期刊
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY
卷 30, 期 5, 页码 2243-2250出版社
IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TCST.2021.3139087
关键词
Trajectory; Vibrations; Trajectory tracking; Aerospace electronics; Mathematical models; Bending; Solid modeling; 3-D flexible wing; distributed parameter system; trajectory tracking control; vibration control
资金
- National Natural Science Foundation of China [61933001, 62073030, U20A20225]
- Beijing Natural Science Foundation [JQ20026]
- Beijing Top Discipline for Artificial Intelligence Science and Engineering, University of Science and Technology Beijing
This paper mainly discusses trajectory tracking and vibration suppression for a 3-D flexible wing. A control strategy involving two angles is proposed for trajectory tracking, while two active boundary controllers are suggested to suppress vibrations. Numerical simulations confirm the effectiveness of the proposed control schemes.
This brief mainly considers trajectory tracking and vibration suppression for a 3-D flexible wing. The dynamical model of the flexible wing is regarded as a distributed parameter system, which is described by partial differential equations and ordinary differential equations. A control strategy regulates the flexible wing to track the desired trajectory by controlling two angles. Meanwhile, two active boundary controllers are proposed to restrain the vibrations both in bending and twisting. By using Lyapunov's direct method, the stability of the flexible wing system can be ensured. Numerical simulations based on the finite-difference method demonstrate the effectiveness of the proposed control schemes.
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