-----------------------------------------------------------------
Summary
-----------------------------------------------------------------
System configuration: Windows 7/MATLAB R2017a/VS 2013
Tested build: 2018-02-09
Regression build: 2018-02-08

Total number of scripts: 13845 (+134 deferred)
Percent Passed: 99.95%
New issues: 30
        Output changes: 30
        New truth failures: 0
        New crashes: 0
        New script errors: 0
        New comparator errors: 0
Fixed issues: 0
Total issues: 7

Test system warnings: 49
New deferred issues: 14
Fixed deferred issues: 1
Total deferred issues: 104

Run Time: 11 hours, 14 minutes, 33 seconds

-----------------------------------------------------------------
New Issues
-----------------------------------------------------------------
New truth failures:
        None

Output changes (but still pass):
        BatchEstimator_OLSEUseRMSP_False_DSN
        BatchEstimator_OLSEUseRMSP_False_DsnSeqRange
        BatchEstimator_OLSEUseRMSP_False_DsnTcp
        BatchEstimator_OLSEUseRMSP_False_GN
        BatchEstimator_OLSEUseRMSP_False_Range
        BatchEstimator_OLSEUseRMSP_False_RangeRate
        Ephem_GMAT_Code500_CoordinateSystem
        Ephem_GMAT_Code500_ManeuverAtEnd
        Ephem_GMAT_Code500_TimeInteractions
        Ephem_GMAT_Code500_WriteEphemeris
        Ephem_GMAT_STK_60sec
        Ephem_GMAT_STK_60sec_if_loop
        Ephem_GMAT_STK_60sec_IterativeProcess_Optimizer [GMT-6090]
        Ephem_GMAT_STK_60sec_IterativeProcess_Optimizer_NoBoundaries [GMT-6090]
        Ephem_GMAT_STK_60sec_meters
        Ephem_GMAT_STK_60sec_NoEvents
        Ephem_GMAT_STK_60sec_with_600secFB
        Ephem_GMAT_STK_OEM_60sec_with_1DV_IB
        EphemerisFile-STK-IncludeEventBoundariesFalse
        EphemerisFile-STK-IncludeEventBoundariesTrue
        EphemerisFile_Code500_LeapSecond_2d_1sec
        
EphemStressTests_Default_Prop_STK_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_ForwardDirection
 [GMT-6090]
        
EphemStressTests_Default_Prop_STK_60Sec_MixedStopTypes_LogicTypes_DiscontinuityTypes_SolverTypes_ForwardDirect
 [GMT-6090]
        Ex_FirstVersionNumericSettings
        GroundStation_Tropo_Marini_DsnSeqRange_Est
        GroundStation_Tropo_Marini_DsnTcp_Est
        GroundStation_Tropo_Marini_Range_Est
        GroundStation_Tropo_Marini_RangeRate_Est
        SNOPT_OverrideSpecsFile
        SNOPT_SpecsFile

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.:
        CallPythonFunction_Validation_InvalidOutputs_WrongSizeArray_4

Script errors:
        SpacecraftNavigation_SolveFors_KeplerianState_Cd_Cr_RangeRate:
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\scriptTest\gmat\output\SpacecraftNavigation_SolveFors_KeplerianState_Cd_Cr_RangeRate.txt
 does not exist
        SpacecraftNavigation_SolveFors_KeplerianState_Cd_GN:
                ERROR MESSAGE: Output file
C:\Users\gsfc580gmattest\Documents\scriptTest\gmat\output\SpacecraftNavigation_SolveFors_KeplerianState_Cd_GN.txt
 does not exist

Comparator errors:
        GMT-6055-GMATFunctionLargeArrayCrash: (reg)
     ERROR MESSAGE: Undefined function
'comparator.FileDiffComparator.Compare' for input arguments of type
'char'. 

Truth failures:
        BatchEstimator_ReportFile_InitialState [#5 failed] [GMT-6412]
        Optimize_Yukon_Minimize_Height_on_circle_2 [diff 497, tol 0.001]
        Optimize_Yukon_Minimize_Height_on_circle_4 [diff 497, tol 0.001]

-----------------------------------------------------------------
New Issues (Deferred)
-----------------------------------------------------------------
New truth failures (deferred):
        None

Output changes (but still pass) (deferred):
        Ephem_GMAT_Code500_StepSize [GMT-4112]
        ErrorModel_Bias_GpsPosVec2
        StatisticsAcceptFilter_DataTypes_GpsPosVec
        StatisticsRejectFilter_DataTypes_GpsPosVec

Output changes (but still fail) (deferred):
        Ephem_GMAT_Code500_InterpolationOrder [pos err 0.0173914, tol 0.002]
[GMT-4075, GMT-4112]
        Ephem_GMAT_Code500_InterpolationOrder [pos err 0.0463976, tol 0.002]
[GMT-4075, GMT-4112]
        Ephem_GMAT_Code500_StepSize [pos err 305.165, tol 0.002] [GMT-4112]
        
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_ForwardDirection
 [pos err 0.000200836, 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]
        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_RangeRate [The 
test
run failed to converge] [GMT-5954]

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):
        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
        THF_Sim_Accel_ConfigD_None_NA_2 [GMT-5986]
        THF_Sim_Accel_ConfigD_None_NA_3 [GMT-5986]
        THF_Sim_Accel_ConfigD_None_NA_4 [GMT-5986]
        THF_Sim_Accel_ConfigD_None_NA [GMT-5986]
        TrkFile_SimEst_DSN_DS_Range_Solve_Bias_apriori [GMT-5709]
        TrkFile_SimEst_GN_RangeRate_Solve_Cd
        TrkFile_SimEst_GN_RangeRate_Solve_Cr
        TrkFile_SimEst_GN_range_Solve_Cd
        TrkFile_SimEst_GN_range_Solve_Cr

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_ACE_OpsPrototype_v13 [pos err 2.31993, tol 1]
[GMT-4112]
        
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 14.3796, tol 1e-12] [GMT-4077]
        
EphemStressTests_Default_Prop_Code500_60Sec_MixedStopTypes_LogicTypes_ForwardDirection
 [pos err 0.000200836, 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_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_BS [pos err
0.00234382, tol 0.0023]
        
GMAT_ISS_EarthSunLuna_EGM96_MSISE90_SRP_SolidAndPoleTide_Max_Reduction_BS
[pos err 0.00234382, tol 0.0023]
        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]
        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]
        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)
        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]
        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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