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First International Conference on Innovative Computing, Information and Control - Volume I (ICICIC'06)
Design and Simulation of Autonomous Control System of Satellite
Beijing, China
August 30-September 01
ISBN: 0-7695-2616-0
Zhang Yulin, Tsinghua University
Analyzed the influence of main perturbation sources including non-spherical gravitational perturbation, atmospheric drag perturbation and third body gravitation perturbation to the satellite orbit, compensates the influence through the method that biased the semi-major axis and the inclination angle, which enhanced the orbital stability of satellite. Designed the satellite autonomous orbital control system, and discussed the method that through controlling the semi-major axis, the eccentricity and the inclination angle to complete the revisions to ascending node right ascension deviation and phase deviation. Finally through the simulation and the experiment of a satellite which running on nearly earth regression, circular orbit, simulation results indicated the system scheme satisfied the demand of satellite autonomous control.
Citation:
Xiang Junhua, Zhang Yulin, "Design and Simulation of Autonomous Control System of Satellite," icicic, vol. 1, pp.109-112, First International Conference on Innovative Computing, Information and Control - Volume I (ICICIC'06), 2006
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