Fuzzy control of nonlinear aeroelastic system based on neural network identification
Author:
Affiliation:
1. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, China
2. Research Institute of UAV, Nanjing University of Aeronautics and Astronautics, Nanjing, China
Abstract
Funder
National Natural Science Foundation of China
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/09544100211010963
Reference26 articles.
1. Reduced-Order Optimal Feedback Control Law Synthesis for Flutter Suppression
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