Linear Parameter Varying Switching Attitude Tracking Control for a Near Space Hypersonic Vehicle Via Multiple Lyapunov Functions
Author:
Affiliation:
1. College of Electrical Engineering; Anhui Polytechnic University; Wuhu 241000 China
2. School of Automation; Southeast University; Nanjing 210096 China
Funder
National Natural Science Foundation
Natural Science Foundation of Anhui province
Publisher
Wiley
Subject
Control and Systems Engineering
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1002/asjc.1114/fullpdf
Reference40 articles.
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2. Fifty years of hypersonics: where we've been, where we're going;Bertin;Prog. Aerosp. Sci.,2003
3. Passive fault-tolerant control design for near-space hypersonic vehicle dynamical system;Gao;Circuits Syst. Signal. Process.,2012
4. Progress in control approaches for hypersonic vehicle;Duan;Sci. China Technol. Sci.,2012
5. Multiobjective fault detection and isolation for flexible air-breathing hypersonic vehicle;Cai;J. Syst. Eng. Electron.,2011
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