Load reduction on a clipper liberty wind turbine with linear parameter‐varying individual blade pitch control
Author:
Affiliation:
1. Aerospace Engineering and Mechanics University of Minnesota Minneapolis Minnesota USA
2. Institute of Control Systems Hamburg University of Technology Hamburg Germany
Funder
National Science Foundation
Publisher
Wiley
Subject
Renewable Energy, Sustainability and the Environment
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/we.2121
Reference42 articles.
1. BossanyiEA.Developments in closed loop controller design for wind turbines.ASME Wind Energy Conference Reno NV USA 2000;64–74.
2. Individual Blade Pitch Control for Load Reduction
3. ColemanR FeingoldA.Theory of self‐excited mechanical oscillations of helicopter rotors with hinged blades. Technical Report NACA‐TR‐1351 NASA 1958.
4. BirG WrightA ButterfieldC.Stability analysis of a variable‐speed wind turbine.ASME Wind Energy Symposium Reno NV USA 1997;97–0965.
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