According to the structural characteristics of satellite formation, and using the kinematic equations which expressed as fly-around form, designed a model for satellite formation configuration, analysed the relationship between fly-around parameters and the orbital elements, designed a method that meets the mission requirements of the satellite formation configuration, formulated a corresponding operation flow chart, listed several typical satellite formations of simple configuration and complex configuration. Finally, according to the general process of configuration design, obtaioned a configuration based on the requirments, and with the help of software STK and Matlab performed a formation configuration simulation that considering collision avoidance verification and adjustment. The simulation results show that the formation configuration design process and design method are basically right.
Based on STK and Matlab Satellite Formation's Configuration Design and Simulation
2013
6 Seiten
Aufsatz (Konferenz)
Englisch
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