四旋翼飞行器的线性参数变化控制

Samarathunga L. M. D. Rangajeeva, J. Whidborne
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引用次数: 33

摘要

介绍了一种四旋翼飞行器线性变参数控制器的设计。控制器综合要求由建模方程线性化得到的LPV对象模型为仿射形式。然而,四旋翼动力学的LPV表示不是仿射的;利用张量积(TP)变换将其转化为凸多边形形式。采用H∞自增益调度控制方法获得了LPV控制器,并在简化的四旋翼非线性模型上进行了测试。比较了LPV控制器与单独H∞控制器的性能。相对于H∞控制器,LPV控制器表现出显著的近距离跟踪能力。
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Linear Parameter Varying control of a quadrotor
This paper describes a Linear Parameter Varying (LPV) controller design for a quadrotor vehicle. The controller synthesis requires the LPV plant model which is obtained by linearisation of the modelling equations, to be in an affine form. However, the LPV representation of the quadrotor dynamic is not affine; hence it has been transformed into to a convex polytopic form using Tensor Product (TP) transformation. The H∞ self gain scheduling control method has been applied to obtain a LPV controller which is tested on a simplified nonlinear model of the quadrotor. The LPV controller performance was compared with a separate H∞ controller. The LPV controller exhibited significant close tracking capabilities with respect to the H∞ controller.
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