DensityParam_Validation_Disabled_AtmosDensity [no error or exception] - obsolete; deleted
FMParams_Validation_Disabled_Acceleration [no error or exception] - obsolete; deleted
FMParams_Validation_Disabled_AccelerationX [no error or exception] - obsolete; deleted
FMParams_Validation_Disabled_AccelerationY [no error or exception] - obsolete; deleted
FMParams_Validation_Disabled_AccelerationZ [no error or exception] - obsolete; deleted
FindEvents_ControlFlow_While [GMT-5361] - fixed, shortened test and updated tolerance
Ephem_GMAT_SPK_60sec_backward [failed reading state 1/15 from SPK] [GMT-5286] - the 2nd state isn't being read
Ephem_GMAT_SPK_DefaultIntegrationStep_User_Defined_LagrangeOrder [failed reading state 1/19 from SPK] [GMT-5286] - the 2nd state isn't being read
Events_ContactLocator_EarthTransit [diff # events] - fixed truth data
Events_ContactLocator_OccultingBodies_Multiple [diff # events] - corrected script SPK consistency issue & updated truth
Events_EclipseLocator_MarsLong [start diff = 0.001006s (mars/9)] - updated tolerance
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)] - updated tolerance
FindEvents_ControlFlow_For [diff occ bodies] [GMT-5360]
FindEvents_ControlFlow_Target [diff # events for earth]

Summary

Looked through all tests; closed the checked ones above.
For the SPK tests, the first and last state are being thrown out, so this is an error reading the second state. Need some sanity checking on the generated ephems.
TESS ContactLocator tess failed by 3s, on the order as seen by other high-orbit tests. Regenerated truth data using Matlab. Test takes a long time to run, so waiting to confirm.
ControlFlow_For is a multi-chunked report that the comparator seems to have trouble with. Will verify manually.
ControlFlow_Target may just be a bad test - it fails because there aren't enough points in the last iteration to write a valid ephem segment.

RQ

GMATFunction_ACE_impulsive_493_Global_Subscribers_User_Defined_Parameters

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