Co-design of active vibration control and optimal sensor and actuator placement for a flexible wing using reinforcement learning
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, Utah State University, Logan, UT, USA
2. Department of Aerospace Engineering and Mechanics, The University of Alabama, Tuscaloosa, AL, USA
Abstract
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/09544100221149231
Reference40 articles.
1. Nonlinear Aeroelasticity of a Very Flexible Blended-Wing-Body Aircraft
2. Active control technology for flexible solar array disturbance suppression
3. Active flutter suppression of wing with morphing flap
4. Dynamic modeling and vibration control of a coupled rigid-flexible high-order structural system: A comparative study
5. Adaptive neural network vibration control of a flexible aircraft wing system with input signal quantization
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