基于HODFC的小型无人直升机混沌控制

Xitong Guo, Guoyuan Qi, Xia Li, Shengli Ma
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引用次数: 0

摘要

小型无人直升机主旋翼速度快,机体轻,对扰动高度敏感。在装配不当和风干扰的情况下,机身会剧烈晃动,甚至产生混乱的角速度振荡行为。本文给出了角速度混沌振荡的情况。设计了直升机角速度高阶微分反馈控制器(HODFC)。该控制器独立于系统的数学模型,结构简单,对参数调整具有数学意义。最后,在直升机产生混沌振荡后加载控制器。加载控制器后,直升机角速度迅速趋于参考值,表明构建的HODFC能够稳定直升机角速度的混沌振荡。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
On Chaos Control of Small-scale Unmanned Helicopter Based Upon HODFC
The small-scale unmanned helicopter has the high main rotor speed and the light body, which makes it highly sensitive to disturbances. In the case of improper assembly and wind interference, the fuselage will shake violently, and even produce chaotic angular velocity oscillation behavior. In this paper, the situation of chaotic oscillation of the angular velocity is given. The high order differential feedback controller (HODFC) for the angular velocity of the helicopter is designed. The controller is independent of the mathematical model of the system, with simple structure and mathematical significance for parameter adjustment. Finally, the controller is loaded after the helicopter generates oscillations in chaotic situation. The angular velocity of the helicopter tends to the reference value rapidly after the controller is loaded, indicating that the HODFC constructed can stabilize the chaotic oscillation of the helicopter’s angular velocity.
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