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Adaptive Control of Helicopter Groun

时间:2021-12-09 16:32:29 航空航天论文 我要投稿

Adaptive Control of Helicopter Ground Resonance with Magnetorheological Damper

The methodology for adaptive control of helicopter ground resonance with magnetorheological (MR) damper is presented. The adaptive inverse control method is used to control the output damping force of MR damper and the range of the damping force is given.Through the adaptive inverse control, the damping force of MR damper is fit to a desired damping force. With the background of applying MR damper to control of helicopter ground resonance, a model of loss force and an adaptive arithmetic for stabilization of the coupled rotor/fuselage system are presented. The simulation shows that the controller presented in this paper can stabilize the rotor/fuselage coupling system quickly and control the helicopter ground resonance effectively.

作 者: Wang Wei Xia Pinqi   作者单位: College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China  刊 名: 中国航空学报(英文版)  ISTIC 英文刊名: CHINESE JOURNAL OF AERONAUTICS  年,卷(期): 2007 20(6)  分类号: V2  关键词: ground resonance   adaptive control   magnetorheological damper