures (deferred):
AcceptFilter_Validation_RecordNumbers [#5 failed] [GMT-6034]
Achieve_Validation_LHS_Field [ptrn 1 failed] [GMT-3687]
Ephem_GMAT_Code500_InterpolationOrder/Ephem_GMAT_Code500_InterpolationOrder_1.eph
[pos err 0.0173914, 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 15.2466, 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 14.3693, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
[pos err 0.000216981, tol 1e-12] [GMT-4112]
EphemStressTests_PD78_ABM_Prop_Code500_60Sec_Step_ForwardDirection [pos
err 21.5632, 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 greg. diff 1.000005s > tol 0.001000s] [2561]
Epoch_LeapSecond_Out [max mjd diff 1.000146s > tol 0.001000s] [2561]
GMAT_ISS_Earth_JGM2_0_0_NutationUpdateInterval [pos err 0.00081496, tol
1e-06] [GMT-2567]
Math_Inf [GMAT: 53 lines, Truth: 69 lines] [GMT-3195]
Minimize_Validation_Field [ptrn 1 failed] [GMT-3687]
Nonlinear_Validation_LHS_Field [ptrn 1 failed] [GMT-3687]
Nonlinear_Validation_RHS_Field [ptrn 1 failed] [GMT-3687]
Optimize_Yukon_Minimize_Height_on_circle_2 [diff 497, tol 0.001]
Optimize_Yukon_Minimize_Height_on_circle_4 [diff 497, tol 0.001]
RejectFilter_Validation_RecordNumbers [#5 failed] [GMT-6034]
ScriptLanguage_Comments_AfterControlFlow [] [GMT-3332]
ScriptLanguage_LineContinuation_BeginningOfLine [] [GMT-3756]
ScriptLanguage_LiteralArrays_String [] [GMT-3680]
ScriptLanguage_ReferenceArrays_ForceModel_7 [] [GMT-3541]
Simulator_MoonOccultation [GMAT: 11299 lines, Truth: 11306 lines]
[GMT-6134]
SpacecraftNavigation_Validation_Mode [#1 failed] [GMT-5841]
String_AssignNumericParam [] [GMT-2888]
Write_Multiple_ReportFile_Concise_2 [#69 failed] [GMT-5801]
Write_Multiple_ReportFile_Verbose_2 [#69 failed] [GMT-5801]
-----------------------------------------------------------------
Test System Warnings
-----------------------------------------------------------------
Passing tests tagged with bugs:
(To fix, remove bug ID from Bugs key in .tc file)
Achieve_Validation_RHS_Field [GMT-3687]
BatchEstimator_ReportFile_InitialState [GMT-6412]
Comet_Validation_OrientationEpoch_3 [GMT-3252]
CoordSysTest_Luna_MJ2000Eq_To_ICRF [GMT-3227]
CoordinateSystem_Validation_Axes_4 [GMT-3155]
EphemPropagator_Code500_CentralBody_Jupiter [GMT-5795]
EphemPropagator_Code500_CentralBody_Saturn [GMT-5795]
EphemPropagator_Code500_ForwardProp_Interp [GMT-5760]
EphemPropagator_SatAssigmentToNewSatThenProp [GMT-3434]
EphemStressTests_Default_Prop_STK_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection
[GMT-6090]
EphemStressTests_Default_Prop_STK_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect
[GMT-6090]
Ephem_GMAT_SPK_60sec_backward [GMT-5286]
Ephem_GMAT_SPK_DefaultIntegrationStep_User_Defined_LagrangeOrder
[GMT-5286]
Ephem_GMAT_STK_60sec_IterativeProcess_Optimizer [GMT-6090]
Ephem_GMAT_STK_60sec_IterativeProcess_Optimizer_NoBoundaries [GMT-6090]
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_MissingComma [GMT-3672]
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]
Math_Validation_Cross_WrongDim2 [GMT-5676]
ScriptLanguage_Validation_DataTypes_ReferenceArray_Formation_5
[GMT-6064]
ScriptLanguage_Validation_Semicolons_1 [GMT-3545]
Simulator_Propagator_EarthPointMass_Drag [GMT-5417]
Simulator_Propagator_EarthPointMass_SRP_Drag [GMT-5417]
Simulator_Propagator_Sun_EM [GMT-6040]
Simulator_Propagator_Sun_EM_AllPlanets [GMT-6040]
Simulator_Propagator_Sun_EM_AllPlanets_SRP_GR [GMT-6040]
Simulator_Propagator_Sun_EM_GR [GMT-6040]
SpacePointParams_CelestialBody_EpochOutput [3939]
Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
TrkFile_SimEst_TDRS_range_Solve_Cr [GMT-5416]
Vary_Validation_RHS_Field [GMT-3687]
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