Model-based Coordination Control of Networked Spacecraft Formations by Integrator Backstepping
In this paper,based on the leader-follower formation architecture,we propose a tracking control scheme for space-craft formation ying in the framework of networked control systems (NCSs)with time-varying network access intervals.A continuous-time representation of the NCS is considered to model the relative translational motion of the follower spacecraft relative to the leader spacecraft.A model-based controller combined with backstepping technique is developed to guarantee uni-formly ultimate boundedness (UUB)of the relative position and velocity tracking errors in the semiglobal sense.The adjustable parameter with respect to which semiglobal UUB is achieved is the network access deadline between transmission times.Nu-merical simulations are presented to demonstrate the effectiveness of the developed controller.
LIU Xi KUMAR K.D.
Department of Aerospace Engineering,Ryerson University,350 Victoria Street Toronto,ON M5B 2K3 Canada
国际会议
The 30th Chinese Control Conference(第三十届中国控制会议)
烟台
英文
1-6
2011-07-01(万方平台首次上网日期,不代表论文的发表时间)