Relative Motion Model of Satellites Formation Flying Base on the Influence of the J2 Perturbation

摘要：

Cluster of formation flying satellites consists of several companion satellites that make relative motion to a central satellite. The trajectory of relative motion is ellipse with special properties. On secular flying of formation satellites, various perturbation factors may cause relative drifts to the satellites. J2 perturbation has a great effect on the satellites formation flying. The article addresses a linearized relative motion equation. Considering the impact of the J2 perturbation on secular drift of relative motion, An relative motion model of elliptical reference orbit is developed. The simulation results show that the equation can predict the relative motion of satellite formation flying precisely.

作者: Pan Ligong Feng Zhuren Li Ganhua Han Minzhang

作者单位: Xian Jiaotong University,Xian,710049,China Xian Satellite Control Center,Xian,710043,China Xian Jiaotong University,Xian,710049,China Xian Satellite Control Center,Xian,710043,China

会议类型: 国际会议

会议名称: 2009 IEEE International Conference on Robotics and Biomimetics(2009 IEEE 机器人与仿生技术国际会议 ROBIO 2009)

会议地点: 桂林

会议语种:英文

页码: 308-313

在线出版日期: 2009-12-19（万方平台首次上网日期，不代表论文的发表时间）