Integral Sliding Mode Fault-Tolerant Control for Spacecraft With Uncertainties and Saturation
详细信息    查看全文
  • 作者:Duan Wenjie ; Wang Dayi and Liu Chengrui
  • 刊名:Asian Journal of Control
  • 出版年:2017
  • 出版时间:January 2017
  • 年:2017
  • 卷:19
  • 期:1
  • 页码:372-381
  • 全文大小:1542K
  • ISSN:1934-6093
文摘
An integral sliding mode fault-tolerant control method is proposed to deal with faults with matched uncertainties, unmatched uncertainties, and input saturation. Integral sliding mode, control allocation, and parameter identification are included in this method. The Lyapunov stability conditions of the integral sliding mode control for uncertainties and input saturation, respectively, are obtained, which denote the robustness extent of the controller. The direct method for control allocation is improved by adding a judgement before calculating for each facet. Finally, the fault-tolerant scheme is applied to a six-wheel spacecraft and simulations are given to show its effectiveness.

© 2004-2018 中国地质图书馆版权所有 京ICP备05064691号 京公网安备11010802017129号

地址:北京市海淀区学院路29号 邮编:100083

电话:办公室:(+86 10)66554848;文献借阅、咨询服务、科技查新:66554700