共 4 条
- [1] GUO C, 2003, J MISSILE ROCKET JAN
- [2] *NAT INSTR CORP, 2000, MULT LAB WIND TM CVI
- [3] SONG YJ, 2002, THESIS ENG I XIAN
- [4] 1998, 112 NAT INSTR
Testing instrument design for inertial navigation system of a certain type of airplane
被引：0
作者：
Guo Chuang
Yu Jin
Pang Xinmin
机构：
来源：
Proceedings of the First International Conference on Maintenance Engineering
|
2006年
关键词：
inertial navigation;
compact PCI;
multithread;
D O I：
暂无
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
The Inertial Navigation System (INS) is an important part of the navigation and pilot System of certain type of airplane. Developed with LabWindows/CVI and its device-oriented, interactive C language, a testing instrument based on the Compact PCI bus technology for the INS is developed. It realizes independent guarantee, quick testing and rapid maintenance. This paper introduces the overall design, emphasizing on the development of software that adopts the multithread application technology, especially the realization of the critical technology.
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收藏
页码：460 / 465
页数：6
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