Development of Mission and Spacecraft Dynamics Analysis System for Geostationary Communication Satellite

Details Development of Mission and Spacecraft Dynamics Analysis System for Geostationary Communication Satellite Development of Mission and Spacecraft Dynamics Analysis System for Geostationary Communication Satellite

Jun 1998

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1998jass...15..251g&link_type=abstract

Journal of Astronomy and Space Sciences, vol. 15, no. 1, p. 251-260.

Astronomy and Astrophysics

Astronomy

Scientific paper

We consider the motion of the subsystems as separate bodies as well as the entire satellite for the attitude and orbit control of a communication satellite by multi-body modeling technique. Thus, the system can be applied to a general communication satellite as well as a specific communication satellite, i.e. Koreasat I, II. The simulation results can be viewed by two-dimensional graphics and three-dimensional animation. The graphical user interface (GUI) makes its usage much simpler. We have simulated a couple of scenarios for Koreasat I, II which are being operated as geostationary communication satellites to verify the system performance.

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