A new tracking control method for synchronization of spacecraft formation with switching topologies

摘要：

　　This paper studies an attitude synchronization problem for spacecraft formation with switching interaction topologies.An adaptive control architecture which allows for parameter uncertainties and unknown external disturbances is established for the decentralized controllers design.This paper also shows that the attitude synchronization under dynamically changing interaction topologies can be achieved asymptotically if the union of the switching communication graphs is jointly connected in a finite time interval.Finally,some simulations indicate the capabilities of the proposed results.

关键词： Spacecraft formulation attitude synchronization adaptive control switching topology

作者: Ling Zhao Xiu You Fuchun Sun Zhixin Liu Hongjiu Yang

作者单位: Hebei Province Key Laboratory of Heveay Machinery Fluid Power Transmission and Control,College of Me Institute of Electrical Engineering,Yanshan University,Qinhuangdao 066004,China Department of Computer Science and Technology,Tsinghua University,Beijing 10084,P.R.China

会议类型: 国际会议

会议名称: The 33th Chinese Control Conference第33届中国控制会议

会议地点: 南京

会议语种:英文

页码: 1208-1213

在线出版日期: 2014-07-28（万方平台首次上网日期，不代表论文的发表时间）