Active control of an aircraft tail subject to harmonic excitation
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Publication:612432
DOI10.1007/S10409-007-0077-2zbMath1202.70128OpenAlexW2093055680WikidataQ59417457 ScholiaQ59417457MaRDI QIDQ612432
Publication date: 28 December 2010
Published in: Acta Mechanica Sinica (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s10409-007-0077-2
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Cites Work
- A refined nonlinear vibration absorber
- Vibration control of a cantilever beam subject to both external and parametric excitation
- A comparison of semi-active damping control strategies for vibration isolation of harmonic disturbances
- Control of a directly excited structural dynamic model of an F-15 tail section
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