Revision: 10198
http://gmat.svn.sourceforge.net/gmat/?rev=10198&view=rev
Author: wendys-dev
Date: 2012-02-03 20:39:51 +0000 (Fri, 03 Feb 2012)
Log Message:
-----------
- Added method to determine first time of coverage for celestial bodies
- Added code to set initial epoch in ODEModel to first time of coverage
- Added debug
Fixes Bug 2437 - SPK data needed for J2000 epoch even when not used in mission
(GMT-80)
Modified Paths:
--------------
trunk/src/base/forcemodel/ODEModel.cpp
trunk/src/base/forcemodel/ODEModel.hpp
trunk/src/base/forcemodel/PhysicalModel.cpp
trunk/src/base/solarsys/CelestialBody.cpp
trunk/src/base/solarsys/CelestialBody.hpp
trunk/src/base/util/SpiceOrbitKernelReader.cpp
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