教師資料查詢 | 類別: 期刊論文 | 教師: 楊龍杰 Yang Lung-jieh (瀏覽個人網頁)

標題:Dynamical modeling and boundary vibration control of a rigid-flexible wing system
學年
學期
出版(發表)日期2020/12/01
作品名稱Dynamical modeling and boundary vibration control of a rigid-flexible wing system
作品名稱(其他語言)
著者Wei He; Tingting Wang; Xiuyu He; Lung-Jieh Yang; Okyay Kaynak
單位
出版者
著錄名稱、卷期、頁數IEEE/ASME Transactions on Mechatronics 25(6), p.2711-2721
摘要A boundary control approach is used to control a two-link rigid-flexible wing in this article. Its design is based on the principle of bionics to improve the mobility and the flexibility of aircraft. First, a series of partial differential equations (PDEs) and ordinary differential equations (ODEs) are derived through the Hamilton's principle. These PDEs and ODEs describe the governing equations and the boundary conditions of the system, respectively. Then, a control strategy is developed to achieve the objectives including restraining the vibrations in bending and twisting deflections of the flexible link of the wing and achieving the desired angular position of the wing. By using Lyapunov's direct method, the wing system is proven to be stable. The numerical simulations are carried out with the finite difference method to prove the effectiveness of designed boundary controllers.
關鍵字Boundary control;distributed parameter system;rigid-flexible coupled wing;vibration control
語言英文(美國)
ISSN1941-014X
期刊性質國外
收錄於SCI;EI;
產學合作
通訊作者
審稿制度
國別美國
公開徵稿
出版型式,電子版
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