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Автор Wang, P. K. C.
Дата выпуска 1988
dc.description The vibrations of a cantilever wing which may extend or contract during flight are studied. A mathematical model for the coupled bending and torsional vibrations of an extendible wing is developed. It is found that the extending or contracting motion of the wing has a stabilizing or destabilizing effect on the wing vibrations respectively. A Galerkin-type approximation based on an appropriate time-dependent basis for the solution space is used to obtain an approximate finite-dimensional model for simulation studies. A simple implementable nonlinear feedback control for damping the motion-induced vibrations is derived by considering the time rate-of-change of the total vibrational energy of the wing. Simulation studies show that the proposed control law is effective in reducing the peak amplitude of the motion-induced vibrations.
Формат application.pdf
Издатель Oxford University Press
Копирайт Copyright Taylor and Francis Group, LLC
Название Feedback control of vibrations in an extendible cantilever wing
Тип research-article
DOI 10.1080/02681118808806051
Electronic ISSN 1465-3389
Print ISSN 0268-1110
Журнал Dynamics and Stability of Systems
Том 3
Первая страница 109
Последняя страница 133
Аффилиация Wang, P. K. C.; Department of Electrical Engineering, University of California
Выпуск 3-4
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