Virtual Rendezvous and Docking Control for Fractionated Spacecraft Based on Electromagnetic Force
An alternative actuation system for fractionated spacecraft is to use electromagnetic force without the expenditure of fuel. This paper investigates the novel application of virtual rendezvous and docking for fractionated spacecraft with concepts such as wireless power transfer in mind. Firstly, the magnetic force model and relative motion dynamics are introduced. Then, the feedback control law for circular motion of electromagnetic system is presented, and the control scheme for virtual rendezvous and docking is also proposed. Finally, the numerical simulations are carried out. Simulation results verify that the proposed approach is feasible and effective.
Fractionated Spacecraft Electromagnetic Force Virtual Rendezvous and Docking Feedback Control
Hu Min Zeng Guoqiang Li Zhongwen Yao Hong
Academy of Equipment, Beijing 101416, China Institute of Aerospace and Material Engineering, National University of Defense Technology, Changsha
国际会议
The 31st Chinese Control Conference(第三十一届中国控制会议)
合肥
英文
4670-4673
2012-07-01（万方平台首次上网日期，不代表论文的发表时间）