Adaptive neural network vibration control of a flexible aircraft wing system with input signal quantization
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference46 articles.
1. PDE boundary control for flexible articulated wings on a robotic aircraft;Paranjape;IEEE Trans. Robot.,2013
2. Adaptive boundary control of store induced oscillations in a flexible aircraft wing;Bialy;Automatica,2016
3. Control design for nonlinear flexible wings of a robotic aircraft;He;IEEE Trans. Control Syst. Technol.,2017
4. Adaptive fault-tolerant boundary control for a flexible aircraft wing with input constraints;Gao;Aerosp. Sci. Technol.,2019
5. Smooth-switching LPV control for vibration suppression of a flexible airplane wing;He;Aerosp. Sci. Technol.,2019
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