Driving Celestia from an external propagator
Posted: 19.07.2007, 02:30
I'm new to the Celestia forum, and I am trying to find out if anyone has ever used an external orbit propagator to generate spacecraft orbit ephemeris for Celestia to display. I'm interested in using Celestia as a display option for a software system I've been working on for about five years now. Some background, I am an aerospace engineer at NASA's Goddard Space Flight Center and work on trajectory design software (we'll be releasing the system under the NASA Open Source Agreement soon). I'm not a developer, I write mathematical specifications and algorithms, design user interfaces, and use the software to solve problems, among other things...
The software we are developing is called GMAT (General Mission Analysis System). One of the capabilities of GMAT is to propagate spacecraft orbits, and dynamically update 2-D and OpenGL plots dynamically as the orbits are numerically integrated. Not knowing Celestia's architecture, I was wondering if the design supports this or could support this with a reasonable amount of work.
Thanks for the help. When we release GMAT I'll be sure to post a message here.
Steve
The software we are developing is called GMAT (General Mission Analysis System). One of the capabilities of GMAT is to propagate spacecraft orbits, and dynamically update 2-D and OpenGL plots dynamically as the orbits are numerically integrated. Not knowing Celestia's architecture, I was wondering if the design supports this or could support this with a reasonable amount of work.
Thanks for the help. When we release GMAT I'll be sure to post a message here.
Steve