北京航空航天大学学报 ›› 2006, Vol. 32 ›› Issue (01): 27-30.

• 论文 • 上一篇    下一篇

一种无人机通用综合检测系统

路蔼梅1, 李新军2, 何进2, 王松1   

  1. 1. 北京航空航天大学 机械工程及自动化学院, 北京 100083;
    2. 北京航空航天大学 无人驾驶飞行器设计研究所, 北京 100083
  • 收稿日期:2005-02-04 出版日期:2006-01-31 发布日期:2010-09-20
  • 作者简介:路蔼梅(1978-),女,河北石家庄人,硕士生, aimei.lu@gmail.com.

General integrative test system of unmanned aerial vehicle

Lu Aimei1, Li Xinjun2, He Jin2, Wang Song1   

  1. 1. School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;
    2. Research Institute of Unmanned Aerial Vehicle, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
  • Received:2005-02-04 Online:2006-01-31 Published:2010-09-20

摘要: 为了增强无人机系统检测控制设备的通用性,提高检测精度,设计了一种基于面向仪器系统的PCI扩展(PXI)总线及虚拟仪器(VI)的无人机通用综合检测系统.针对无人机系统工作的特点,从功能设计、体系结构、软硬件设计等方面对该系统的通用性进行了探讨.该系统采用了虚拟仪器技术,硬件设计采用PXI体系结构,软件以LabWindows/CVI作为开发平台.通过配备不同的接口适配器和对软件参数设置进行相应更改,可适用于不同型号的无人机电气、舵机、发动机、起飞和回收等系统检测.同时提供矩阵输出,利用系统资源满足无人机各种信号测试/激励的需求.该系统已成功应用于某复杂型号无人机的地面综合检测.

Abstract: A general integrative test system of UAV(unmanned aerial vehicle) was designed to improve the general capability of integrative test system of UAV and to increase the test system’s precision of testing. The general capability of this system was developed in aspects of design of software and hardware, the structure, and the functionality. This system adopted the VI(virtual instrument) technique. The design of hardware based on PXI(PCI extensions for instrumentation) construction and the platform of software was LabWindows/CVI. By changing the interface adaptor and the parameter settings, the system could be used in testing most subsystems of different types of UAV, such as electrocircuit, actors, engines, and so on. The system also provided an output matrix to meet the test requirements. This system was successfully used in the integrative testing of a complicated UAV.

中图分类号: 


版权所有 © 《北京航空航天大学学报》编辑部
通讯地址:北京市海淀区学院路37号 北京航空航天大学学报编辑部 邮编:100191 E-mail:jbuaa@buaa.edu.cn
本系统由北京玛格泰克科技发展有限公司设计开发