出版日期：2020-12-01 00:00:00

著者：Wei He; Tingting Wang; Xiuyu He; Lung-Jieh Yang; Okyay Kaynak

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：en_US

ISSN：1941-014X

期刊性質：國外

收錄於：SCI EI

審稿制度：是

國別：USA

出版型式：電子版