Active Fault Tolerant Control for Flexible Spacecraft with Sensor Faults Using Adaptive Integral Sliding Mode

摘要：

1 Introduction The attitude control system is one of the most important problem in spacecraft design.In modern space related missions,there is a high demand on safety,reliability and performance of spacecraft.

作者: Zhifeng Gao Bing Han Moshu Qian Jing Zhao

作者单位: College of Automation,Nanjing University of Posts and Telecommunications,Nanjing 210023,Peoples Rep College of Electrical Engineering and Control Science,Nanjing Tech University,Nanjing 211800,People

会议类型: 国际会议

会议名称: 2017 Chinese Intelligent Automation Conference(CIAC2017)(2017中国智能自动化会议)

会议地点: 天津

会议语种:英文

页码: 23-30

在线出版日期: 2017-10-14（万方平台首次上网日期，不代表论文的发表时间）