Full‐order sliding mode control for finite‐time attitude tracking of rigid spacecraft-Reference-Cited by-同舟云学术

Full‐order sliding mode control for finite‐time attitude tracking of rigid spacecraft

Published:2018-03-19 Issue:8 Volume:12 Page:1086-1094
ISSN:1751-8652
Container-title:IET Control Theory & Applications
language:en
Short-container-title:IET Control Theory & Applications

Author:

Song Zhuoyue¹²,Duan Chao¹²,Su Housheng³,Hu Jinchang⁴

Affiliation:

1. School of Automation, Beijing Institute of TechnologyBeijing100081People's Republic of China

2. State Key Laboratory of Intelligent Control and Decision of Complex Systems, Ministry of Education of the People's Republic of ChinaBeijing100081People's Republic of China

3. School of Automation, Image Processing and Intelligent Control Key Laboratory of Education Ministry of China, Huazhong University of Science and TechnologyLuoyu Road 1037Wuhan430074People's Republic of China

4. Beijing Institute of Control Engineering3rd South Street, Zhongguancun, HaidianBeijingPeople's Republic of China

Funder

National Natural Science Foundation of China

Publisher

Institution of Engineering and Technology (IET)

Subject

Electrical and Electronic Engineering,Control and Optimization,Computer Science Applications,Human-Computer Interaction,Control and Systems Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1049/iet-cta.2017.0583

Reference42 articles.

1. High-Performance Spacecraft Adaptive Attitude-Tracking Control Through Attracting-Manifold Design

2. Attitude Tracking and Disturbance Rejection of Rigid Spacecraft by Adaptive Control

3. Adaptive fault‐tolerant attitude tracking control of spacecraft with prescribed performance;Hu Q.L.;IEEE/ASME Trans. Mech.,2017

4. Polytopic H∞ filter design and relaxation for nonlinear systems via tensor product technique

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