Observer‐based non‐linear H ∞ attitude control for a flexible satellite-Reference-Cited by-同舟云学术

Observer‐based non‐linear H ∞ attitude control for a flexible satellite

Published:2017-10 Issue:15 Volume:11 Page:2403-2411
ISSN:1751-8652
Container-title:IET Control Theory & Applications
language:en
Short-container-title:IET Control Theory & Applications

Author:

Bai Huihui¹,Zhou Yanru¹,Sun Hongfei¹,Zeng Jianping¹

Affiliation:

1. Department of AutomationXiamen UniversityXiamen361005FujianPeople'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.2017.0129

Reference30 articles.

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2. Mixed H2/H∞ state-feedback design for microsatellite attitude control

3. Adaptive fuzzy tracking control for a class of pure‐feedback stochastic nonlinear systems with non‐lower triangular structure;Wang H.Q;Fuzzy Sets Syst.,2016

4. Observer-Based Adaptive Fuzzy Control for a Class of Nonlinear Delayed Systems

5. Tracking control of a class of non‐linear systems with applications of cruise control of hypersonic vehicles;Sun H.F.;Int. J. Control,2015

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