I took a look at the following failures:
Thruster_FBurn_Jupiter_ScA_ThrusterE_CS2_TankA [pos err 0.000016]
Thruster_FBurn_Neptune_ScA_ThrusterE_CS2_TankA [pos err 0.000023]
They test has a position tolerance of 1e-5. So, we almost meet the tolerance.
These two scripts use RSSStep with an accuracy of 1e-9 which is a bit loose. I
did some experiments:
R2018a
Truth failures:
Thruster_FBurn_Jupiter_ScA_ThrusterE_CS2_TankA [pos err 0.000009]
Thruster_FBurn_Neptune_ScA_ThrusterE_CS2_TankA [pos err 0.000006]
Master (this latest run with John's changes)
Truth failures:
Thruster_FBurn_Jupiter_ScA_ThrusterE_CS2_TankA [pos err 0.000016]
Thruster_FBurn_Neptune_ScA_ThrusterE_CS2_TankA [pos err 0.000023]
Now change accuracy tolerance from 1e-9 to 1e-12. Also, set minstep to 0.
Master
Truth failures:
Thruster_FBurn_Jupiter_ScA_ThrusterE_CS2_TankA [pos err 0.000012]
Thruster_FBurn_Neptune_ScA_ThrusterE_CS2_TankA [pos err 0.000065]
R2018a (so with a tighter tolerance, R2018a would fail. Odd. )
Truth failures:
Thruster_FBurn_Jupiter_ScA_ThrusterE_CS2_TankA [pos err 0.000012]
Thruster_FBurn_Neptune_ScA_ThrusterE_CS2_TankA [pos err 0.000095]
So, tightening the tolerance doesn't do what we think it should. Is the truth
file not perfect? Or, maybe, this is best GMAT can do. Not sure.
In any event, my take away is that we are probably (?) OK but if there is a
problem, it is pre-existing.
Thoughts?
Unless I hear otherwise, I will probably change tolerance on these 2 tests from
1e-5 to 3e-5.
(for one of the scripts, I set nutation update interval to 0 to no affect)
-----Original Message-----
From: [email protected] <[email protected]>
Sent: Saturday, May 4, 2019 3:58 AM
To: Cooley, D S. (GSFC-5950) <[email protected]>;
[email protected]
Subject: Test results: 2019-05-03 (GS580W-GMAT-T6/Win7-64/GMAT-64/M2016a/VS2017)
-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Windows 10/MATLAB R2017a/VS 2013 Tested build: 2019-05-03
Regression build: 2019-05-02
Total number of scripts: 14268 (+75 deferred) Percent Passed: 99.65% New
issues: 247
Output changes: 212
New truth failures: 18
New crashes: 0
New script errors: 17
New comparator errors: 0
Fixed issues: 7
Total issues: 51
Test system warnings: 43
New deferred issues: 9
Fixed deferred issues: 1
Total deferred issues: 49
Run Time: 14 hours, 42 minutes, 38 seconds
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
fmincon_Report [#3 failed]
fmincon_ShowProgress [#1 failed]
GMATFunction_1stTarget_InFunction_2nd_In_Script_GlobalObjects_GlobalSC_As_Input_Output
[diff 0.000178855, tol 9e-05]
GMATFunction_Mars_B_Plane_Targeting_Global_Subscribers [diff
0.000528951, tol 0.0005]
Mars_B_Plane_Targeting_In_FunctionMode [diff 0.000528951, tol
0.0005]
Optimize_vf13ad_SolveMode_SaveAndContinue_GMT-4346 []
OREx_Outbound_Cruise_Optimization [diff 0.000606119, tol 0.0005]
OREx_Outbound_Cruise_Optimization_In_FunctionMode [diff
0.000606119, tol 0.0005]
OREx_Outbound_Cruise_Optimization_With_Global_Subscribers_And_Objects
[diff 0.00065214, tol 0.0004]
Simulator_AsteroidOccultation [#1 failed]
Thruster_FBurn_Jupiter_ScA_ThrusterE_CS2_TankA [pos err 0.000016]
Thruster_FBurn_Neptune_ScA_ThrusterE_CS2_TankA [pos err 0.000023]
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]
Output changes (but still pass):
ACE_impulsive_493
ACE_impulsive_493_In_FunctionMode
Achieve_PiC_Tolerance_SatParameter
Achieve_PiC_Tolerance_UserArray
Ballistic_and_Mass_Case01_GTO
Ballistic_and_Mass_Case01_LEO
Ballistic_and_Mass_Case01_LEO_Cmd
Ballistic_and_Mass_Case02_GTO
Ballistic_and_Mass_Case02_LEO
Ballistic_and_Mass_Case03_LEO
Ballistic_and_Mass_Case04_LEO
BatchEstimator_ReportFile_MeasurementModeling
BeginFBurn_ChangePropDuringBurn
EKF_ErrorModel_NoiseSigma_Range
ElectricThruster_Propagation_CentralBodyStressTest
Ephem_GMAT_Code500_60sec
Ephem_GMAT_Code500_ACE_OpsPrototype_v13
Ephem_GMAT_Code500_CoordinateSystem
Ephem_GMAT_Code500_CoordinateSystem
Ephem_GMAT_Code500_TimeInteractions
Ephem_GMAT_Code500_TimeInteractions
FBurn_Mars_VNB
GMAT_Asteroid_NonsphericalGravity
GMAT_Comet_NonsphericalGravity
GMAT_IncludeMacro_MarsBPlaneTarget_All_ResourcesCommands_From_IncludeScript
GMAT_IncludeMacro_MarsBPlaneTarget_OnlyResourceObjects_From_IncludeFile
GMAT_ISS_Earth_0_MSISE86_0_NonDefaultEarthRadiusFlattening
GMAT_ISS_Earth_0_MSISE90_0
GMAT_ISS_Earth_0_MSISE90_0_NonDefaultEarthRadiusFlattening
GMAT_ISS_Earth_0_MSISE90_ModifiedFluxAndGeoMag
GMAT_ISS_Earth_0_NRLMSISE00_0
GMAT_ISS_Earth_0_NRLMSISE00_0_NonDefaultEarthRadiusFlattening
GMAT_ISS_Earth_0_NRLMSISE00_ModifiedFluxAndGeoMag
GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP
GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Lower_Error_ABM
GMAT_ISS_EarthSunLuna_JGM2_NRLMSISE00_SRP
GMAT_ISS_EarthSunLuna_JGM3_MSISE90_SRP_Cmd
GMAT_LunarTran_PropSynchronization_ABM
GMAT_MarsTransfer_2
GMAT_MarsTransfer_4_ABM
GMAT_MAVEN_Mars_0_MarsGRAM2005_0
GMAT_Moon_NonsphericalGravity
GMAT_UserAsteroid_AllPlanets_SRP_Mars50c
GMAT_UserComet_AllPlanets_SRP_Mars50c
GMAT_UserDefinedMars_NonsphericalGravity
GMAT_UserMoon-Titan_AllPlanets_SRP
GMAT_UserPlanet_AllPlanets_SRP_Mars50c
GMAT_UserPlanet_NonsphericalGravity
GMATFunction_1stTargeter_In_Function_2nd_In_MainScript_Global_Objects
GMATFunction_ACE_impulsive_493_Global_Subscribers_User_Defined_Parameters
GMATFunction_ACE_Ops_Global_Objects_Send_GlobalSCs_As__Input_And_Output
GMATFunction_ACE_Ops_Global_Objects_Send_GlobalSCs_As__Output
GMATFunction_EarthFixedPropFun
GMATFunction_EarthFixedPropFun_Periapsis
GMATFunction_Function_Inside_While_If_Else_Loop_Global_SC_Subscribers_Other_Objects
GMATFunction_Global_SC_And_Subscribers_And_Also_Pass_LocalSCs_Params_As_IO
GMATFunction_LEOStationKeeping_Targeting_LocalSC_In_LocalSC_Out_Method_1
GMATFunction_LEOStationKeeping_Targeting_LocalSC_In_LocalSC_Out_Method_2
GMATFunction_Mars_B_Plane_Targeting_InFunction_Pass_Local_SC_In_Out
GMATFunction_Mars_BPlane_Targeting_GlobalObjects_GlobalSC_As_Input_Output
GMATFunction_Mars_BPlane_Targeting_GlobalObjects_GlobalSC_As_Output_Only
GMATFunction_MJ2000EcProp
GMATFunction_MJ2000EcPropFun_Apoapsis
GMATFunction_MJ2000EqProp
GMATFunction_MJ2000EqPropFun_Apoapsis
Integrator_GEO_ABM_2Body
Mars_B_Plane_Targeting
OREx_Outbound_Cruise_Optimization_Global_Objects_Send_GlobalSC_As_InputOutput
ScriptEvent_SmokeTests_Ballistic_and_Mass_Case04_LEO
ScriptEvent_SmokeTests_GMAT_Asteroid_NonsphericalGravity
Simulator_EpochFormat_TDBGregorian
Simulator_EpochFormat_TDBModJulian
Simulator_MoonOccultation
StopCond_GMAT_EarthAll_MA90
StopGroupingBug
Target_Raise_Apogee
Thruster_FBurn_Jupiter_ScA_ThrusterA_CS1_TankA
Thruster_FBurn_Jupiter_ScA_ThrusterA_CS2_TankA
Thruster_FBurn_Jupiter_ScA_ThrusterB_CS1_TankA
Thruster_FBurn_Jupiter_ScA_ThrusterB_CS2_TankA
Thruster_FBurn_Jupiter_ScA_ThrusterC_CS1_TankA
Thruster_FBurn_Jupiter_ScA_ThrusterC_CS2_TankA
Thruster_FBurn_Jupiter_ScA_ThrusterD_CS1_TankA
Thruster_FBurn_Jupiter_ScA_ThrusterD_CS2_TankA
Thruster_FBurn_Jupiter_ScA_ThrusterE_CS1_TankA
Thruster_FBurn_Jupiter_ScA_ThrusterF_CS1_TankA
Thruster_FBurn_Jupiter_ScA_ThrusterF_CS2_TankA
Thruster_FBurn_Jupiter_ScA_ThrusterH_CS1_TankA
Thruster_FBurn_Jupiter_ScA_ThrusterH_CS2_TankA
Thruster_FBurn_Luna_ScA_ThrusterA_CS1_TankA
Thruster_FBurn_Luna_ScA_ThrusterA_CS2_TankA
Thruster_FBurn_Luna_ScA_ThrusterB_CS1_TankA
Thruster_FBurn_Luna_ScA_ThrusterB_CS2_TankA
Thruster_FBurn_Luna_ScA_ThrusterC_CS1_TankA
Thruster_FBurn_Luna_ScA_ThrusterC_CS2_TankA
Thruster_FBurn_Luna_ScA_ThrusterD_CS1_TankA
Thruster_FBurn_Luna_ScA_ThrusterD_CS2_TankA
Thruster_FBurn_Luna_ScA_ThrusterE_CS1_TankA
Thruster_FBurn_Luna_ScA_ThrusterE_CS2_TankA
Thruster_FBurn_Luna_ScA_ThrusterF_CS1_TankA
Thruster_FBurn_Luna_ScA_ThrusterF_CS2_TankA
Thruster_FBurn_Luna_ScA_ThrusterH_CS1_TankA
Thruster_FBurn_Luna_ScA_ThrusterH_CS2_TankA
Thruster_FBurn_Mars_ScA_ThrusterA_CS1_TankA
Thruster_FBurn_Mars_ScA_ThrusterA_CS2_TankA
Thruster_FBurn_Mars_ScA_ThrusterB_CS1_TankA
Thruster_FBurn_Mars_ScA_ThrusterB_CS2_TankA
Thruster_FBurn_Mars_ScA_ThrusterC_CS1_TankA
Thruster_FBurn_Mars_ScA_ThrusterC_CS2_TankA
Thruster_FBurn_Mars_ScA_ThrusterD_CS1_TankA
Thruster_FBurn_Mars_ScA_ThrusterD_CS2_TankA
Thruster_FBurn_Mars_ScA_ThrusterE_CS1_TankA
Thruster_FBurn_Mars_ScA_ThrusterE_CS2_TankA
Thruster_FBurn_Mars_ScA_ThrusterF_CS1_TankA
Thruster_FBurn_Mars_ScA_ThrusterF_CS2_TankA
Thruster_FBurn_Mars_ScA_ThrusterH_CS1_TankA
Thruster_FBurn_Mars_ScA_ThrusterH_CS2_TankA
Thruster_FBurn_Mercury_ScA_ThrusterA_CS1_TankA
Thruster_FBurn_Mercury_ScA_ThrusterA_CS2_TankA
Thruster_FBurn_Mercury_ScA_ThrusterB_CS1_TankA
Thruster_FBurn_Mercury_ScA_ThrusterB_CS2_TankA
Thruster_FBurn_Mercury_ScA_ThrusterC_CS1_TankA
Thruster_FBurn_Mercury_ScA_ThrusterC_CS2_TankA
Thruster_FBurn_Mercury_ScA_ThrusterD_CS1_TankA
Thruster_FBurn_Mercury_ScA_ThrusterD_CS2_TankA
Thruster_FBurn_Mercury_ScA_ThrusterE_CS1_TankA
Thruster_FBurn_Mercury_ScA_ThrusterE_CS2_TankA
Thruster_FBurn_Mercury_ScA_ThrusterF_CS1_TankA
Thruster_FBurn_Mercury_ScA_ThrusterF_CS2_TankA
Thruster_FBurn_Mercury_ScA_ThrusterF_CS2_TankA_2
Thruster_FBurn_Mercury_ScA_ThrusterF_CS2_TankA_3
Thruster_FBurn_Mercury_ScA_ThrusterF_CS2_TankA_4
Thruster_FBurn_Mercury_ScA_ThrusterF_CS2_TankA_5
Thruster_FBurn_Mercury_ScA_ThrusterH_CS1_TankA
Thruster_FBurn_Mercury_ScA_ThrusterH_CS2_TankA
Thruster_FBurn_Neptune_ScA_ThrusterA_CS1_TankA
Thruster_FBurn_Neptune_ScA_ThrusterA_CS2_TankA
Thruster_FBurn_Neptune_ScA_ThrusterB_CS1_TankA
Thruster_FBurn_Neptune_ScA_ThrusterB_CS2_TankA
Thruster_FBurn_Neptune_ScA_ThrusterC_CS1_TankA
Thruster_FBurn_Neptune_ScA_ThrusterC_CS2_TankA
Thruster_FBurn_Neptune_ScA_ThrusterD_CS1_TankA
Thruster_FBurn_Neptune_ScA_ThrusterD_CS2_TankA
Thruster_FBurn_Neptune_ScA_ThrusterE_CS1_TankA
Thruster_FBurn_Neptune_ScA_ThrusterF_CS1_TankA
Thruster_FBurn_Neptune_ScA_ThrusterF_CS2_TankA
Thruster_FBurn_Neptune_ScA_ThrusterH_CS1_TankA
Thruster_FBurn_Neptune_ScA_ThrusterH_CS2_TankA
Thruster_FBurn_Pluto_ScA_ThrusterA_CS1_TankA
Thruster_FBurn_Pluto_ScA_ThrusterA_CS2_TankA
Thruster_FBurn_Pluto_ScA_ThrusterB_CS1_TankA
Thruster_FBurn_Pluto_ScA_ThrusterB_CS2_TankA
Thruster_FBurn_Pluto_ScA_ThrusterC_CS1_TankA
Thruster_FBurn_Pluto_ScA_ThrusterC_CS2_TankA
Thruster_FBurn_Pluto_ScA_ThrusterD_CS1_TankA
Thruster_FBurn_Pluto_ScA_ThrusterD_CS2_TankA
Thruster_FBurn_Pluto_ScA_ThrusterE_CS1_TankA
Thruster_FBurn_Pluto_ScA_ThrusterE_CS2_TankA
Thruster_FBurn_Pluto_ScA_ThrusterF_CS1_TankA
Thruster_FBurn_Pluto_ScA_ThrusterF_CS2_TankA
Thruster_FBurn_Pluto_ScA_ThrusterH_CS1_TankA
Thruster_FBurn_Pluto_ScA_ThrusterH_CS2_TankA
Thruster_FBurn_Saturn_ScA_ThrusterA_CS1_TankA
Thruster_FBurn_Saturn_ScA_ThrusterA_CS2_TankA
Thruster_FBurn_Saturn_ScA_ThrusterB_CS1_TankA
Thruster_FBurn_Saturn_ScA_ThrusterB_CS2_TankA
Thruster_FBurn_Saturn_ScA_ThrusterC_CS1_TankA
Thruster_FBurn_Saturn_ScA_ThrusterC_CS2_TankA
Thruster_FBurn_Saturn_ScA_ThrusterD_CS1_TankA
Thruster_FBurn_Saturn_ScA_ThrusterD_CS2_TankA
Thruster_FBurn_Saturn_ScA_ThrusterE_CS1_TankA
Thruster_FBurn_Saturn_ScA_ThrusterE_CS2_TankA
Thruster_FBurn_Saturn_ScA_ThrusterF_CS1_TankA
Thruster_FBurn_Saturn_ScA_ThrusterF_CS2_TankA
Thruster_FBurn_Saturn_ScA_ThrusterH_CS1_TankA
Thruster_FBurn_Saturn_ScA_ThrusterH_CS2_TankA
Thruster_FBurn_Uranus_ScA_ThrusterA_CS1_TankA
Thruster_FBurn_Uranus_ScA_ThrusterA_CS2_TankA
Thruster_FBurn_Uranus_ScA_ThrusterB_CS1_TankA
Thruster_FBurn_Uranus_ScA_ThrusterB_CS2_TankA
Thruster_FBurn_Uranus_ScA_ThrusterC_CS1_TankA
Thruster_FBurn_Uranus_ScA_ThrusterC_CS2_TankA
Thruster_FBurn_Uranus_ScA_ThrusterD_CS1_TankA
Thruster_FBurn_Uranus_ScA_ThrusterD_CS2_TankA
Thruster_FBurn_Uranus_ScA_ThrusterE_CS1_TankA
Thruster_FBurn_Uranus_ScA_ThrusterE_CS2_TankA
Thruster_FBurn_Uranus_ScA_ThrusterF_CS1_TankA
Thruster_FBurn_Uranus_ScA_ThrusterF_CS2_TankA
Thruster_FBurn_Uranus_ScA_ThrusterH_CS1_TankA
Thruster_FBurn_Uranus_ScA_ThrusterH_CS2_TankA
Thruster_FBurn_Venus_ScA_ThrusterA_CS1_TankA
Thruster_FBurn_Venus_ScA_ThrusterA_CS2_TankA
Thruster_FBurn_Venus_ScA_ThrusterB_CS1_TankA
Thruster_FBurn_Venus_ScA_ThrusterB_CS2_TankA
Thruster_FBurn_Venus_ScA_ThrusterC_CS1_TankA
Thruster_FBurn_Venus_ScA_ThrusterC_CS2_TankA
Thruster_FBurn_Venus_ScA_ThrusterD_CS1_TankA
Thruster_FBurn_Venus_ScA_ThrusterD_CS2_TankA
Thruster_FBurn_Venus_ScA_ThrusterE_CS1_TankA
Thruster_FBurn_Venus_ScA_ThrusterE_CS2_TankA
Thruster_FBurn_Venus_ScA_ThrusterF_CS1_TankA
Thruster_FBurn_Venus_ScA_ThrusterF_CS2_TankA
Thruster_FBurn_Venus_ScA_ThrusterH_CS1_TankA
Thruster_FBurn_Venus_ScA_ThrusterH_CS2_TankA
Thruster_Finite_Burn_Permutations_Separate_Propagators_LVLH_2
Thruster_Finite_Burn_Permutations_Separate_Propagators_VNB_2
TrackingFileSet_ChebyshevDEBoundary_1day
TrackingFileSet_ChebyshevDEBoundary_1hour
TrackingFileSet_UseETminusTAI_AzimuthElevation_Est
TrackingFileSet_UseETminusTAI_XEastYNorth_Est
TrackingFileSet_UseETminusTAI_XSouthYEast_Est
Output changes (but still fail):
THF_Sim_Accel_ConfigD_None_NA_FixedStep [ Observable Error:
0.3425 m.] [FixedStep 1 second, Sim, constant thrust over entire interval,
should it pass]
New crashes/hangs/etc.:
None
New script errors:
SpacecraftNavigation_SolveFors_CartesianState_TSF_AzimuthElevation
SpacecraftNavigation_SolveFors_CartesianState_TSF_XEastYNorth
SpacecraftNavigation_SolveFors_CartesianState_TSF_XSouthYEast
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable
Vary_optimizer_fmincon_Perturbation_ArrayElement
Vary_optimizer_fmincon_Perturbation_RealNumber
Vary_optimizer_fmincon_Perturbation_Variable
Vary_optimizer_fmincon_UpperBound_ArrayElement
Vary_optimizer_fmincon_UpperBound_Variable
Vary_optimizer_fmincon__InitialValue_Array
Vary_optimizer_fmincon__InitialValue_RealNumber
Vary_optimizer_fmincon__InitialValue_Variable
Vary_optimizer_fmincon__LowerBound_Array
Vary_optimizer_fmincon__LowerBound_Variable
completed_steps_1_thru_10_of_FRC_1_using_fmincon_Optimizer
fmincon_ConstraintTolerance
New comparator errors:
None
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
Matlab_NoOutputs
Tut_MultipleShootingTutorial_Step3
Fixed crashes/hangs/etc.:
None
Fixed script errors:
Optimize_fmincon_ExitMode_DiscardAndContinue
Optimize_fmincon_Minimize_Height_on_circle_2
Optimize_fmincon_cvg_status
Transmitter_Frequency_DSN_Doppler_DeepSpace_2
scriptEvent_optimizer_fmincon__InitialValue_Variable
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
None
Script errors:
Optimize_fmincon_ExitMode_SaveAndContinue_3:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Optimize_fmincon_ExitMode_SaveAndContinue_3.report
does not exist
SpacecraftNavigation_SolveFors_CartesianState_TSF_AzimuthElevation:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\SpacecraftNavigation_SolveFors_CartesianState_TSF_AzimuthElevation.txt
does not exist
SpacecraftNavigation_SolveFors_CartesianState_TSF_XEastYNorth:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\SpacecraftNavigation_SolveFors_CartesianState_TSF_XEastYNorth.txt
does not exist
SpacecraftNavigation_SolveFors_CartesianState_TSF_XSouthYEast:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\SpacecraftNavigation_SolveFors_CartesianState_TSF_XSouthYEast.txt
does not exist
THF_Sim_Accel_ConfigD_None_NA_2: [GMT-6451]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\THF_Sim_Accel_ConfigD_None_NA_2.gmd
does not exist
THF_Sim_Accel_ConfigD_None_NA_3: [GMT-6451]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\THF_Sim_Accel_ConfigD_None_NA_3.gmd
does not exist
THF_Sim_Accel_ConfigD_None_NA_4: [GMT-6451]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\THF_Sim_Accel_ConfigD_None_NA_4.gmd
does not exist
THF_Sim_Accel_ConfigD_None_NA: [GMT-6451]
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\THF_Sim_Accel_ConfigD_None_NA.gmd
does not exist
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_InitialGuess_ForLoopVariable_2.report
does not exist
Vary_optimizer_fmincon_InitialGuess_ForLoopVariable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_InitialGuess_ForLoopVariable.report
does not exist
Vary_optimizer_fmincon_Perturbation_ArrayElement:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_Perturbation_ArrayElement.report
does not exist
Vary_optimizer_fmincon_Perturbation_RealNumber:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_Perturbation_RealNumber.report
does not exist
Vary_optimizer_fmincon_Perturbation_Variable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_Perturbation_Variable.report
does not exist
Vary_optimizer_fmincon_UpperBound_ArrayElement:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_UpperBound_ArrayElement.report
does not exist
Vary_optimizer_fmincon_UpperBound_Variable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon_UpperBound_Variable.report
does not exist
Vary_optimizer_fmincon__InitialValue_Array:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__InitialValue_Array.report
does not exist
Vary_optimizer_fmincon__InitialValue_RealNumber:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__InitialValue_RealNumber.report
does not exist
Vary_optimizer_fmincon__InitialValue_Variable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__InitialValue_Variable.report
does not exist
Vary_optimizer_fmincon__LowerBound_Array:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__LowerBound_Array.report
does not exist
Vary_optimizer_fmincon__LowerBound_RealNumber:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\output\Vary_optimizer_fmincon__LowerBound_RealNumber.report
does not exist
Vary_optimizer_fmincon__LowerBound_Variable:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\ScriptTest\gmat\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\ScriptTest\gmat\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\ScriptTest\gmat\output\fmincon_ConstraintTolerance.report
does not exist
Comparator errors:
None
Truth failures:
EKF_AcceptFilter_Level2_FileNames_GpsPosVec [#1 failed]
[GMT-6762]
EKF_RejectFilter_Level2_FileNames_GpsPosVec [#457 failed]
[GMT-6762]
EKF_TrackingFileSet_AddTrackingConfig_All [#15 failed] [GMT-6785]
EphemStressTests_Default_Prop_CCSDS_Forward_and_BackwardDirect []
fmincon_Report [#3 failed]
fmincon_ShowProgress [#1 failed]
ForceModel_Drag_SpaceWeatherFile_LineEndings [pos err 1.22211,
tol 2e-06] [GMT-6673]
GMATFunction_1stTarget_InFunction_2nd_In_Script_GlobalObjects_GlobalSC_As_Input_Output
[diff 0.000178855, tol 9e-05]
GMATFunction_Mars_B_Plane_Targeting_Global_Subscribers [diff
0.000528951, tol 0.0005]
KalmanFilter_Validation_MatlabFile [#1 failed] [GMT-6784]
Mars_B_Plane_Targeting_In_FunctionMode [diff 0.000528951, tol
0.0005]
Optimize_fmincon_cvg_status/Optimize_fmincon_cvg_status_Report1.report []
Optimize_fmincon_cvg_status/Optimize_fmincon_cvg_status_Report2.report [#2
failed]
Optimize_vf13ad_SolveMode_SaveAndContinue_GMT-4346 []
OREx_Outbound_Cruise_Optimization [diff 0.000606119, tol 0.0005]
OREx_Outbound_Cruise_Optimization_In_FunctionMode [diff
0.000606119, tol 0.0005]
OREx_Outbound_Cruise_Optimization_With_Global_Subscribers_And_Objects
[diff 0.00065214, tol 0.0004]
Simulator_AsteroidOccultation [#1 failed]
THF_Sim_Accel_ConfigD_None_NA_FixedStep [ Observable Error:
0.3425 m.] [FixedStep 1 second, Sim, constant thrust over entire interval,
should it pass]
Thruster_FBurn_Jupiter_ScA_ThrusterE_CS2_TankA [pos err 0.000016]
Thruster_FBurn_Neptune_ScA_ThrusterE_CS2_TankA [pos err 0.000023]
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):
Thruster_Finite_Burn_Permutations_Separate_Propagators_2
[GMT-3455]
Output changes (but still fail) (deferred):
Ephem_GMAT_Code500_InterpolationOrder [pos err 0.0173914, tol
0.002] [GMT-4075, GMT-4112]
Ephem_GMAT_Code500_StepSize [pos err 305.165, tol 0.002]
[GMT-4112]
EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection
[pos err 15.2508, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection
[pos err 9.57601, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect
[pos err 14.3834, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
[pos err 0.000217107, tol 1e-12] [GMT-4112]
EphemStressTests_PD78_ABM_Prop_Code500_60Sec_Step_ForwardDirection [pos err
21.5632, tol 1e-12] [GMT-4112]
GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS [pos err 0.0756285, tol
0.002]
New crashes/hangs/etc. (deferred):
None
New script errors (deferred):
None
New comparator errors (deferred):
None
-----------------------------------------------------------------
Fixed Issues (Deferred)
-----------------------------------------------------------------
Fixed truth failures (deferred):
TrkFile_SimEst_TDRS_range_Solve_Cr [GMT-5416]
Fixed crashes/hangs/etc. (deferred):
None
Fixed script errors (deferred):
None
Fixed comparator errors (deferred):
None
-----------------------------------------------------------------
All Known Issues (Deferred)
-----------------------------------------------------------------
Crashes/hangs/etc. (deferred):
GMAT_LunarTransfer_AllPlanets_DE421_BS
GMAT_MarsTransfer_4_BS
Script errors (deferred):
BatchEstimator_EstimationEpoch [GMT-5708]
Math_Shadowed_Builtins [GMT-3043]
Python_IO_String [5317]
ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522]
THF_Sim_Thrust_CSF2_None_NA_ZeroTSF [GMT-6451]
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]
Achieve_Validation_RHS_Field [no error or exception] [GMT-3687]
BatchEstimator_ReportFile_InitialState [#5 failed] [GMT-6412]
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 15.2508, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection
[pos err 9.57601, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect
[pos err 14.3834, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
[pos err 0.000217107, 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]
Formation_Validation_MissingComma [no error or exception]
[GMT-3672]
GMAT_ISS_Earth_JGM2_0_0_NutationUpdateInterval [pos err
0.00081496, tol 1e-06] [GMT-2567]
GMAT_LEO_PropSynchronization_BS []
GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS [pos err 0.0756285, tol
0.002]
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]
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]
ScriptLanguage_Validation_Semicolons_1 [no error or exception]
[GMT-3545]
SpacecraftNavigation_Validation_Mode [#1 failed] [GMT-5841]
String_AssignNumericParam [] [GMT-2888]
Vary_Validation_RHS_Field [no error or exception] [GMT-3687]
Write_Multiple_ReportFile_Concise_2 [#24 failed] [GMT-5801]
Write_Multiple_ReportFile_Verbose [#24 failed]
Write_Multiple_ReportFile_Verbose_2 [#24 failed] [GMT-5801]
-----------------------------------------------------------------
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_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_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]
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]
SpacecraftNavigation_CdSigma_Range_MSISE86 [GMT-6829 Linux only]
SpacecraftNavigation_SPADDragScaleFactorSigma_GN_MSISE86
[GMT-6829 Linux only]
SpacecraftNavigation_SolveFors_CartesianState_SPADDragScaleFactor_GN_MSISE86
[GMT-6829 Linux only]
THF_AccelMass_CSC_None_None [GMT-5981]
THF_Accel_CSC_None_None [GMT-5981]
THF_ThrustMass_CSC_None_None [GMT-5981]
THF_Thrust_CSC_None_None [GMT-5981]
THF_Thrust_CSC_None_None_2 [GMT-5981]
Thruster_Finite_Burn_Permutations_Separate_Propagators_2
[GMT-3455]
TrkFile_SimEst_TDRS_range_Solve_Cr [GMT-5416]
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