Adaptive Pose Tracking Control for On-orbit Tumbling Target Spacecraft

摘要：

　　It is assumed in this paper that the service spacecraft perform autonomous rendezvous and proximity operation to a tumbling target in space. Under this background, this paper proposes a relative coupled position and attitude dynamics. Using a Lyapunov framework, an adaptive controller is designed with the mass property of the service spacecraft uncertain. Numerical simulation is finally provided to illustrate the performance of the proposed controller.

关键词： autonomous rendezvous pose coupling dual quaternion mass property adptive control

作者: Ying Chen Siyuan Rong Shunli Li Chen He

作者单位: School of Astronautics Harbin Institute of Technology Harbin, China

会议类型: 国际会议

会议名称: 2015 Fifth International Conference on Instrumentation and Measurement,Computer,Communication and Control (IMCCC2015)(第五届仪器测量、计算机通信与控制国际会议)

会议地点: 秦皇岛

会议语种:英文

页码: 1972-1976

在线出版日期: 2015-09-18（万方平台首次上网日期，不代表论文的发表时间）