Closed-Loop Neurocontroller Tests on Piezoactuated Smart Rotor Blades in Hover
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1829
Reference32 articles.
1. Application of Higher Harmonic Control to Rotors Operating at High Speed and Thrust
2. A Numerical Simulation Study of Open‐Loop, Closed‐Loop and Adaptive Multicyclic Control Systems
3. A Unified Approach to the Optimal Design of Adaptive and Gain Scheduled Controllers to Achieve Minimum Helicopter Rotor Vibration
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