三自由度四转子系统的h_∞鲁棒控制算法

Jianying Liu, Shiyue Liu, Qingbo Geng
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引用次数: 0

摘要

三自由度四转子系统是典型的高阶非线性多变量强耦合复杂系统。横摆轴、俯仰轴和横滚轴的运动方程可以模拟实际直升机的飞行特性。对于参数摄动和外部扰动的影响,通常很难建立精确的数学模型。针对这种情况,提出了混合灵敏度鲁棒控制方法,以提高系统的控制质量。仿真结果表明,当模型对象参数存在不确定性时,该控制器能使三自由度直升机系统具有良好的鲁棒稳定性和动态性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The H_Infinity Robust Control Algorithm of the 3-DOF Four Rotors System
The 3-DOF four rotors system is a typical high-order, nonlinear, multi-variable and strong coupling complex system. the motion equations of the yaw, pitch and roll axes can simulate the flight characteristics of the actual helicopter. It is usually difficult to establish the accurate mathematical model for the influence of the parameter perturbation and the external disturbance. According to this instance, the mixed sensitivity robust control method is proposed to improve the system control qualities. the simulation results shown that the controller can make the 3-DOF helicopter system have good robust stability and dynamic performance when the model object parameters exist uncertainty.
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