Delayed feedback control of pitch-flap instabilities in helicopter rotors-Reference-Cited by-同舟云学术

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Delayed feedback control of pitch-flap instabilities in helicopter rotors

Published:2019 Issue: Volume: Page:123-142
ISSN:
Container-title:Stability, Control and Application of Time-delay Systems
language:
Short-container-title:

Author:

Cepeda-Gomez Rudy

Publisher

Elsevier

Reference23 articles.

1. Control algorithms for helicopter vibration reduction;Hall;J. Guid. Control Dyn.,1992

2. An lpv/h∞ framework for the active control of vibrations in helicopters;Mura,2014

3. Robust harmonic control for helicopter vibration attenuation;Mura,2014

4. Periodic active control of vibrations in helicopter: a gain-scheduled multi-objective approach;Bittanti;Control Eng. Pract.,2002

5. Periodic control of helicopter rotors for attenuation of vibrations in forward flight;Arcara;IEEE Trans. Control Syst. Technol.,2000

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