Flight Control Energy Saving via Helicopter Rotor Active Morphing
Author:
Affiliation:
1. Civil Aviation School, Erciyes University, 38039 Kayseri, Turkey
2. Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032494
Reference32 articles.
1. Benefits of variable rotor speed in integrated helicopter/engine control
2. Rotor State Feedback Control for Rotorcraft with Variable Rotor Speed
3. Use of Rotor State Feedback to Improve Closed-Loop Stability and Handling Qualities
4. Assessment of Active Controls for Rotor Performance Enhancement
5. Dynamic Blade Shape for Improved Helicopter Rotor Performance
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