Design and Development of an Y4 Copter Control System

M. S. Hossain, A. Kabir, P. Mazumder, Ahmedullah Aziz, M. Hassan, Md. Azizul Islam, P. K. Saha
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引用次数: 9

Abstract

The y4 copter is intended to be a UAV (Unmanned Aerial Vehicle) with autonomous subsystems. Automation is implemented in case of maintaining the desired roll, pitch and yaw. An improved algorithm that uses Quaternion is implemented to determine Euler angles avoiding Gimbal lock. It has a self-stabilization system achieved using Proportional Integral Derivative (PID) control system. A custom remote is built to communicate with the y4 copter using XBee modules which offer long range and security. Secured data transmission between the controller and the copter makes it suitable for military applications. Perhaps the most significant purpose of this y4 copter is to exercise a low cost and efficient engineering design with total automation considering all possible aerodynamics which is intended to be the first y4 copter built in the Indian subcontinent.
运- 4直升机控制系统的设计与开发
y4直升机打算成为一种具有自主子系统的无人机(UAV)。在保持所需的横摇、俯仰和偏航的情况下,实现自动化。提出了一种改进的四元数算法来确定避免万向节锁定的欧拉角。采用比例积分导数(PID)控制系统实现自稳定。一个定制的遥控器是建立与y4直升机使用XBee模块,提供远程和安全通信。安全的数据传输之间的控制器和直升机使其适用于军事应用。也许这架y4直升机最重要的目的是为了实现低成本和高效的工程设计,考虑到所有可能的空气动力学,这将是在印度次大陆建造的第一架y4直升机。
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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