Test system results from last night.
These results are from a master build, with the STK propagator updates
folded in. On the STK propagator side, this one:
EphemPropagator_STK_Filter_Mnvr [pos err 0.00123461, tol 3e-06]
was a surprise, so I'll look into it. (We are still working truth data
for the TESS .e files, so it might just be something there.)
Steve S -- I packaged this build. Do you want the tarball?
- 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 d...@thinksysinc.com
-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: RHEL_7.2
Tested build: RHEL_GMAT_Console
Regression build: RHELBaseline
Total number of scripts: 13529 (+88 deferred)
Percent Passed: 99.73%
New issues: 4
Output changes: 0
New truth failures: 3
New crashes: 0
New script errors: 0
New comparator errors: 1
Fixed issues: 19
Total issues: 37
Test system warnings: 43
New deferred issues: 0
Fixed deferred issues: 0
Total deferred issues: 61
Run Time: 07 hours, 50 minutes, 11 seconds
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
EphemPropagator_STK_EphemCompare_LeapSecond [Output field 333.230000
failed tolerance in record 3602]
SpacecraftNavigation_CrSigma_DsnTcp [#1 failed]
SpacecraftNavigation_SolveFors_CartesianState_EarthFixed [The test run
failed to converge]
Output changes (but still pass):
None
Output changes (but still fail):
None
New crashes/hangs/etc.:
None
New script errors:
None
New comparator errors:
EphemTest_DE405_Moon_Neptune (truth)
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
BatchEstimator_ReportFile_CovarianceCorrelationMatrix
BatchEstimator_ReportFile_StateInformation
SpacecraftNavigation_SolveFors_CartesianState_Cd_Cr_GN
TrackingFileSet_UseAllCorrections_DsnTcp_Est
TrackingFileSet_UseAllCorrections_DsnTcp_Sim
TrackingFileSet_UseETminusTAI_Range_Est
TrackingFileSet_UseETminusTAI_RangeRate_Est
TrackingFileSet_UseLightTime_DsnSeqRange_Est
TrackingFileSet_UseLightTime_DsnTcp_Est
TrackingFileSet_UseLightTime_Range_Est
TrackingFileSet_UseLightTime_Range_RangeRate_Est
TrackingFileSet_UseLightTime_RangeRate_Est
TrackingFileSet_UseRelativityCorrection_DsnSeqRange_Est
Fixed crashes/hangs/etc.:
None
Fixed script errors:
Transmitter_Frequency_DSN_Doppler_DeepSpace_2
Transmitter_Frequency_DSN_Doppler_DeepSpace
Transmitter_Frequency_DSN_Range_DeepSpace_2
Transmitter_Frequency_DSN_Range_DeepSpace
TrkFile_SimEst_DSN_DS_Range_Solve_Inc_RAAN_apriori
TrkFile_SimEst_DSN_DS_Range_Solve_RAAN_apriori
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
None
Script errors:
None
Comparator errors:
EphemTest_DE405_Moon_Neptune: (truth)
ERROR MESSAGE: Comparator PVComparator failed: Error using fileread (line
26)
Could not open file
/home/buildbot/jazz/test/script/input/Resources/FRR-16_SolarSystem/truth/RotationDataSource_Deprecation_Warning.txtEphemTest_DE405_Moon_Neptune.truth.
No such file or directory.
Truth failures:
EphemPropagator_STK_EphemCompare_LeapSecond [Output field 333.230000
failed tolerance in record 3602]
EphemPropagator_STK_Filter_Mnvr [pos err 0.00123461, tol 3e-06]
EphemPropagator_STK_VelocityDiscontinuity [pos err 0.00639492, tol
1e-06]
ForceModel_Validation_TideFile [#1 failed]
ForceModel_Validation_TideFile_ZeroTideModel [#1 failed]
ForceModel_Validation_TideModel [#1 failed]
Integrator_LEO_PD853_Accuracy []
Integrator_NoErrorControl_Warning [#1 failed]
Simulator_MoonOccultation [GMAT: 11299 lines, Truth: 11306 lines]
[GMT-6134]
SpacecraftNavigation_CrSigma_DsnTcp [#1 failed]
SpacecraftNavigation_SolveFors_CartesianState_EarthFixed [The test run
failed to converge]
SpacecraftNavigation_SolveFors_KeplerianState_Cd_Cr_GN [Parameter
EstSat.EarthMJ2000Eq.AOP value 62.335799 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_Cd_Cr_Range [Parameter
EstSat.EarthMJ2000Eq.AOP value 62.340586 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_Cd_Cr_RangeRate
[Parameter EstSat.EarthMJ2000Eq.AOP value 62.335227 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_Cd_GN [Parameter
EstSat.EarthMJ2000Eq.AOP value 62.336294 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_Cd_Range [Parameter
EstSat.EarthMJ2000Eq.AOP value 62.332306 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_Cd_RangeRate [Parameter
EstSat.EarthMJ2000Eq.AOP value 62.336466 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_Cr_DSN [Parameter
EstSat.EarthMJ2000Eq.RAAN value 63.521781 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_Cr_GN [Parameter
EstSat.EarthMJ2000Eq.AOP value 62.336450 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_Cr_Range [Parameter
EstSat.EarthMJ2000Eq.AOP value 62.337331 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_DSN [Parameter
EstSat.EarthMJ2000Eq.AOP value 62.336071 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_DSN_GEO [Parameter
EstSat.EarthMJ2000Eq.AOP value 338.503074 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_DSN_Moon [Parameter
EstSat.MoonMJ2000Eq.MA value 259.008020 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_DSN_Sun [Parameter
EstSat.SunMJ2000Eq.X value -130354491.716972 exceeds tolerance 0.500000]
SpacecraftNavigation_SolveFors_KeplerianState_DsnSeqRange_L1 [Parameter
EstSat.EarthMJ2000Eq.SMA value 847184.798576 exceeds tolerance 0.001000]
SpacecraftNavigation_SolveFors_KeplerianState_DsnSeqRange_L2 [Parameter
EstSat.EarthMJ2000Eq.SMA value 917322.817890 exceeds tolerance 0.001000]
SpacecraftNavigation_SolveFors_KeplerianState_EarthFixed [The test run
failed to converge] [GMT-6394]
SpacecraftNavigation_SolveFors_KeplerianState_EarthTODEq [Parameter
EstSat.EarthTODEq.AOP value 62.337282 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_GN [Parameter
EstSat.EarthMJ2000Eq.AOP value 62.336626 exceeds tolerance 0.000100]
SpacecraftNavigation_SolveFors_KeplerianState_LeapSec_Range [Parameter
TDRS10.EarthTODEq.X value -11597.448674 exceeds tolerance 0.010000] [GMT-5954]
SpacecraftNavigation_SolveFors_KeplerianState_LeapSec_RangeRate [The
test run failed to converge] [GMT-5954]
SpacecraftNavigation_SolveFors_KeplerianState_RangeRate [Parameter
EstSat.EarthMJ2000Eq.AOP value 62.336230 exceeds tolerance 0.000100]
TrackingFileSet_ChebyshevDEBoundary_1day [ Observable Error: 0.0002632
Hz]
TrackingFileSet_ChebyshevDEBoundary_1hour [ Observable Error: 0.8751 Hz]
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):
GMAT_LunarTransfer_AllPlanets_DE421_BS
GMAT_MarsTransfer_4_BS
Script errors (deferred):
BatchEstimator_EstimationEpoch [GMT-5708, GMT-5701]
Math_Shadowed_Builtins [GMT-3043]
Python_IO_String [5317]
ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522]
TrkFile_SimEst_DSN_DS_Range_Solve_Bias_apriori [GMT-5709]
TrkFile_SimEst_GN_RangeRate_Solve_Cd [GMT-5701]
TrkFile_SimEst_GN_RangeRate_Solve_Cr [GMT-5701]
TrkFile_SimEst_GN_range_Solve_Cd [GMT-5701]
TrkFile_SimEst_GN_range_Solve_Cr [GMT-5701]
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]
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]
GMAT_LEO_PropSynchronization_BS []
GMAT_LunarTran_PropSynchronization_BS [max diff 2.79401e-07 > tol 5e-08]
GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS [pos err 0.0748552, tol 0.002]
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_Propagator_EarthPointMass_Drag/Simulator_Propagator_EarthPointMass_Drag_PosErr.report
[diff 0.0310455, tol 4e-05] [GMT-5417]
Simulator_Propagator_EarthPointMass_SRP_Drag/Simulator_Propagator_EarthPointMass_SRP_Drag_PosErr.report
[diff 0.0437413, tol 5e-05] [GMT-5417]
SpacecraftNavigation_SolveFors_CartesianState_LeapSec_Range [Parameter
TDRS10.EarthTODEq.X value -11597.448774 exceeds tolerance 0.010000] [GMT-5954]
SpacecraftNavigation_SolveFors_CartesianState_LeapSec_Range [Parameter
TDRS10.EarthTODEq.X value -11597.448774 exceeds tolerance 0.010000] [GMT-5954]
SpacecraftNavigation_SolveFors_CartesianState_LeapSec_RangeRate
[Parameter Aura.EarthMJ2000Eq.X value -4277.420299 exceeds tolerance 0.010000]
[GMT-5954]
SpacecraftNavigation_SolveFors_CartesianState_LeapSec_RangeRate
[Parameter Aura.EarthMJ2000Eq.X value -4277.420299 exceeds tolerance 0.010000]
[GMT-5954]
SpacecraftNavigation_Validation_Mode [#1 failed] [GMT-5841]
String_AssignNumericParam [] [GMT-2888]
THF_Sim_Accel_ConfigD_None_NA [ Observable Error: 0.3426 m.] [GMT-5986]
THF_Sim_Accel_ConfigD_None_NA_2 [ Observable Error: 739.3 m.] [GMT-5986]
THF_Sim_Accel_ConfigD_None_NA_3 [ Observable Error: 0.2607 m.]
[GMT-5986]
THF_Sim_Accel_ConfigD_None_NA_4 [ Observable Error: 0.04548 m.]
[GMT-5986]
TrkFile_SimEst_TDRS_range_Solve_Cr [] [GMT-5416, GMT-5701]
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_STK_CentralBody_Moon_Meters [GMT-6093]
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_Code500_ACE_OpsPrototype_v13 [GMT-4112]
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_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]
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]
------------------------------------------------------------------------------
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