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SPH

Case By Case Analysis

  • Python_IO_String [5317]:  Will add to deferred list.  We are not going to fix this.
  • Ephem_GMAT_SPK_60sec_target [vel err 0.900016, tol 1e-06]:  Was a quirky edge condition.  Fixed truth data and passes locally.  Expect this will pass in RC2.
  • GMAT_ISS_Earth_0_JR_0_CSSI [pos err 2.73498, tol 0.002]: This will pass as bug GMT-
  • GMAT_ISS_Earth_0_MSISE86_0_CSSI [pos err 0.0463992, tol 0.002]
  • GMAT_ISS_Earth_0_MSISE90_0_CSSI [pos err 0.0125291, tol 0.002]
  • GMAT_ISS_Earth_0_MSISE90_0_CSSI_AssignmentOperator [pos err 0.0125291, tol 0.002]
  • GMAT_ISS_Earth_0_NRLMSISE00_0_CSSI [pos err 0.0123784, tol 0.002]
  • GMAT_UserMoon-Titan_AllPlanets_SRP_AboutAsteroid [pos err 5569.14, tol 0.002] [GMT-5262]:   Investigating.  I don't understand this yet. This has switched from passing to failing recently.
  • GMAT_UserMoon-Titan_AllPlanets_SRP_AboutComet [pos err 5569.14, tol 0.002] [GMT-5262]: Investigating.  I don't understand this yet. This has switched from passing to failing recently.
  • ScriptLanguage_Validation_FilePaths_3 [no error or exception]:  This is a false positive in my opinion.  It tests if files that have "`" character at beginning and end of a filename are invalid.  We do not trap it, but correctly write data the filename specified.  So I deleted the test and so it should not fail in RC2.
  • SolarSystem_Bug2437 [max diff 2.09863e-12 > tol 1e-12max diff 1e-12 > tol ]:  Fixed the tolerance. Should not fail in RC2. 

Summary

This test keeps Thruster_Finite_Burn_Permutations_Separate_Propagators_VNB_2 sometimes passes and sometimes fails in the nightly.  It passes locally for me and Darrel, and passed in RC1.   Not sure what to do but keep an eye on it.

JJKP

Case By Case Analysis

  • FindEvents_ControlFlow_While [GMT-5361]
  • DensityParam_Validation_Disabled_AtmosDensity [no error or exception]
  • FMParams_Validation_Disabled_Acceleration [no error or exception]
  • FMParams_Validation_Disabled_AccelerationX [no error or exception]
  • FMParams_Validation_Disabled_AccelerationY [no error or exception]
  • FMParams_Validation_Disabled_AccelerationZ [no error or exception]
  • Ephem_GMAT_SPK_60sec_backward [failed reading state 1/15 from SPK] [GMT-5286]
  • Ephem_GMAT_SPK_DefaultIntegrationStep_User_Defined_LagrangeOrder [failed reading state 1/19 from SPK] [GMT-5286]
  • Events_ContactLocator_EarthTransit [diff # events]
  • Events_ContactLocator_OccultingBodies_Multiple [diff # events]
  • Events_EclipseLocator_MarsLong [start diff = 0.001006s (mars/9)]
  • Events_TESS_Optimize_TwoStage_FromLaunch_master_03b4b32/Events_ContactLocator_TESS.report [start diff = 3.279996s (event 2125)]
  • Events_TESS_Optimize_TwoStage_FromLaunch_master_03b4b32/Events_EclipseLocator_TESS.report [start diff = 1.161993s (earth/15)]
  • FindEvents_ControlFlow_For [diff occ bodies] [GMT-5360]
  • FindEvents_ControlFlow_Target [diff # events for earth]

Summary

RQ

Case By Case Analysis

GMATFunction_ACE_impulsive_493_Global_Subscribers_User_Defined_Parameters       

Summary

 

              

 

             

 

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