Quadrotor Attitude Control Using Special Orthogonal Matrix

Tsung Chen, Jen-te Yu
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引用次数: 2

Abstract

This paper studies the quadrotor attitude control problem. First, the drawbacks of traditional control methods are discussed. Following that is a brief review of SO(3) that is a framework based on which the attitude dynamics and kinematics can be defined globally by a special orthogonal matrix eliminating the drawbacks encountered by traditional methods. A controller based on Lyapunov function is presented whose effectiveness is verified by numerical simulations.
基于特殊正交矩阵的四旋翼飞行器姿态控制
本文研究了四旋翼飞行器的姿态控制问题。首先,讨论了传统控制方法的缺点。在此基础上,用一种特殊的正交矩阵对姿态动力学和运动学进行全局定义,消除了传统方法所遇到的缺点。提出了一种基于李雅普诺夫函数的控制器,并通过数值仿真验证了其有效性。
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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