Study on the effects of time-delays on quadrotor-type helicopter dynamics

A. Ailon, S. Arogeti
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引用次数: 8

Abstract

This study considers a simple velocity-free controller for altitude/attitude regulation for the highly nonlinear model of a quadrotor-type helicopter. Some useful structural properties of the proposed closed-loop system are considered for studying stability when time-delay appears in the feedback loop. Numerical and simulation results demonstrate the impact of the time delays on the system dynamics.
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时滞对四旋翼直升机动力学影响的研究
本文研究了一种简单的无速度控制器,用于高度非线性四旋翼直升机的高度/姿态调节。考虑了所提闭环系统的一些有用的结构性质,用于研究反馈回路中出现时滞时的稳定性。数值和仿真结果验证了时滞对系统动力学的影响。
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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