The most recent test system results (Red Hat), Dev build.
- DJC
--
Darrel J. Conway, Ph.D. Thinking Systems, Inc.
Senior Scientist and CEO 437 W Thurber Road, Suite 6
Phone: (623) 298-4530 Tucson, AZ 85705
FAX: (520) 232-2533www.thinksysinc.com
Cell: (520) [email protected]
-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: RedHatEnterpriseWorkstation7.9
Tested build: RedHatEnterpriseWorkstation7.9-GMAT_Console
Regression build: RedHatEnterpriseWorkstation7.9Baseline
Total number of scripts: 16363 (+123 deferred)
Percent Passed: 99.11%
New issues: 3
Output changes: 0
New truth failures: 0
New crashes: 3
New script errors: 0
New comparator errors: 0
Fixed issues: 2
Total issues: 165
Test system warnings: 49
New deferred issues: 0
Fixed deferred issues: 0
Total deferred issues: 101
Run Time: 01 hours, 44 minutes, 18 seconds
-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
None
Output changes (but still pass):
None
Output changes (but still fail):
None
New crashes/hangs/etc.:
BatchEstimator_OLSEAdditiveConstant_DSN_GN
Epoch_AssignmentMode_MultEpochFormat
SpacecraftNavigation_LEO_GpsPosVec_Fermi_EstimatedState
New script errors:
None
New comparator errors:
None
-----------------------------------------------------------------
Fixed Issues
-----------------------------------------------------------------
Fixed truth failures:
API_ScriptTest (API)
Fixed crashes/hangs/etc.:
GroundStation_Tropo_Marini_XEastYNorth_DeepSpace
Fixed script errors:
None
Fixed comparator errors:
None
-----------------------------------------------------------------
All Known Issues
-----------------------------------------------------------------
Crashes/hangs/etc.:
*BatchEstimator_OLSEAdditiveConstant_DSN_GN
*Epoch_AssignmentMode_MultEpochFormat
*PropOffEphem_Backward_SPK
*PropOffEphem_Forward_SPK
*SpacecraftNavigation_LEO_GpsPosVec_Fermi_EstimatedState
Script errors:
*CustomFOV_FOVFileName_AzimuthElevationAngles:
*CustomFOV_FOVFileName_StkFormatMask:
EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_SPICE: [GMT-7483]
EKFS_ThrustSegment_SolveFors_ThrustScaleFactor_SN: [GMT-7376]
EphemPropagator_SPK_CentralBody_Moon_PA: [GMT-7606]
EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_SPICE: [GMT-7483]
*Events_ContactLocator_IntervalStepSize_0sec:
*Events_ContactLocator_IntervalStepSize_60sec:
*Events_ContactLocator_ReportColumnsInOrder_Observer_Multiple_Many:
*Events_ContactLocator_ReportColumnsInOrder_Observer_Multiple:
*Events_ContactLocator_StationMaskingAndMinimumElevation:
Events_ContactLocator_StationMasking_CeresBase: [GMT-7614]
*Events_ContactLocator_StationMasking_CustomFOVIsNotClosed:
*Events_ContactLocator_StationMasking_Lunar:
*Events_ContactLocator_StationMasking_MarsBase:
*Events_ContactLocator_StationMasking_MaskFileIsNotClosed:
*Events_ContactLocator_StationMasking_MoonBase:
Events_ContactLocator_StationMasking_MultipleFOV: [GMT-7614]
Events_ContactLocator_StationMasking_Multiple_Many: [GMT-7614]
*Events_ContactLocator_StationMasking_RunMode_Disabled:
Events_ContactLocator_StationMasking_RunMode_Manual_Append: [GMT-7614]
*Events_ContactLocator_StationMasking_RunMode_Manual:
*Events_ContactLocator_StationMasking:
*GroundStation_HorizonMaskFileName_FormatCompressed:
*GroundStation_HorizonMaskFileName_FormatTabbed:
*GroundStation_HorizonMaskFileName_MacLineEndings:
*GroundStation_HorizonMaskFileName_MoonBase:
*GroundStation_HorizonMaskFileName_StkFormat:
*GroundStation_HorizonMaskFileName_UnixLineEndings:
*GroundStation_HorizonMaskFileName:
KalmanFilter_Smoother_PredictTimeSpan_Both_OEM: [GMT-6949]
MatAPI_PrecessingSpinner: (MatAPI) [GMT-7595]
*SpacecraftNavigation_IOD_Gibbs_GEO_SDO:
*SpacecraftNavigation_IOD_Gibbs_LEO_ISS:
*SpacecraftNavigation_IOD_HerrickGibbs_GEO_SDO:
*SpacecraftNavigation_IOD_HerrickGibbs_LEO_ISS:
*SpacecraftNavigation_IOD_IODFunctions:
*SpacecraftNavigation_IOD_NotCoplanar:
*SpacecraftNavigation_IOD_SpecifyMu:
*SpacecraftNavigation_IOD_Vallado:
Comparator errors:
CustomFOV_FOVFileName_ClockConeAngles: (truth) [GMT-7614]
EphemerisFile_OEM_CoordinateSystem_LocalAlignedConstrained_Disallowed:
(truth) [GMT-7598]
EphemerisFile_OEM_Earth_TOD_WriteDisallowed: (truth) [GMT-7598]
PlanetographicRegion_Validation_LatValueMissing: (truth) [GMT-7699]
Propagate_Covariance_SNC_EarthMoonSun_Synchronized: (truth) [GMT-7687]
Propagate_Covariance_SNC_EarthMoonSun_Synchronized: (truth) [GMT-7687]
Propagate_Covariance_SNC_EarthMoonSun_Synchronized: (truth) [GMT-7687]
Propagate_Covariance_SNC_EarthMoonSun_Unsynchronized: (truth) [GMT-7687]
Propagate_Covariance_SNC_EarthMoonSun_Unsynchronized: (truth) [GMT-7687]
Propagate_Covariance_SNC_EarthMoonSun_Unsynchronized: (truth) [GMT-7687]
Truth failures:
API_PrecessingSpinner (API) [#1 failed] [GMT-7595]
*API_ScriptFunctions (API) [#16 failed]
BatchEstimator_Propagator_OEM_EarthFixed_GN [Residual failed at 01 Mar
2005 02:20:50.000] [GMT-7598]
BatchEstimator_Propagator_OEM_TDRS_Multiple_EarthFixed [The test run
failed to converge] [GMT-7598]
BatchEstimator_Propagator_OEM_TOD_GN [Residual failed at 01 Mar 2005
01:00:00.000] [GMT-7598]
BatchEstimator_Propagator_STK_TDRS_Multiple_EarthFixed [Parameter
EstSat.EarthMJ2000Eq.X error 0.099521 exceeds tolerance 0.005000] [GMT-7289]
*BatchEstimator_ReportStyle_Verbose_MultiSat_SpaceToSpace [#177 failed]
ContactLocator_PlanetoRegion_Square [start diff = 61.882002s (event 3)]
[GMT-7699]
*CustomFOV_El_GreaterThan90 [#3 failed]
*CustomFOV_InterpolationStepSize_1deg [diff # events]
*EKF_ProcessNoiseModel_UpdateTimeStep_60sec/EKF_ProcessNoiseModel_UpdateTimeStep_60sec_Prop.txt
[Output field 0.042317 failed tolerance in record 620]
*EKFS_EphemerisFile_STK_PredDv/EKFS_EphemerisFile_STK_PredDv_Filter.e
[CovarianceTimePos failed tolerance at row 27652]
*EKFS_EphemerisFile_STK_PredDv/EKFS_EphemerisFile_STK_PredDv_Smoother.e
[CovarianceTimePos failed tolerance at row 27652]
EKFS_ErrorModel_SolveFors_Bias_RandomConstant_GN/EKFS_ErrorModel_SolveFors_Bias_RandomConstant_GN_Smoother_backfilter.txt
[Parameter EstMAD.EstSat_EstRangeModel.Bias error 0.118138 exceeds tolerance
0.020000] [GMT-7434-Linux]
*EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_Filter.e
[CovarianceTimePos failed tolerance at row 17161]
*EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_Smoother.e
[CovarianceTimePos failed tolerance at row 17161]
*EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_SmoEph/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_WarmStart_PredDv_SmoEph_Smoother.e
[CovarianceTimePos failed tolerance at row 17161]
EKFS_SpacecraftNavigation_OrbitErrorCovariance_GN_Moon [Failed to find
a covariance record at 10 Sep 2005 00:00:00.000] [GMT-6801]
*EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantTSF_DSN/EKFS_SpacecraftNavigation_ProcessNoiseModel_RandomConstantTSF_DSN_FPS.mat
[Covariance comparison failed tolerance at 7 of 14 significant digits at index
(7,6,349)]
EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr/EKFS_SpacecraftNavigation_Sun_DSN_STEREOB_Cr_Smoother_backfilter.txt
[Parameter STEREO_B.SunMJ2000Eq.X error 0.177174 exceeds tolerance 0.015000]
[GMT-7278-Linux]
EKFS_ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_GpsPosVec/EKFS_ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_GpsPosVec_Smoother_backfilter.txt
[Parameter FM.Est_Thruster1_SetPoint1.ThrustAngle1.C0 error 14.780763 exceeds
tolerance 0.005000] [GMT-7483]
EphemerisFile_SPK_GetEphemStates_Sun_MJ2000Ec [Output field
94210467.402783 failed tolerance in record 1] [GMT-7602]
*EphemerisFile_STK_LeapSecond_2d_60sec [EphemerisTimePosVel failed
velocity magnitude tolerance at row 2]
EphemPropagator_OEM_CentralBody_Earth_TODEq/EphemPropagator_OEM_CentralBody_Earth_TODEq_EarthTODRpt.txt
[pos err 8.21702, tol 2e-06] [GMT-7589]
EphemPropagator_OEM_CentralBody_Earth_TODEq/EphemPropagator_OEM_CentralBody_Earth_TODEq_EarthJ2000Rpt.txt
[pos err 8.21702, tol 2e-06] [GMT-7589]
EphemPropagator_OEM_CentralBody_Earth_TODEq/EphemPropagator_OEM_CentralBody_Earth_TODEq_SunJ2000Rpt.txt
[pos err 8.21655, tol 0.0005] [GMT-7589]
EphemPropagator_OEM_CentralBody_Mars_MJ2000Eq/EphemPropagator_OEM_CentralBody_Mars_MJ2000Eq_EarthJ2000Rpt.txt
[pos err 0.000950917, tol 1e-06] [GMT-7598]
EphemPropagator_OEM_CentralBody_Sun_MJ2000Eq/EphemPropagator_OEM_CentralBody_Sun_MJ2000Eq_BodyFixedRpt.txt
[pos err 0.102575, tol 0.0001] [GMT-7598]
EphemPropagator_OEM_CentralBody_Sun_MJ2000Eq/EphemPropagator_OEM_CentralBody_Sun_MJ2000Eq_EarthJ2000Rpt.txt
[pos err 0.102725, tol 0.0005] [GMT-7598]
EphemPropagator_OEM_CentralBody_Sun_MJ2000Eq/EphemPropagator_OEM_CentralBody_Sun_MJ2000Eq_BodyJ2000Rpt.txt
[pos err 0.10259, tol 5e-08] [GMT-7598]
EphemPropagator_OEM_Earth_GRC_60sec [pos err 9.36262e+08, tol 1.2e-05]
[GMT-7563]
EphemPropagator_OEM_Earth_ICRF_60sec [pos err 0.00181204, tol 1.2e-05]
[GMT-7563]
EphemPropagator_OEM_Sun_60sec [pos err 0.00181207, tol 1e-05] [GMT-7598]
EphemPropagator_SPK_CentralBody_Earth_MJ2000Eq/EphemPropagator_SPK_CentralBody_Earth_MJ2000Eq_EarthJ2000Rpt.txt
[pos err 0.00127621, tol 5e-06] [GMT-7606]
EphemPropagator_SPK_CentralBody_Earth_MJ2000Eq/EphemPropagator_SPK_CentralBody_Earth_MJ2000Eq_SunJ2000Rpt.txt
[pos err 0.00575362, tol 0.0001] [GMT-7606]
EphemPropagator_SPK_CentralBody_Earth_MJ2000Eq_BackProp/EphemPropagator_SPK_CentralBody_Earth_MJ2000Eq_BackProp_EarthJ2000Rpt.txt
[pos err 0.00128938, tol 5e-06] [GMT-7606]
EphemPropagator_SPK_CentralBody_Earth_MJ2000Eq_BackProp/EphemPropagator_SPK_CentralBody_Earth_MJ2000Eq_BackProp_SunJ2000Rpt.txt
[pos err 0.00580238, tol 0.0001] [GMT-7606]
EphemPropagator_SPK_CentralBody_Moon_MJ2000Eq/EphemPropagator_SPK_CentralBody_Moon_MJ2000Eq_BodyFixedRpt.txt
[pos err 0.00060908, tol 5e-05] [GMT-7606]
EphemPropagator_SPK_CentralBody_Moon_MJ2000Eq/EphemPropagator_SPK_CentralBody_Moon_MJ2000Eq_BodyJ2000Rpt.txt
[pos err 0.00061091, tol 1e-06] [GMT-7606]
EphemPropagator_SPK_CentralBody_Moon_MJ2000Eq/EphemPropagator_SPK_CentralBody_Moon_MJ2000Eq_EarthJ2000Rpt.txt
[pos err 0.00102931, tol 5e-05] [GMT-7606]
EphemPropagator_SPK_HasGap/EphemPropagator_SPK_HasGap_EarthFixedRpt.txt
[GMAT: 1381 lines, Truth: 1380 lines] [GMT-7602]
EphemPropagator_SPK_HasGap/EphemPropagator_SPK_HasGap_EarthJ2000Rpt.txt
[GMAT: 1381 lines, Truth: 1380 lines] [GMT-7602]
EphemPropagator_SPK_HasGap/EphemPropagator_SPK_HasGap_SunJ2000Rpt.txt
[GMAT: 1381 lines, Truth: 1380 lines] [GMT-7602]
EphemPropagator_SPK_LeapSecond/EphemPropagator_SPK_LeapSecond_60sec.txt
[Output field 01 Jul 2012 00:00:00.000 did not match truth field 30 Jun 2012
23:59:60.000] [GMT-7602]
Events_ContactLocator_StationMasking_ClockConeAngles [start diff =
23.276991s (event 28)] [GMT-7614]
*Events_ContactLocator_StationMasking_DeepSpace [diff # events]
*Events_ContactLocator_StationMasking_DeepSpace_LightTimeDirection_Transmit
[diff # events]
*Events_ContactLocator_StationMasking_DeepSpace_UseLightTimeDelay_False
[diff # events]
*Events_ContactLocator_StationMasking_DeepSpace_UseStellarAberration_False
[diff # events]
*Events_IntrusionLocator_SingleIntrudingBody_LightTimeDelay_StellarAberration
[diff # events]
*Events_IntrusionLocator_SingleIntrudingBody_MultipleSensors_FixedGrid
[diff # events]
*ForceModel_Validation_NoSPKforUserBody [no error or exception]
*GMAT_Mars1_Mars_0_MarsGRAM2005_0_NonDefaultF107 [pos err 0.000406033,
tol 0.0003]
*GroundStation_Validation_HorizonMaskFileName [#7 failed]
KalmanFilter_MatlabFile_GN_Moon [Variable EstimationConfig.StateNames
did not match at index 1] [GMT-6801]
MatAPI_Epoch_LeapSecond_In (MatAPI) [#7 failed] [2561]
MatAPI_Epoch_LeapSecond_Out (MatAPI) [#7 failed] [2561]
*MatAPI_LoadAndRunScript (MatAPI) [#3 failed]
*MatAPI_MJ2000Ec (MatAPI) [#6 failed]
*MatAPI_MJ2000Eq (MatAPI) [#12 failed]
*MatAPI_PD45PropagationE8x8SMPM (MatAPI) [pos err 0.000753373, tol
1e-07]
*MatAPI_ScriptFunctions (MatAPI) [#16 failed]
*MatAPI_ScriptTest (MatAPI) [#2 failed]
Plate_Validation_PlateNormalHistoryFile [#1 failed] [GMT-7022]
*ProcessNoiseModel_Validation_UpdateTimeStep [#8 failed]
*Propagate_Covariance_FilterSmoother_Ephemeris_STK_CovPosition/Propagate_Covariance_FilterSmoother_Ephemeris_STK_CovPosition_Filter.e
[CovarianceTimePos failed tolerance at row 10476]
*Propagate_Covariance_FilterSmoother_Ephemeris_STK_CovPosition/Propagate_Covariance_FilterSmoother_Ephemeris_STK_CovPosition_Smoother.e
[CovarianceTimePos failed tolerance at row 10283]
*Propagate_Covariance_FilterSmoother_Ephemeris_STK_CovPositionVelocity/Propagate_Covariance_FilterSmoother_Ephemeris_STK_CovPositionVelocity_Filter.e
[CovarianceTimePosVel failed tolerance at row 32916]
*Propagate_Covariance_FilterSmoother_Ephemeris_STK_CovPositionVelocity/Propagate_Covariance_FilterSmoother_Ephemeris_STK_CovPositionVelocity_Smoother.e
[CovarianceTimePosVel failed tolerance at row 32303]
*Propagate_Covariance_SNC_EarthMJ2000Eq_Backward [max diff 6.28317e-09
> tol 1e-10]
*Propagate_Covariance_SNC_MoonMJ2000Eq_Moon [max diff 2.7979e-10 > tol
1e-10]
*Propagate_Covariance_SNC_None_EarthFull [max diff 4.69849e-08 > tol
1e-10]
*Propagate_Covariance_SNC_None_MoonFull [max diff 1.94056e-10 > tol
1e-10]
Propagate_Covariance_SNC_SunGSE_Sun [Output field 2.078945 failed
tolerance in record 3459] [GMT-7687]
Propagate_Covariance_SNC_SunMJ2000Ec_Sun [Output field 0.918693 failed
tolerance in record 1729] [GMT-7687]
RotationMatrixTest_MercuryMJ2000Ec [max diff 1.09735e-09 > tol 1e-12]
[GMT-7223]
Simulator_Propagator_OEM_EarthFixed_GN [Failed to find a Range residual
record at 01 Mar 2005 02:20:50.000] [GMT-7598]
Simulator_Propagator_OEM_MoonMJ2000Eq_GN [Residual failed at 10 Jun
2011 04:00:00.000] [GMT-7289]
Simulator_Propagator_OEM_TOD_GN [Residual failed at 01 Mar 2005
01:00:00.000] [GMT-7598]
Simulator_Propagator_SPK_MoonOccultation [#66 failed] [GMT-7289]
Simulator_Propagator_SPK_MultipleOccultation [#1 failed] [GMT-7289]
Simulator_Propagator_SPK_TDRS [Residual failed at 01 Mar 2005
01:00:00.000] [GMT-7289]
Simulator_Propagator_STK_TDRS [Residual failed at 01 Mar 2005
01:00:00.000] [GMT-7289]
*Smoother_Filter_ProcessNoiseTimeStep_0sec_SN [Sigma-V failed at 01 Mar
2005 21:28:00.000]
Smoother_MatlabFile_BackfilterMatfileCorruption [Found extra field
BackwardComputed] [GMT-6949]
Spacecraft_Validation_AddPlates [#1 failed] [GMT-7022]
*SpacecraftNavigation_IOD_ChooseGibbs_LEO [Found 3 output records and 4
truth records]
*SpacecraftNavigation_IOD_ChooseGibbs_LEO [#1 failed]
*SpacecraftNavigation_IOD_ChooseHerrickGibbs_LEO [Found 3 output
records and 4 truth records]
*SpacecraftNavigation_IOD_ChooseHerrickGibbs_LEO [#1 failed]
*SpacecraftNavigation_IOD_Gibbs_Cislunar [#4 failed]
*SpacecraftNavigation_IOD_Gibbs_GEO [Found 3 output records and 4 truth
records]
*SpacecraftNavigation_IOD_Gibbs_LEO [Found 3 output records and 4 truth
records]
*SpacecraftNavigation_IOD_Gibbs_LEO_FullFM [Found 3 output records and
4 truth records]
*SpacecraftNavigation_IOD_HerrickGibbs_Cislunar [Found 3 output records
and 4 truth records]
*SpacecraftNavigation_IOD_HerrickGibbs_GEO [#4 failed]
*SpacecraftNavigation_IOD_HerrickGibbs_GEO_FullFM [#4 failed]
*SpacecraftNavigation_IOD_HerrickGibbs_LEO [Found 3 output records and
4 truth records]
*SpacecraftNavigation_IOD_OutOfTimeOrder [#1 failed]
*SpacecraftNavigation_IOD_Verbose_SpecifyGibbs [#1 failed]
*SpacecraftNavigation_IOD_Verbose_SpecifyHerrickGibbs [#1 failed]
SpacecraftNavigation_LEO_TDRS_EphProp_OEM_LeapSec_Terra [Residual
failed at 31 Dec 2016 23:55:00.000] [GMT-7598]
SpacecraftNavigation_MultiSat_J2000_EarthFixed [Residual failed at 01
Mar 2005 01:00:00.000] [GMT-7421]
SpacecraftNavigation_SimEphProp_MixedInitialFrame_TDRS [Residual failed
at 01 Mar 2005 01:20:00.000] [GMT-7289]
SpacecraftNavigation_SPADSRPScaleFactorSigma_ConstrainInc [#3 failed]
[GMT-7078, Linux only]
*THF_Validation_EndThrustMissing [#1 failed]
*THF_Validation_InvalidRecordData [#1 failed]
ThrustSegment_SolveFors_ThrustAngles_Constant_Spinner_EpochAfterBurn_GpsPosVec
[The test run failed to converge] [GMT-7483]
ThrustSegment_SolveFors_ThrustAngles_Constant_ThreeAxisKinematic_EpochAfterBurn_GpsPosVec
[The test run failed to converge] [GMT-7483]
*ThrustSegment_SolveFors_ThrustAngles_SN [Parameter
EstSat.EarthMJ2000Eq.VZ error 0.000002 exceeds tolerance 0.000001]
-----------------------------------------------------------------
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]
EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_DuringEstimationArc_CCSDS
[GMT-7483]
EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_DuringEstimationArc_SPICE
[GMT-7483]
EKFS_ErrorModel_SolveFors_PassBiases_GN
EKFS_SpacecraftNavigation_LEO_TDRS_Aqua_FogmCd [GMT-7376]
EKFS_SpacecraftNavigation_MultiSat_TdrsAndUser_DifferentProcessNoise
[GMT-7421]
EKFS_SpacecraftNavigation_MultiSat_TdrsAndUser
EKFS_SpacecraftNavigation_Multisat_AquaTD6_Cd
EKF_SpacecraftNavigation_OrbitErrorCovariance_Keplerian_GpsPosVec
EKF_SpacecraftNavigation_SolveFors_KeplerianState_Cd_RandomConstant_GN
EKF_SpacecraftNavigation_SolveFors_KeplerianState_Cr_RandomConstant_DSN
EKF_SpacecraftNavigation_SolveFors_KeplerianState_GN
EKF_SpacecraftNavigation_SolveFors_KeplerianState_GpsPosVec
KalmanFilter_InputWarmStartFile_GN_Moon_Keplerian [GMT-6801]
KalmanFilter_InputWarmStartFile_GpsPosVec_KeplerianToCartesian
[GMT-6801]
KalmanFilter_OutputWarmStartFile_GpsPosVec_Keplerian [GMT-6801]
KalmanFilter_Propagator_Multiple_MixedCentralBody [GMT-7421]
KalmanFilter_Propagator_Multiple_SunEarthMoon [GMT-7421]
KalmanFilter_Propagator_SN
KalmanFilter_Propagator_SPK_TDRS_Multiple
KalmanFilter_Propagator_SPK_TDRS
KalmanFilter_Propagator_STK_TDRS_Multiple
KalmanFilter_Propagator_STK_TDRS
Math_Shadowed_Builtins [GMT-3043]
OCPropTest_SPAD_Drag_1deg_Bicubic_LEO [GMT-7147]
OCPropTest_SPAD_Drag_SRP_1deg_Bicubic_LEO [GMT-7147]
ScriptLanguage_WhiteSpace_AfterArrayName [GMT-3522]
THF_Sim_Accel_ConfigD_None_NA_2 [GMT-6451]
THF_Sim_Accel_ConfigD_None_NA_3 [GMT-6451]
THF_Sim_Accel_ConfigD_None_NA_4 [GMT-6451]
THF_Sim_Accel_ConfigD_None_NA [GMT-6451]
THF_Sim_Thrust_CSF2_None_NA_ZeroTSF [GMT-6451]
ThrustHistoryFile_EstimateTSF_EpochBeforeBurn_RSSStep_Aqua [GMT-6451]
ThrustSegment_SolveFors_ThrustScaleFactor_Multiple_RSSStep [GMT-6451]
ThrustSegment_SolveFors_ThrustScaleFactor_RSSStep [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_NormalMatrixReduction_UseInitialCovariance [#1 failed]
[GMT-7274]
BatchEstimator_ReportFile_InitialState [#1 failed]
EKFS_EphemerisFile_FiniteBurnTHF_DuringEstimationArc_CCSDS_Disallowed
[#1 failed]
EKFS_EphemerisFile_FiniteBurnTHF_DuringEstimationArc_SPICE_Disallowed
[#1 failed]
EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_DuringEstimationArc_STK/EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_DuringEstimationArc_STK_Smoother.e
[Unable to read STK ephemeris
/home/buildbot/jazz/test/script/output/RedHatEnterpriseWorkstation7.9-GMAT_Console/Resources/FRR-31_EphemerisFile/script/EKFS_EphemerisFile_FiniteBurnTHF_EphemerisSegmentation_DuringEstimationArc_STK_Smoother.e]
[GMT-7483]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond_Filter.e
[EphemerisTimePosVel failed epoch tolerance at row 988] [GMT-7291, GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond_Smoother.e
[EphemerisTimePosVel failed epoch tolerance at row 988] [GMT-7291, GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond_Filter.mat
[Found extra field CartesianStateNames] [GMT-7291, GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond_Smoother.mat
[Found extra field CartesianStateNames] [GMT-7291, GMT-7398]
EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond/EKFS_SpacecraftNavigation_LEO_GpsPosVec_Fermi_FOGM_Cd_ADSF_LeapSecond.tab
[Output field 0.000751 failed tolerance in record 575] [GMT-7291, GMT-7398]
EKFS_SpacecraftNavigation_MultiSat_DifferentInitialEpochs [#1 failed]
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]
EphemPropagator_STK_CentralBody_Moon_ME/EphemPropagator_STK_CentralBody_Moon_ME_BodyJ2000Rpt.txt
[pos err 138.57, tol 1e-06] [GMT-7604]
EphemPropagator_STK_CentralBody_Moon_ME/EphemPropagator_STK_CentralBody_Moon_ME_EarthJ2000Rpt.txt
[pos err 138.57, tol 5e-05] [GMT-7604]
EphemStressTests_Default_and_ABM_Integrator_Code500_60Sec_MultipleSCs_ForwardDirection
[pos err 15.2546, 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 14.3171, tol 1e-12] [GMT-4077]
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
[pos err 0.000219127, 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 0.000808928,
tol 1e-06] [GMT-2567]
GMAT_LEO_PropSynchronization_BS []
GMAT_LunarTran_PropSynchronization_BS [max diff 3.05778e-07 > tol 5e-08]
GMAT_Molniya_EarthSunLuna_JGM2_JR_SRP_BS [pos err 0.0761958, tol 0.002]
GroundStation_Tropo_TRK223_DsnTcp_OREX/GroundStation_Tropo_TRK223_DsnTcp_OREX.txt
[Residual failed at 02 Feb 2021 09:25:00.000] [GMT-7455]
KalmanFilter_InputWarmStartFile_SN [Output field -4638.170949 failed
tolerance in record 1] [GMT-7376]
KalmanFilter_Propagator_Multiple_NonParticipatingSpacecraft [ptrn 1
failed]
KalmanFilter_Propagator_Multiple_SpacecraftDoesNotExist [ptrn 1 failed]
KalmanFilter_Propagator_Multiple_UnassignedSpacecraft [ptrn 1 failed]
KalmanFilter_WarmStartEpoch_SN [Output field -4638.170949 failed
tolerance in record 1] [GMT-7376]
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_LiteralArrays_String [] [GMT-3680]
ScriptLanguage_ReferenceArrays_ForceModel_7 [] [GMT-3541]
ScriptLanguage_Validation_Semicolons_1 [no error or exception]
[GMT-3545]
Smoother_PredictTimeSpan_STK_SN [Test ScenarioEpoch does not match
truth ScenarioEpoch] [GMT-7376]
SpacecraftNavigation_Validation_Mode [#1 failed] [GMT-5841]
String_AssignNumericParam [] [GMT-2888]
ThrustSegment_ThrustAngle1_Cubic [diff. num. lines] [GMT-7483]
TrackingFileSet_InconsistentSpacecraftState [Output field
-1254560.770370 failed tolerance in record 1] [GMT-7553]
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)
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_OEM_Usable_Start_Stop [GMT-7563]
EphemPropagator_STK_CentralBody_Sun_Fixed [GMT-7594]
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]
Events_TESS_Optimize_TwoStage_FromLaunch_master_03b4b32 [GMT-7629]
Ex_GmatFunction [GMT-3604]
FMParams_GMAT_UserAsteroid(OSIRIS)_HarmonicGravity_SRP_PointMasses
[GMT-6955]
ForceModel_SPAD_Drag_1deg_Bicubic_Mars [Linux, Mac]
ForceModel_SPAD_Drag_1deg_Bilinear_Mars [Linux, Mac]
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]
IntegratedFlyby_MarsFlyby [GMT-7169]
KalmanFilter_TimeUpdate_GpsPosVec [GMT-6801]
MatAPI_Functions [GMT-7597]
Math_Validation_Cross_WrongDim2 [GMT-5676]
Phase_EpochFormat_TAIGregorian [GMT-7168]
Phase_Type_Radau [GMT-7168]
ProcessNoiseModel_UpdateTimeStep_10sec [GMT-7687]
Python_IO_String [5317]
ScriptLanguage_LineContinuation_BeginningOfLine [GMT-3756]
ScriptLanguage_Validation_DataTypes_ReferenceArray_Formation_5
[GMT-6064]
Simulator_Propagator_EarthPointMass_Drag [GMT-5417]
SpacePointParams_CelestialBody_EpochOutput [3939]
SpacecraftNavigation_CdSigma_Range_MSISE86 [GMT-6829 Linux only]
SpacecraftNavigation_SPADDragScaleFactorSigma_ConstrainInc [GMT-7078,
Ubuntu only]
SpacecraftNavigation_SPADDragScaleFactorSigma_GN_MSISE86 [GMT-6829
Linux only]
SpacecraftNavigation_SolveFors_CartesianState_SPADDragScaleFactor_GN_MSISE86
[GMT-6829 Linux only]
Thruster_Finite_Burn_Permutations_Separate_Propagators_2 [GMT-3455]
Tut_MultipleShootingTutorial_Step3 [GMT-7280]
Write_Spacecraft_NavigationHardware [GMT-7578]
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