时滞对四旋翼直升机动力学影响的研究

22nd Mediterranean Conference on Control and Automation Pub Date : 2014-06-16 DOI:10.1109/MED.2014.6961388

A. Ailon, S. Arogeti

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引用次数: 8

摘要

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

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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22nd Mediterranean Conference on Control and Automation

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