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无人机捷联惯导系统测试设备的设计
引用本文:肖刘.无人机捷联惯导系统测试设备的设计[J].航空电子技术,2011,42(1):51-54.
作者姓名:肖刘
作者单位:西北工业大学电子信息学院,西安,710129;海军驻安顺地区航空军事代表室,安顺,561018
摘    要:针对某型无人机捷联惯导系统(SINS)的测试问题,采用虚拟仪器技术设计出了满足系统检测需求的测试设备.简单论述了该系统测试设备的总体设计,并对其软硬件设计进行了详细介绍.该测试设备以工业控制计算机为硬件平台,所有的测试板卡都安装在工业控制计算机插槽上,利用工业控制计算机的强大功能,完成信号采集、任务管理等功能.测试平台...

关 键 词:捷联惯导系统(SINS)  虚拟仪器技术  测试设备

Design of Testing Equipment for SINS in UAV
XIAO Liu.Design of Testing Equipment for SINS in UAV[J].Avionics Technology,2011,42(1):51-54.
Authors:XIAO Liu
Institution:XIAO Liu ( 1.Department of Electronic and Information, Northwestern Polytechnic University, Xi'an 710129, China; 2.Aeronautical Military Representatives Office of Navy in Anshun, Anshun 561018,China; )
Abstract:In order to test the strap-down inertial navigation system (SINS) in UAV, the paper puts forward designs that satisfy testing equipment requirements by adopting virtual instrument technique and it briefly introduces the total design of this testing system, and then it discusses the hardware and software composing in detail. The hardware of test platform is based on the industry control computer, while the signal connection and task management is completed by the industry control computer. The software which adopts the LabVIEW Program language achieves the function of system test, fault examination, user management, system maintenance and report management..
Keywords:strap-down inertial navigation system ( SINS )  virtual instrument technique  testing equipment
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