DocumentCode :
3200291
Title :
Design of Virtual Test Mode on the Antiaircraft Gun Weapon System Firing Test
Author :
Lin Yang ; Xianguo Meng ; Yuanchang Zhu ; Yanqiang Di
Author_Institution :
Second Dept., Ordnance Eng. Coll., Shijiazhuang, China
fYear :
2012
fDate :
8-10 Dec. 2012
Firstpage :
383
Lastpage :
385
Abstract :
The advance and complexity of the weapon system are improving by a wide margin. This makes the demand for the range test ability improving constantly. On the basis of analyzing in depth the present firing test situation of the antiaircraft gun weapon system, this text has put forward a virtual test mode, in which the virtual flight path is being substituted for the real drone aircraft. This text has also defined the structural principle and the organized implementation of the new virtual test mode. It is significant for reducing the test cost, shortening the test period, improving the test benefit, and advancing the conversion of the range test mode.
Keywords :
aircraft testing; military aircraft; weapons; antiaircraft gun weapon system; firing test; range test ability; range test mode; real drone aircraft; virtual flight path; virtual test mode; Aircraft; Computers; Control systems; Fires; Firing; Industries; Weapons; Test and Training Enabling Architecture (TENA); Virtual test; antiaircraft gun weapon system; firing precision; virtual flight path;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation, Measurement, Computer, Communication and Control (IMCCC), 2012 Second International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4673-5034-1
Type :
conf
DOI :
10.1109/IMCCC.2012.94
Filename :
6428927
Link To Document :
بازگشت