Sliding Mode Control of Concomitant Satellites Formation Tracking via STK

摘要：

　　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.

关键词： Formation Tracking Satellite Tool Kit Sliding Mode Control Concomitant Satellites Decoupling Approach

作者: CHEN Yangyang ZHANG Guoxi FENG Yuan WEI Ping

作者单位: School of Automation,Southeast University,Nanjing 210096,P. R. China Department of Electronic Information Engineering,Anhui Business College,Wuhu 241002,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: 344-348

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）