RC1 Issues

Issue and Proposed Solution

Owner

Solution:Status

Debug written by SPICEOrbitKernelReader.cpp causes tests to time out and appear as crashes.

Fix is trivial.  Comment out the debug.

SPH

Done

STKEphemReader rejects Scenario Epochs with precision more than millisecond.

Modify STKEphemerisFile::UTCGregorianToA1ModJulian to handle more precision for setting epoch.

DJC

Committed and ready for a test run

STKEphemReader has issues when reading files with covariance.

Modify reader to ignore covariance.

DJC

Committed and ready for a test run

STKEphemReader assumes DistanceUnit is required but it is not a required field in the STK spec.

Modify the reader so that we do not require DistanceUnit.

DJC

Committed and ready for a test run

Missing test for TESS ephem case

Create a test case and commit that uses a TESS STK ephem.

DJC

Splash screen too big on Mac

Resize the splash screen to be consistent with the size for R2016a.

SPH

Done

Final analysis of Ephem test failures

Verify these are comparator issues.

SPH

Final analysis of navigation failures

DSC/SES

Reverted the SpaceWeather files in the repo and this seems to have corrected the extra failures.

Update ionosphere file.

Put the old file in the appropriate place in the Jazz repo so that it gets used in regression tests.  Then, update the file in mesa-file application with the new version

• Low Thrust is allowed in R2017A but it is not described anywhere in the help.  Thus, most likely, a user would not know to use it, which is probably good since Low Thrust is not fully working yet.  Should it be disabled, by default, in the gmat_startup file?   The user would then only be able to access the feature by setting Run_Mode=TESTING.