Not sure. A lot of his questions seem to be non-GMAT. I forward to team From: Slojkowski, Steven E. (GSFC-595.0)[OMITRON] <[email protected]> Sent: Wednesday, September 25, 2019 7:45 AM To: Cooley, D S. (GSFC-5950) <[email protected]> Subject: FW: [EXTERNAL] [Gmat-users] Doubts related to Gmat
Does someone handle responding to these messages? From: Bavya Lakshmi <[email protected]<mailto:[email protected]>> Sent: Tuesday, September 24, 2019 7:23 AM To: [email protected]<mailto:[email protected]> Subject: [EXTERNAL] [Gmat-users] Doubts related to Gmat Hi, I was trying to find out the look angle of a satellite with respect to an earth station and used SGP4 propagator where the input element set is NORAD TLE. I want to cross check the result using GMAT and i found out that i need true anomaly and semi major axis as the input which i am not getting from TLE. 1.Is there any way to convert NORAD TLE to SPK kernel file and directly simulate satellite orbit? 2.Is it possible to obtain true anomaly and semi major axis from TLE set? 3.The default window i obtained after installation doesn't have MATLAB under the interface option,but the tutorials show the default window has already MATLAB in it.I attach the screenshot of my default GMAT window i obtained within. Please help me to solve the mentioned problems. Thanks in advance.
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