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一种用于四旋翼飞行器控制器实验调整的定制平台的设计与实现。

The Design and Implementation of a Custom Platform for the Experimental Tuning of a Quadcopter Controller.

机构信息

Faculty of Mechatronics and Aerospace, Military University of Technology, 00-661 Warsaw, Poland,

Department of Engineering, University of Sannio, 82100 Benevento, Italy.

出版信息

Sensors (Basel). 2020 Mar 30;20(7):1940. doi: 10.3390/s20071940.

Abstract

This paper describes the development process of the quadcopter-based unmanned flying platform, designed for testing and experimentation purposes. The project features custom-made hardware, which includes the prototype quadcopter frame and the flight controller, and software solutions, such as control loop setup. The article specifies the controller tuning used for the initialization of the flight stabilization system and presents the final results of the quadcopter performance evaluation.

摘要

本文描述了基于四旋翼无人机的无人飞行平台的开发过程,该平台专为测试和实验目的而设计。该项目采用了定制化的硬件,包括四旋翼原型框架和飞行控制器,以及软件解决方案,如控制回路设置。本文详细说明了用于初始化飞行稳定系统的控制器调优,并介绍了四旋翼性能评估的最终结果。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/7302/7181302/0a0d05b811cc/sensors-20-01940-g001.jpg

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