Optimal control of quad-rotor helicopter using state feedback LPV method

A. Serirojanakul, M. Wongsaisuwan
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引用次数: 9

Abstract

In this paper, the control of a quad-rotor helicopter is considered. The nonlinear model of the quad-rotor is transformed to a linear model subject to time-varying parameters called linear parameter-varying (LPV) systems. Then, the composite quadratic Lyapunov function and the quadratic cost function are used to find the optimal state feedback gain. To obtain the optimal solution, the LPV control problem is cast to the semi-definite programing problem with a set of Linear Matrix Inequality (LMI) constraints. The simulation results are provided to demonstrate the effectiveness of the proposed method.
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基于状态反馈LPV方法的四旋翼直升机优化控制
本文研究了四旋翼直升机的控制问题。将四旋翼的非线性模型转化为受时变参数影响的线性模型,称为线性变参系统。然后,利用复合二次Lyapunov函数和二次代价函数求最优状态反馈增益。为了得到最优解,将LPV控制问题转化为具有线性矩阵不等式约束的半确定规划问题。仿真结果验证了该方法的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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