Sliding Mode Reconfigurable Fault Tolerant Control for Nonlinear Aircraft Systems-Reference-Cited by-同舟云学术

Sliding Mode Reconfigurable Fault Tolerant Control for Nonlinear Aircraft Systems

Published:2015-05 Issue:3 Volume:28 Page:04014086
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Wang Tao¹,Xie Wenfang²,Zhang Youmin³

Affiliation:

1. Ph.D. Candidate, Dept. of Mechanical and Industrial Engineering, Concordia Univ., Montreal, QC, Canada H3G 1M8.

2. Associate Professor, Dept. of Mechanical and Industrial Engineering, Concordia Univ., Montreal, QC, Canada H3G 1M8 (corresponding author).

3. Associate Professor, Dept. of Mechanical and Industrial Engineering, Concordia Univ., Montreal, QC, Canada H3G 1M8.

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.1943-5525.0000420

Reference30 articles.

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2. Fault tolerant control using sliding modes with on-line control allocation

3. Buffington J. M. (1996). “Control design and analysis for systems with redundant limited controls.” Ph.D. thesis Univ. of Minnesota Minneapolis MN.

4. Buffington J. M. (1997). “Tailless aircraft control allocation.” Rep. No. 97-3605 American Institution of Aeronautics and Astronautics (AIAA) Reston VA.

5. Analytical redundancy and the design of robust failure detection systems

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