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- W2029179660 abstract "The individual blade control of bearingless composite helicopter rotors aiming at vibration attenuation using adaptive structures is studied in this paper. A periodic model-following regulator is developed in the frequency domain to approximate the aeroelastic response of a single blade in forward flight to its hover characteristics. Two control strategies are investigated: a more robust one using distributed control, and a more cost-efficient one using lumped control. Selective linearization of the periodic system at determined frequencies is demonstrated in both cases." @default.
- W2029179660 created "2016-06-24" @default.
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- W2029179660 date "1994-04-21" @default.
- W2029179660 modified "2023-10-13" @default.
- W2029179660 title "Designing efficient helicopter individual blade controllers using smart structures" @default.
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- W2029179660 doi "https://doi.org/10.2514/6.1994-1766" @default.
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