DocumentCode :
1802216
Title :
Research of flight control hardware-in-the-loop simulation based on windows operation system
Author :
Qianlong Yang ; Qifeng Zhao ; Tao Min ; Chuanyan Tian ; Gang Zhou ; Fengqi Zhou
Author_Institution :
Institute of Precise Guidance and Control, Northwestern Polytechnical University, Xi´an 710072, China
fYear :
2013
fDate :
1-8 Jan. 2013
Firstpage :
1
Lastpage :
4
Abstract :
A hardware-in-the-loop (HIL) simulation platform in use of windows operation system was successfully established based on general industrial PC combined with an external timer. The following HIL simulation process of missile flight control system indicated that the novel platform could not only satisfied the real-time requirement of HIL simulation, but also is low-cost and universal, which could provide a convenient new choice in the similar applications.
Keywords :
Atmospheric modeling; Computational modeling; Computers; Data models; Mathematical model; Missiles; Numerical models; Flight control system; Missile; Windows operation system; hardware-in-the-loop; timer;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Conference Anthology, IEEE
Conference_Location :
China
Type :
conf
DOI :
10.1109/ANTHOLOGY.2013.6784827
Filename :
6784827
Link To Document :
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