Stability study and control of helicopter blade flapping vibrations
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Publication:636524
DOI10.1016/j.apm.2010.12.002zbMath1219.74020OpenAlexW2079143820MaRDI QIDQ636524
Publication date: 28 August 2011
Published in: Applied Mathematical Modelling (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.apm.2010.12.002
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Cites Work
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- A comparison between active and passive vibration control of nonlinear simple pendulum. I: Transversally tuned absorber and negative \(G\dot\varphi^n\) feedback
- A comparison between active and passive vibration control of nonlinear simple pendulum. II: Longitudinal tuned absorber and negative \(G\ddot\varphi\) and \(G\varphi^n\) feedback
- Vibration reduction of a three DOF nonlinear spring pendulum
- Saturation and resonance of nonlinear system under bounded noise excitation
- Regulation of a Two-Degree-of-Freedom Structure Using Internal Resonance
- Control of a nonlinear dynamic structural model of an F-15 tail section under primary resonance
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