Closed-Loop Control of a Microtab-Based Load Control System
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, University of California, Davis, Davis, California 95616
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032582
Reference28 articles.
1. Active load reduction using individual pitch, based on local blade flow measurements
2. Further load reductions with individual pitch control
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4. Deformable trailing edge flaps for modern megawatt wind turbine controllers using strain gauge sensors
5. On the temporal response of active load control devices
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