Global finite-time attitude regulation using bounded feedback for a rigid spacecraft
Yusong ZHOU
Wenwu ZHU
Haibo DU
摘要：This paper investigates the problem of global attitude regulation control for a rigid spacecraft under input saturation. Based on the technique of finite-time control and the switching control method, a novel global bounded finite-time attitude regulation controller is proposed. Under the proposed controller, it is shown that the spacecraft attitude can reach the desired attitude in a finite time. In addition, the bound of a proposed attitude controller can be adjusted to any small level to accommodate the actuation bound in practical implementation.
机标关键词：rigid spacecraftinput saturationcontrol methodfinite time
资助基金：the National Natural Science Foundation of China()the National Natural Science Foundation of China(61304007)the National Natural Science Foundation of China(61673153)the Ph.D. Programs Foundation of Ministry of Education of China(20130111120007)the China Postdoctoral Science Foundation Funded Project()the China Postdoctoral Science Foundation Funded Project(2012M521217)the China Postdoctoral Science Foundation Funded Project(2014T70584)
论文发表日期：2017-01-01
在线出版日期：2025-08-15（本平台首次上网日期，不代表文献的发表时间）
页数：8( 26-33 )
英文信息