Attitude control of a quadrotor

I. Can Dikmen, A. Arisoy, H. Temeltas
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引用次数: 102

Abstract

This study includes altitude stabilization, hovering control any desired position and attitude control of quadrotor. Classically PD controller derived and applied to this system. Inverse dynamic control, feedback linearization control and sliding mode control methods have used to derive as nonlinear controllers. Linear and nonlinear control techniques applied to attitude control of this vehicle. Derived control methods have been performed using computer simulations and compared the results according to this study objective.
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四旋翼飞行器的姿态控制
研究内容包括四旋翼飞行器的高度稳定、悬停控制和姿态控制。经典的PD控制器推导并应用于该系统。逆动态控制、反馈线性化控制和滑模控制方法被用来推导非线性控制器。将线性和非线性控制技术应用于该飞行器的姿态控制。根据本研究的目的,推导了控制方法,并对结果进行了比较。
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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