中国科技核心期刊

中文核心期刊

CSCD来源期刊

空间控制技术与应用 ›› 2013, Vol. 39 ›› Issue (5): 39-42.doi: 10.3969/j.issn.1674-1579.2013.05.008

• 技术交流 • 上一篇    下一篇

基于离子推进技术的轨道转移设计

  

  • 出版日期:2013-10-25 发布日期:2013-10-28

Design for OrbitTransfer Based on Ion Propulsion

  • Online:2013-10-25 Published:2013-10-28

摘要: 将太阳能离子推力器应用于卫星的推进系统,完成从地球同步转移轨道(GTO)到地球同步轨道(GEO)转移任务;建立任务模型,设计基于纬度幅角的反馈控制策略,对发动机开关时间进行优化.采用图形处理器(GPU, graphic processing unit)加速的遗传算法(GA,genetic algorithm)对卫星转移轨道任务进行优化设计.仿真结果表明:通过对该闭环控制器的定常参数进行优化,可将轨道导引至目标轨道附近;采用太阳能离子推力器可减少燃料消耗.基于GPU加速的遗传算法,可缩短算法运算时间.

关键词: 离子推力器, 轨道转移, GPU加速遗传算法

Abstract: Solar energy ion thruster is applied to achieve satellite orbittransfer from the earth synchronous transfer orbit (GTO) to geosynchronous orbit (GEO). The control strategy is designed via the feedback of latitude amplitude, and the ion thruster on/off time is optimized. The genetic algorithm (GA) based on graphic processing unit (GPU) is applied to optimize the transfer orbit. The results show that the closedloop controller completes the orbittransfer task. The fuel consumption of solar energy ion thruster is fairly less than that of the chemical fuel. Genetic algorithm based on GPU can greatly shorten the operating time.

Key words: ion thrust, orbittransfer, genetic algorithm based on graphic processing unit

中图分类号: 

  • V412.41