中国空间科学技术

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圆轨道串行卫星编队的相对运动研究

雪丹;曹喜滨;吴云华;   

  1. 哈尔滨工业大学卫星技术研究所,哈尔滨工业大学卫星技术研究所,哈尔滨工业大学卫星技术研究所 哈尔滨150080,哈尔滨150080,哈尔滨150080
  • 发布日期:2006-10-25

Relative Motion of Leader-follower Formation on Circular Orbit

Xue DanCao XibinWu Yunhua(Research Center of Satellite Technology,Harbin Institute of Technology,Harbin 150080)   

  • Online:2006-10-25

被引次数

2

摘要： 针对圆形轨道串行卫星编队进行研究,推导出满足开普勒轨道假设的相对运动方程,从物理概念上证明了这种描述关系的正确性;并在此基础上利用星间测量信息,设计扩展卡尔曼滤波器进行相对轨道自主确定,仿真结果验证了此相对运动方程与导航方案的有效性。

关键词: 编队飞行, 相对运动, 导航, 圆轨道

Abstract: A group of relative motion equations were given with the Keplerian motion assumption,which was proved to be true in physical concept.On the basis of these equations,an efficient approach for relative navigation of satellites flying in formation through inter-satellite measurements was developed,and an EKF was designed to estimate the orbit states of slave satellite.The simulation results verify the validity of these equations and the navigation method.