Adaptive Fuzzy Integral Sliding Mode Control for Flexible Air-Breathing Hypersonic Vehicles Subject to Input Nonlinearity-Reference-Cited by-同舟云学术

Adaptive Fuzzy Integral Sliding Mode Control for Flexible Air-Breathing Hypersonic Vehicles Subject to Input Nonlinearity

Published:2013-10 Issue:4 Volume:26 Page:721-734
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Hu Xiaoxiang¹,Wu Ligang²,Hu Changhua³,Gao Huijun⁴

Affiliation:

1. 302 Unit, Xi’an Research Institute of High-Tech, Xi’an 710025, P.R. China.

2. Professor, Space Control and Inertial Technology Research Center, Harbin Institute of Technology, Harbin 150001, P.R. China.

3. Professor, 302 Unit, Xi’an Research Institute of High-Tech, Xi’an 710025, P.R. China.

4. Professor, Space Control and Inertial Technology Research Center, Harbin Institute of Technology, Harbin 150001, P.R. China (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000193

Reference50 articles.

1. Fifty years of hypersonics: where we've been, where we're going

2. Nonlinear Longitudinal Dynamical Model of an Air-Breathing Hypersonic Vehicle

3. Bolender M. A. and Doman D. B. (2006). “A non-linear model for the longitudinal dynamics of a hypersonic air-breathing vehicle.” Air Force Research Laboratory (AFRL) Wright-Patterson AFB OH.

4. Uncertainty Modeling and Fixed-Order Controller Design for a Hypersonic Vehicle Model

5. Nonlinear Integral-Type Sliding Surface for Both Matched and Unmatched Uncertain Systems

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