Dear GMAT team, For a project we try to use the Python GMAT API to create a simple Hohmann transfer and receive the coordinates and velocity vectors in 60 second time steps. We have used the example from the API user guide to propagate a simple orbit. However, we couldn't figure out how to create a mission sequence with burn maneuver and there are no examples in the user guide. We would really appreciate any example or direction that could help us.
Thanks in advance. Best regards, David -------------------------- German Aerospace Center (DLR) Galileo Competence Center | Oberpfaffenhofen, Münchener Str. 20 | 82234 Weßling | Germany David Hiebl | Modeling & Simulation Engineer | GK-RBT Telephone +49 8153 28 1843 | david.hi...@dlr.de<mailto:david.hi...@dlr.de> www.DLR.de<http://www.dlr.de/>
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