After yesterday's GMAT meeting, I compiled GMAT locally and ran the entire
suite of regression tests. (not sure how Steve H and Tuan fared in their work
to fix the automated system)
The results are not bad. Steve S, can you take a look at the SPAD failures?
Thanks,
Steve
-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Windows 10/MATLAB R2017b/TestBuild
Tested build: Master Sep 6
Regression build: $prevbuild$
Total number of scripts: 13814 (+51 deferred)
Percent Passed: 99.96%
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: 5
Test system warnings: 34
New deferred issues: 0
Fixed deferred issues: 0
Total deferred issues: 45
Run Time: 12 hours, 42 minutes, 04 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.:
None
Script errors:
AttitudeProp_CCSDS_EulerAngle:
ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\Builds\GMAT-R2018a-Windows-x64\output\AttitudeProp_CCSDS_EulerAngle.report
does not exist
Comparator errors:
None
Truth failures:
Sphere_SPAD_J2000OffSetAttitude_EarthSPAD [GMAT: 1 lines, Truth:
101 lines]
Sphere_SPAD_J2000OffSetAttitude_EarthSPAD_CommandMode [GMAT: 1
lines, Truth: 101 lines]
Sphere_SPAD_J2000OffSetAttitude_EarthSPAD_ScaleFactor [GMAT: 1
lines, Truth: 101 lines]
Sphere_SPAD_J2000OffSetAttitude_EarthSPAD_WholeObjectAssignment
[GMAT: 1 lines, Truth: 101 lines]
-----------------------------------------------------------------
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]
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 15.2466, 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]
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]
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]
Simulator_MoonOccultation [GMAT: 11299 lines, Truth: 11306
lines] [GMT-6134]
SpacecraftNavigation_Validation_Mode [#1 failed] [GMT-5841]
String_AssignNumericParam [] [GMT-2888]
TrkFile_SimEst_TDRS_range_Solve_Cr [] [GMT-5416]
Vary_Validation_RHS_Field [no error or exception] [GMT-3687]
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)
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]
Thruster_Finite_Burn_Permutations_Separate_Propagators_2
[GMT-3455]
------------------------------------------------------------------------------
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