Motion Camouflage for In-orbit Maneuvers

摘要：

A strategy for trajectory design, motion camouflage, is introduced within the context of orbital relative motion. At first the equations of orbital motion for this approach are developed. The control strategy is then implemented using both an impulsive and continuous approach. A number of parameters are then optimized to minimize the fuel mass. The simulation results reveal that the predator successfully reaches the target and thus proving the validity of this approach.

作者: Tao Yang Gianmarco Radice Weihua Zhang

作者单位: Astronautics and Material Engineering,National University of Defense Technology,410073,Chang Sha,Hu Department of Aerospace Engineering,University of Glasgow,Glasgow G12 8QQ,United Kingdom. College of Astronautics and Material Engineering,National University of Defense Technology,410073,Ch

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: 442-447

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）