基于遗传算法的四轴飞行器模型PID整定

M. Say, E. Sybingco, A. Bandala, R. R. Vicerra, A. Chua
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引用次数: 1

摘要

UAV应用程序正在为各种应用程序开发,并且正在销售为农业、工业甚至娱乐应用程序提供解决方案。为了创造这些应用,无人机具有良好的稳定性是至关重要的,这些无人机的大多数控制系统仍然使用PID。PID的调整可以通过试错或使用齐格勒-尼科尔斯方法来完成。另一种方法是使用遗传算法,该算法可以找到最佳的PID值,而无需经历每一步的试错或Ziegler-Nichols方法。利用遗传算法方法优化PID系数,使系统产生可接受的响应。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Genetic Algorithm Approach to PID Tuning of a Quadcopter UAV Model
UAV applications are being developed for various applications and are being marketed to provide solutions for agricultural, industrial, and even entertainment applications. In order to create these applications, it is vital that the UAV has good stability, and most control system of these UAVs still makes use of PID. Tuning of PID can be done by trial and error or by using the Ziegler-Nichols method. Another approach is to use a Genetic Algorithm that will find the optimal PID values without having to go through each step of trial and error or the Ziegler-Nichols method. Using the Genetic Algorithm approach optimizes the PID coefficients to produce an acceptable response to the system.
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