Autonomous Navigation Based on Stellar Refraction for Elliptic Orbit Spacecraft

摘要：

This paper proposes a novel method based on stellar refraction to create a dynamic stellar catalogue for autonomous navigation and presents a principle of stellar choosing. Then, through the unscented Kalman filter, it analyses the applicability and the navigational accuracy that uses the stellar refraction method on the elliptic orbit spacecraft. The simulation results demonstrate that the proposed method and principle are simple and utility; the autonomous navigation method based on stellar refraction still has good applicability for elliptic orbit.

作者: Haiyan Yang Xueying An Jie Wu Guojian Tang

作者单位: College of Aerospace and Material Engineering,National University of Defense Technology,Changsha 410 College of Aerospace and Material Engineering,National University of Defense Technology,Changsha 410

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 1029-1032

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）