Finite-Time Tracking Control of Rigid Spacecraft Under Actuator Saturations and Faults

被引：6
|
作者：
Lu, Kunfeng [1 ,2 ,3 ]
Xia, Yuanqing [1 ]
Yu, Chunmei [2 ,3 ,4 ]
Liu, Hailiang [2 ]
机构：
[1] Beijing Inst Technol, Sch Automat, Beijing 100081, Peoples R China
[2] Beijing Aerosp Automat Control Inst, Beijing 100854, Peoples R China
[3] Natl Key Lab Sci & Technol Aerosp Intelligent Con, Beijing 100854, Peoples R China
[4] Natl Univ Def Technol, Aerosp & Mat Engn, Changsha 410073, Hunan, Peoples R China
来源：
IEEE TRANSACTIONS ON AUTOMATION SCIENCE AND ENGINEERING | 2016年 / 13卷 / 01期
基金：
中国国家自然科学基金;
关键词：
Actuator saturations and faults; adaptive control; attitude tracking; fast terminal sliding mode control (FTSMC); finite-time control; SLIDING MODE CONTROL; QUATERNION BASED CONTROL; ATTITUDE TRACKING; TOLERANT CONTROL; STABILIZATION; FEEDBACK; DESIGN; MANIPULATORS; SATELLITE; SUBJECT;
D O I：
10.1109/TASE.2014.2379615
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
In this paper, an adaptive fast terminal sliding mode control control law (AFTSMCL) is presented to resolve attitude tracking control problem for rigid spacecraft, which can provide finite-time convergence, strong robustness, and fault-tolerant control. Rigorous proof is achieved first. Simulation results are presented to illustrate the effectiveness of presented control law.
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页码：368 / 381
页数：14
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