惯导测试系统软件设计与开发
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- 英文论文题名：Design and Development of Inertial Navigation Test System Software
- 论文作者：张振环 ; 石峰 ; 张峰
- 英文论文作者：ZHANG Zhen-huan ; SHI Feng ; ZHANG Feng ; Research and Development Center ; AVIC Aircraft Co. ; Ltd. ; AVIC Aircraft Aircraft Co. ; Ltd. ; Hanzhong Aircraft Branch
- 年：2016
- 作者机构：中航飞机股份有限公司研发中心;中航飞机股份有限公司汉中飞机分公司;
- 论文关键词：惯导 ; ARINC429 ; GL Studio
- 英文论文关键词：INS ; ARINC429 ; GL studio
- 会议召开时间：2016-07-15
- 会议录名称：2016航空试验测试技术学术交流会论文集
- 语种：中文
- 分类号：V249.322
- 学会代码：ZGHU
- 学会名称：中国航空学会
- 页数：3
- 文件大小：705k
- 原文格式：O
摘要
惯导是重要的装机成品,为飞机提供高精度的即时航向、姿态、速度等参数,其功能的完备和性能的良好直接决定着飞机的飞行安全。根据国军标的要求惯导必须进行装机前试验验证,试验合格方可装机,惯导的测试项目主要有数据装订与查看功能、改航功能、姿态精度、航向精度、位置精度等~([1])。通过设计一套具有良好的人机交互环境和较高的自动化程度的自动测试系统,不仅可以保证惯导的性能指标得到有效验证,并且能大大提高测试效率。
INS is an important installed finished product,which provides high-precision parameters of real-time aircraft heading,attitude,speed and other,its complete functions and good performances directly determine the safety of aircraft flight.According to the military standard requirements,INS must be carried out before installed test verification,and can be installed only passing the test.INS mainly tests for data binding and viewing,reroute,attitude accuracy,heading accuracy,position accuracy.By designing a set of automatic test system with good interactive environment and a high degree of automation,not only performance indicators of INS can ensure to be effectively verified,but also test efficiency can be greatly improved.
INS is an important installed finished product,which provides high-precision parameters of real-time aircraft heading,attitude,speed and other,its complete functions and good performances directly determine the safety of aircraft flight.According to the military standard requirements,INS must be carried out before installed test verification,and can be installed only passing the test.INS mainly tests for data binding and viewing,reroute,attitude accuracy,heading accuracy,position accuracy.By designing a set of automatic test system with good interactive environment and a high degree of automation,not only performance indicators of INS can ensure to be effectively verified,but also test efficiency can be greatly improved.
引文
[1]GJB4859-2003机载激光捷联惯性导航装置通用规范.
[2]杨大光,常波,孙国庆,等.GL Studio在飞机仪表板仿真中的应用[J].现代电子技术,2010,33(24):158-160.
[3]范秀英.基于VC++6.0的ARINC429总线接口卡通讯程序[J].兵工自动化,2011,30(4):91-92.
[4]丁云霞,曾连荪.基于VC++6.0的RS-422串口通讯设计[J].信息技术,2010(9):73-75.
[5]Distributed Simulation Technology Inc.GL Studio Version3.2API Documentation[Z].2007.
[2]杨大光,常波,孙国庆,等.GL Studio在飞机仪表板仿真中的应用[J].现代电子技术,2010,33(24):158-160.
[3]范秀英.基于VC++6.0的ARINC429总线接口卡通讯程序[J].兵工自动化,2011,30(4):91-92.
[4]丁云霞,曾连荪.基于VC++6.0的RS-422串口通讯设计[J].信息技术,2010(9):73-75.
[5]Distributed Simulation Technology Inc.GL Studio Version3.2API Documentation[Z].2007.