Revision: 10127
http://gmat.svn.sourceforge.net/gmat/?rev=10127&view=rev
Author: wendys-dev
Date: 2012-01-05 18:33:29 +0000 (Thu, 05 Jan 2012)
Log Message:
-----------
- Corrected code so that anomaly type is correctly set to "TA" (since that is
currently the only allowed value)
- Changed code to display saved values instead of the current text values for
state, to avoid changing values on "Apply"
------> Fixes Bug 2686 - Error message for not being able to convert state from
Cartesian to Keplerian is confusing
Modified Paths:
--------------
trunk/src/gui/spacecraft/OrbitPanel.cpp
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