中国空间科学技术2016，Vol.36Issue(3)：77-84,8.DOI:10.16708/j.cnki.1000-758X.2016.0037
GEO 卫星基于电推进系统的倾角与偏心率联合控制方法
Incl ination and eccentricity combination control method using electric propulsion for GEO satel l ite stationkeeping
李强 1周志成 1袁俊刚 1王敏1
作者信息
- 1. 中国空间技术研究院 通信卫星事业部，北京 100094
- 折叠
摘要
Abstract
Nowadays most advanced GEO satellites collocate electric thrusters with high specific impulse to execute north-south stationkeeping, which can efficiently decrease propellant consumption. For GEO satellites, electric thrusters usually controls nothing but inclination,whi le bipropellant thruster controls eccentricity and mean longitude.Aiming at the stationkeeping of GEO satellite with electric thruster,a sort of combination control method of inclination and eccentricity using electric thrusters was proposed.The optimization model for solving the control equations was developed. Two kinds of simplified algorithm were induced by reducing the optimization model dimensionality, which deeply decrease the computational complexity and was convenient for autonomous computation of GEO satellite stationkeeping.This method can be used to simulate the combined inclination and eccentricity simultaneously and precisely, which leads to the reduction of propellant consumption for stationkeeping.The simulation results indicate that the combination control method has the advantages of high stationkeeping efficiency and high control precision.关键词
GEO 卫星/位置保持/电推进系统/倾角控制/偏心率控制/联合控制Key words
GEO satellite/stationkeeping/electric propulsion system/inclination control/eccentricity control/combination control分类
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李强,周志成,袁俊刚,王敏..GEO 卫星基于电推进系统的倾角与偏心率联合控制方法[J].中国空间科学技术,2016,36(3):77-84,8.
