LPV Model-Based Multivariable Indirect Adaptive Control of Damaged Asymmetric Aircraft-Reference-Cited by-同舟云学术

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LPV Model-Based Multivariable Indirect Adaptive Control of Damaged Asymmetric Aircraft

Published:2019-11 Issue:6 Volume:32 Page:04019095
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhang Jing¹^ORCID,Xu Xieyu²,Yang Lingyu³,Yang Xiaoke⁴^ORCID

Affiliation:

1. Assistant Professor, School of Automation Science and Electrical Engineering, Beihang Univ., Beijing 100191, China. ORCID: .

2. Research Assistant, Dept. of Control Technology, CNIGC Institution of Navigation and Control, Beijing 100089, China.

3. Associate Professor, School of Automation Science and Electrical Engineering, Beihang Univ., Beijing 100191, China (corresponding author).

4. Postdoctor, School of Automation Science and Electrical Engineering, Beihang Univ., Beijing 100191, China. ORCID: .

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.1943-5525.0001089

Reference32 articles.

1. Bacon B. J. and I. M. Gregory. 2007. “General equations of motion for a damaged asymmetric aircraft.” In Proc. 2007 AIAA Atmospheric Flight Mechanics Conf. and Exhibit 1–13. Reston VA: American Institute of Aeronautics and Astronautics.

2. Bailey R. M. R. W. Hostetler K. N. Barnes C. M. Belcastro and C. M. Belcastro. 2005. “Experimental validation: Subscale aircraft ground facilities and integrated test capability.” In Proc. AIAA Guidance Navigation and Control Conf. and Exhibit 110. Reston VA: American Institute of Aeronautics and Astronautics.

3. Bao P. M. Yuan H. Song W. Guo and J. Xue. 2011. “Aircraft wing structural damage localization research based on rbf neural network.” In Proc. 2011 IEEE 5th Int. Conf. on Cybernetics and Intelligent Systems 57–62. New York: IEEE.

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