J2 Perturbation Effect on the Deployment of Tether-Assisted Deorbit System

摘要：

This paper provides the dynamic model of the deployment of tether-assisted re-entry system includeJ2 perturbation based on Lagrange equation. Some qualitative analyses of J2 perturbation effect on the system are given based on the dynamic model:J2 perturbation effect will induce some offset according to the deployment track of the system. Then a mathematic simulation is provided to validate and analyze the J2 perturbation effect on the deployment of the system in free and exponential deployment scheme. The results showed that J2 perturbation can effect the movement of the system in-plane, but cant induce the movement of the system out-of-plane.

作者: Pengfei Zheng Xibin Cao Shijie Zhang

作者单位: ISSCAA 2008 92 West Dazhi Harbin Institute of Technology,Harbin,150001 China

会议类型: 国际会议

会议名称: The 2nd International Symposium on Systems and Control in Aeronautics and Astronautics(第二届航空航天系统与控制国际会议 ISSCAA 2008)

会议地点: 深圳

会议语种:英文

页码: 796-800

在线出版日期: 2008-12-10（万方平台首次上网日期，不代表论文的发表时间）