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A multivariable adaptive controller for a quadrotor with guaranteed matching conditions

机译:保证匹配条件的四旋翼多变量自适应控制器

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This paper develops an adaptive control system for a quadrotor unmanned aerial vehicle. It employs a state feedback output tracking design for multi-input multi-output systems, using a less restrictive matching condition than a state tracking design, and offers a simpler controller structure than an output feedback design. Some key characteristics of the quadrotor dynamics are derived for adaptive control design which deals with system uncertainties from changing operating points. The plant–model matching is ensured despite of system parameter uncertainties which cannot be handled by an existing state tracking design. The adaptive law is based on a parametrization using an LDS decomposition of the high-frequency gain matrix, which ensures closed-loop stability and asymptotic output tracking. A simulation study is carried out on the nonlinear quadrotor model, and results are presented to demonstrate the desired adaptive system performance.
机译:本文开发了一种四旋翼无人机的自适应控制系统。它采用了针对多输入多输出系统的状态反馈输出跟踪设计,使用的匹配条件比状态跟踪设计的限制要少,并且提供的控制器结构比输出反馈设计更简单。推导了四旋翼动力学的一些关键特性,用于自适应控制设计,该设计可解决由于工作点变化而引起的系统不确定性。尽管存在系统状态不确定性无法处理的系统参数不确定性,也可以确保工厂模型匹配。自适应律基于使用高频增益矩阵的LDS分解的参数化,可确保闭环稳定性和渐进输出跟踪。对非线性四旋翼模型进行了仿真研究,并给出了结果以证明所需的自适应系统性能。

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