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Robust H-infinity Tracing Control of 3-DOF Helicopter Model

机译:三自由度直升机模型的鲁棒H无限跟踪控制

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The stability and anti-jamming of 3-DOF helicopter model system are weak because of non-linearity and parameter uncertainty, so H-infinity mixed sensitivity laws are adopted to design trajectory tracking controller. Firstly, the bounded non-linear parameters are transformed into the uncertainty of parameters and added by inherent parameters perturbation it composes the linear uncertainty model. The H-infinity control method based on mixed sensitivity is adopted. By setting the weighting function of sensitivity and complementary sensitivity, the multitask controller of disturbance rejection and robust tracking is translated to a stander H-infinity controller of regulate problem. Simulation results demonstrate that the trajectory of helicopter attitude tracks well and system robust stability is improved.
机译:由于三自由度直升机模型系统的非线性和参数不确定性,其稳定性和抗干扰性较弱,因此采用H-无限混合灵敏度法则来设计轨迹跟踪控制器。首先,将有界非线性参数转化为参数的不确定性,并通过固有参数扰动相加,从而构成了线性不确定性模型。采用基于混合灵敏度的H无限控制方法。通过设置灵敏度和互补灵敏度的加权函数,将干扰抑制和鲁棒跟踪的多任务控制器转换为标准的H-infinity调节问题控制器。仿真结果表明,直升机姿态轨迹轨迹良好,系统鲁棒稳定性得到改善。

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