基于“H”型四旋翼飞行器的等效滑模控制器设计

Linqi Zhang, Jianan Wu, Sujie Liu, Zean Zhen, Xin He
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引用次数: 1

摘要

基于“H”型四旋翼原型机,采用牛顿-欧拉法建立了六自由度数学模型,对复杂非线性问题的位置和姿态控制进行了研究。然后,在此背景下,设计了等效滑模控制器来解决四旋翼飞行器的高度和姿态控制,并设计了PID控制器来解决水平位置控制。最后,在MATLAB/Simulink仿真环境下进行了仿真。仿真结果表明,所设计的控制器有效地实现了对四旋翼飞行器的控制,具有良好的跟踪能力和抗干扰能力。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Equivalent sliding mode controller design based on "H" type quadrotor
Based on the "H" type quadrotor prototype, a 6DOF mathematical model is developed by the Newton-Euler method in order to proceed the research of position and attitude control of complex nonlinear problems. Then, in this context equivalent sliding mode controllers are designed to solve the altitude and attitude control of the quadrotor in addition that PID controllers are designed for the horizontal position control. At last, simulations are carried out under MATLAB/Simulink simulation environment. The simulation results illustrate that the designed controllers effectively realize the control of the quadrotor revealing good tracking ability and anti — interference ability.
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