*RESENDING, This time with the right outputs!**
*
The attached results are a run of GMAT R2017a (Feb 27 build, which
matches the release and includes the internal plugins) using MATLAB
R2018b, requested by Steve S. GMAT R2018a was built using MATLAB
R2017b, so this is a validation test of a GMAT R2018a/MATLAB R2018b Red
Hat configuration.
- DJC
--
Darrel J. Conway, Ph.D. Thinking Systems, Inc.
Senior Scientist and CEO 6441 N Camino Libby
Phone: (623) 298-4530 Tucson, AZ 85718
FAX: (520) 232-2533 www.thinksysinc.com
Cell: (520) 425-3626 [email protected]
-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: RHEL_7.2
Tested build: RHEL_GMAT_Console
Regression build: RHELBaseline
Total number of scripts: 13741 (+97 deferred)
Percent Passed: 99.95%
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: 7
Test system warnings: 43
New deferred issues: 0
Fixed deferred issues: 0
Total deferred issues: 92
Run Time: 08 hours, 46 minutes, 32 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:
None
Comparator errors:
None
Truth failures:
BatchEstimator_InversionAlgorithm_Cholesky [diff 0.000114567, tol
0.00011diff 1e-07, tol ]
BatchEstimator_RelativeTol_Range_RangeRate [#1 failed]
Optimize_Yukon_Minimize_Height_on_circle_2 [diff 497, tol 0.001]
Optimize_Yukon_Minimize_Height_on_circle_4 [diff 497, tol 0.001]
SpacecraftNavigation_CdSigma_Range_MSISE86 [#1 failed]
Write_Spacecraft_MultipleObjects [#12 failed]
Write_Spacecraft_Thruster [#10 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):
All_in_One_STEREO
All_in_One
BatchEstimator_EstimationEpoch [GMT-5708]
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
Estimate_LEO_PointMass_USNTwoWayRange_LightTimeOnly_NonPerturbedIC
Estimate_LEO_PointMass_USNTwoWayRange_LightTimeOnly_PerturbedIC
Math_Shadowed_Builtins [GMT-3043]
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
Python_IO_String [5317]
ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522]
Simulate_DeepSpace_DSNTwoWayRange_LT_GR_Transponder_RampTable
Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_GR_RampTable
Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable_2
Simulate_DeepSpace_DSNTwoWayRange_LightTimeOnly_RampTable
Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly_Ramp
Simulate_LEO_DSNTwoWayDoppler_LightTimeOnly_Zero_Ramp
Simulate_LEO_DSNTwoWayRange_LightTimeOnly_RampTable
Simulate_LEO_USNTwoWayRange_LightTime-Bias
Simulate_LEO_USNTwoWayRange_LightTimeOnly
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 0.0200021, 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
305.166, tol 0.002] [GMT-4112]
EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection
[pos err 15.2507, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection
[pos err 9.57663, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect
[pos err 14.3819, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
[pos err 0.000200011, 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 0.00081572, 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]
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_SolveFors_CartesianState_LeapSec_Range [Parameter
TDRS10.EarthTODEq.X error 2.248285 exceeds tolerance 0.010000] [GMT-5954]
SpacecraftNavigation_SolveFors_CartesianState_LeapSec_RangeRate
[Parameter Aura.EarthMJ2000Eq.X error 1.965657 exceeds tolerance 0.010000]
[GMT-5954]
SpacecraftNavigation_SolveFors_KeplerianState_LeapSec_Range [Parameter
TDRS10.EarthTODEq.X error 2.248283 exceeds tolerance 0.010000] [GMT-5954]
SpacecraftNavigation_SolveFors_KeplerianState_LeapSec_RangeRate [The
test run failed to converge] [GMT-5954]
SpacecraftNavigation_Validation_Mode [#1 failed] [GMT-5841]
StatisticsRejectFilter_DataTypes_All [#1 failed]
StatisticsRejectFilter_DataTypes_DsnSeqRange [#2 failed]
StatisticsRejectFilter_DataTypes_DsnTcp [#1 failed]
StatisticsRejectFilter_ObservedObjects_All [#3 failed]
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 [#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)
BatchEstimator_InversionAlgorithm_Internal_Singular [GMT-6395]
BatchEstimator_InversionAlgorithm_Schur_Singular [GMT-6395]
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]
ErrorModel_NoiseSigma_RangeRate2 [GMT-5417]
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_L1_DsnSeqRange_SOHO_AncillaryElements [GMT-6040]
SpacecraftNavigation_L1_DsnSeqRange_SOHO_CovarianceCorrelationMatrix
[GMT-6040]
SpacecraftNavigation_L1_DsnSeqRange_SOHO_EstimatedState [GMT-6040]
SpacecraftNavigation_SolveFors_CartesianState_Cd_GN [GMT-4128]
SpacecraftNavigation_SolveFors_CartesianState_EarthFixed [GMT-6408]
SpacecraftNavigation_SolveFors_KeplerianState_EarthFixed [GMT-6408]
Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
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