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Helicopter rotor loads are cyclic loads that cause fatigue in different components of the rotor. This study proposes a control method that reduces these loads, prolonging the useful life of the rotor components and, therefore, reducing the cost of maintenance.
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This page is a summary of: Load Alleviation on Compound Rotorcraft Using Load Feedback and Extremum Seeking Control, Journal of Guidance Control and Dynamics, December 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g007192.
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