A Global Fast Integral Operator Terminal Adaptive Sliding-mode Controller

摘要：

　　Attitude Control System (ACS) with high performance, high precision, and high reliability is the kernel technology of the research of spacecraft, which directly affects the whole performance of spacecraft.Hence, a global fast integral operator Terminal adaptive sliding-mode controller is proposed to come true the high performance control.The theory of this controller is to introduce the limited time mechanics—Terminal mode to the sliding-mode control and introduce the integral operator to the sliding-mode plane, which can realize the convergence of spacecraft attitude in limited time in the condition of serious disturbance, in order to enhance the performance of fast response.At last, the simulation results demonstrate the high reliability and advantages of the control approach.

关键词： Attitude Control System (ACS) Terminal Adaptive Integral operator

作者: Lu Cao Xiaoqian Chen Yong Zhao

作者单位: College of Aerospace and Materials Engineering National University of Defense Technology,Changsha 410073,China

会议类型: 国际会议

会议名称: the 3nd International Conference on Digital Manufacturing & Automation (第三届数字制造与自动化国际会议(ICDMA 2012))

会议地点: 桂林

会议语种:英文

页码: 880-885

在线出版日期: 2012-08-01（万方平台首次上网日期，不代表论文的发表时间）