Testing Instrument Design for Inertial Navigation System of a Certain Type of Airplane
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.
inertial navigation compact PCI multithread
GUO Chuang YU Jin PANG Xinmin
Engineering Institute, AFEU, China The Fourth Flying College of PLA Air Force, China
国际会议
The First International Conference on Maintenance Engineering(首届维修工程国际学术会议)
成都
英文
460-465
2006-10-15（万方平台首次上网日期，不代表论文的发表时间）