Retrofit Flight Control Using an Adaptive Chebyshev Function Approximator-Reference-Cited by-同舟云学术

Retrofit Flight Control Using an Adaptive Chebyshev Function Approximator

Published:2013-10 Issue:4 Volume:26 Page:735-749
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Shin Sung-Sik¹,Min Byoung-Mun²,Tahk Min-Jea³

Affiliation:

1. Patent Examiner, Transport Machinery Exam. Division, Korean Intellectual Property Office, Gov. Complex Daejeon Bldg. 4, 189, Cheongsa-ro, Seo-gu, Daejeon 302-701, Republic of Korea; formerly, Senior Researcher and Head of Group, Flight Control Group, Korean Air Research and Development Center, 461-1 Jeonmin-dong, Yuseong-gu, Daejeon 305-811, Republic of Korea.

2. Researcher, Flight Control Group, Korean Air Research and Development Center, 461-1 Jeonmin-dong, Yuseong-gu, Daejeon 305-811, Republic of Korea.

3. Professor, Dept. of Aerospace Engineering, Korea Advanced Institute of Science and Technology (KAIST), Daejeon 305-701, Republic of Korea (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.1943-5525.0000191

Reference24 articles.

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3. Retrofit Fault-Tolerant Flight Control Design Under Control Effector Damage

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5. Campa G. Sharma M. Calise A. J. and Innocenti M. (2000). “Neural network augmentation of linear controllers with application to underwater vehicles.” Proc. American Control Conf . Vol. 1 IEEE New York 75–79.