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Uncertain T-S model-based robust controller design with D-stability constraints-A simulation study of quadrotor attitude stabilization

机译:基于D稳定性约束的不确定T-S模型鲁棒控制器设计-四旋翼姿态稳定仿真研究

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摘要

The problem of the attitude stabilization of a quadrotor unmanned aerial vehicle is considered in simulation. An uncertain-like Takagi-Sugeno model of the quadrotor, where the nonlinear entries which depend on the input motor voltages are reported in uncertainties, is proposed to avoid closed-loop algebraic loops. The design of a Parallel Distributed Compensation (PDC) control law is considered with D-stability constraints in order to improve the closed-loop transient response. In this context, new generic and relaxed Linear Matrix Inequality (LMI) conditions are proposed. These new PDC controller design conditions constitute an alternative to previously proposed D-stabilizing non-PDC controller ones. Indeed, non-PDC controllers require online inversions of time-varying matrices, which is a major drawback for embedded applications with low computational capabilities. The conservatism of the proposed LMI conditions with respect to previous results is illustrated through an academic example. Then, simulations of the quadrotor with usual prescribed LMI regions are proposed to show the effectiveness of the proposed conditions.
机译:在仿真中考虑了四旋翼无人机的姿态稳定问题。为了避免闭环代数环路,提出了一种不确定性的四旋翼Takagi-Sugeno模型,其中非线性项依赖于输入电动机电压被不确定性报告。为了改善闭环瞬态响应,考虑了具有D稳定性约束的并行分布式补偿(PDC)控制律的设计。在这种情况下,提出了新的通用和宽松线性矩阵不等式(LMI)条件。这些新的PDC控制器设计条件构成了先前提出的D稳定非PDC控制器的替代方案。实际上,非PDC控制器需要时变矩阵的在线求逆,这对于计算能力低的嵌入式应用程序来说是一个主要缺点。通过一个学术实例说明了所提出的LMI条件相对于先前结果的保守性。然后,对具有通常规定的LMI区域的四旋翼进行了仿真,以表明所提出条件的有效性。

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