Sliding Mode Control of Concomitant Satellites Formation Tracking via STK
This paper considers the formation tracking control problem of concomitant satellites by using STK (Satellite Tool Kit).A new sliding mode control protocol which is suitable to fight against the gravitational perturbation is proposed to achieve the robust tracking around the given orbit.Information flows are able to be translated in STK simulations by using the time-share scheme.The effective of the decoupling approach is tested and verified by STK,which is more meaningful than the results obtained by MATLAB.
Formation Tracking Satellite Tool Kit Sliding Mode Control Concomitant Satellites Decoupling Approach
CHEN Yangyang ZHANG Guoxi FENG Yuan WEI Ping
School of Automation,Southeast University,Nanjing 210096,P. R. China Department of Electronic Information Engineering,Anhui Business College,Wuhu 241002,P. R. China
国际会议
The 33th Chinese Control Conference第33届中国控制会议
南京
英文
344-348
2014-07-28(万方平台首次上网日期,不代表论文的发表时间)