一种无人机通用综合检测系统

路蔼梅; 李新军; 何进; 王松

一种无人机通用综合检测系统

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

详细信息

作者简介:
路蔼梅(1978-),女,河北石家庄人,硕士生, aimei.lu@gmail.com.

中图分类号: V 249
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- 被引次数: 0
出版历程
- 收稿日期: 2005-02-04
- 网络出版日期: 2006-01-31

General integrative test system of unmanned aerial vehicle

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

摘要

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.
- 无人机 /
- 综合检测 /
- 面向仪器系统的PCI扩展(PXI) /
- 虚拟仪器
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.
- unmanned vehicles /
- integrative testing /
- PCI extensions for instrumentation (PXI) /
- virtual instrument

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参考文献(1)

[1] u Yong, Jiang Fukang, Scott Newbern, et al. Flexible shearstress sensor skin and its application to unmanned aerial vehicles[J] Sensors and Actuators A, 2003, 105(3):321～329 [2] ung Kyung Hong. Fuzzy logic based closedloop strapdown attitude system for unmanned aerial vehicle[J] Sensors and Actuators A, 2003,107(1):109～118 [3] 书全，吕晓林，刘志强，等.一种基于虚拟仪器的无人机综合检测控制系统[J] 控技术，2002， 21(5):53～54 Cong Shuquan, Lv Xiaolin, Liu Zhiqiang, et al.The unmanned vehicle comprehensive control system by virtual instrument [J] Technique of Measure and Control, 2002， 21(5):53～54(in Chinese)[4] 晓红.无人机飞行器综合检测控制系统[J] 控技术，1999， 18(1):25～26 Qiu Xiaohong. Monitoring and control integrated system for UAVs[J] Technique of Measure and Control, 1999，18(1)：25～26(in Chinese) [5] 炎祥，黄浩，石莉，等.软件体系结构中五种常见风格的剖析[J] 计算机工程，2000， 26(10):31～32He Yanxiang, Huang Hao, Shi Li, et al. Analysis of common styles of software architecture [J] Computer Engineering, 2000, 26(10)：31～32(in Chinese)

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