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Design and Development of an Y4 Copter Control System

机译:Y4直升机控制系统的设计与开发

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摘要

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.
机译:y4直升机旨在成为具有自主子系统的UAV(无人机)。在保持所需的滚动,俯仰和偏航的情况下实现自动化。实现了一种使用四元数的改进算法来确定避免万向节锁定的欧拉角。它具有使用比例积分微分(PID)控制系统实现的自稳定系统。使用XBee模块构建了一个自定义遥控器,以与y4直升机通信,该模块提供了远距离和安全性。控制器和直升机之间安全的数据传输使其适合军事应用。这架y4直升机的最重要目的也许是在考虑所有可能的空气动力学特性的基础上,以低成本和高效的工程设计进行全自动化,这将是印度次大陆建造的第一架y4直升机。

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