Sliding Mode Robust Control for Maximum Allowable Vertical Tail Damage to Aircraft Based on Linear Matrix Inequality-Reference-Cited by-同舟云学术

Sliding Mode Robust Control for Maximum Allowable Vertical Tail Damage to Aircraft Based on Linear Matrix Inequality

Published:2021-07 Issue:4 Volume:34 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhuang Huixuan¹^ORCID,Sun Qinglin²,Chen Zengqiang³^ORCID,Dehmer Matthias⁴

Affiliation:

1. Ph.D. Student, College of Artificial Intelligence, Nankai Univ., Tianjin 300350, China; Lecturer, School of Artificial Intelligence, Beijing Technology and Business Univ., Beijing 100048, China. ORCID: .

2. Professor, College of Artificial Intelligence, Nankai Univ., Tianjin 300350, China (corresponding author).

3. Professor, College of Artificial Intelligence, Nankai Univ., Tianjin 300350, China. ORCID: .

4. Professor, Dept. for Biomedical Computer Science and Mechatronics, UMIT-Health and Life Sciences Univ., Tyrol A-6060, Austria.

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.1943-5525.0001291

Reference29 articles.

1. A chattering-free robust adaptive sliding mode controller for synchronization of two different chaotic systems with unknown uncertainties and external disturbances;Aghababa M. P.;Appl. Math. Comput.,2012

2. Boukas, E. 2008. Control of singular systems with random abrupt changes. Berlin: Springer.

3. Piloting Strategies for Controlling a Transport Aircraft After Vertical-Tail Loss

4. Crider L. 2004. “Control of commercial aircraft with vertical tail loss.” In Proc. AIAA Aviation Technology Integration & Operations Forum. Chicago: American Institute of Aeronautics and Astronautics.

5. Etkin, B., and T. Teichmann. 1982. Dynamics of flight: Stability and control. Chichester, UK: Wiley.

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