DocumentCode :
3322873
Title :
Design and implementation of a certain type of missile timing sequence testing system
Author :
Liu Zhaoqing ; Wang Chu ; Zhang Yigang
Author_Institution :
Sch. of Electr. Eng. & Autom., Harbin Inst. of Technol., Harbin, China
Volume :
2
fYear :
2013
fDate :
16-19 Aug. 2013
Firstpage :
765
Lastpage :
770
Abstract :
Timing sequence test is a core part for missile ground testing, the results directly determine whether the missile can be well launched. A specialized CPCI timing sequence testing system for missile is presented in this paper, which is able to complete the sequence test of tail boot, gesture controller, sequence circuit, instant flight for both equivalent device and actual missile. Also, the design of structure, firmware, driver and host computer software of the sequence test system are described in details. The experimental results show that the system is stable and efficient, conforming to the design requirements.
Keywords :
equivalent circuits; field programmable gate arrays; missile control; test equipment; virtual instrumentation; CPCI timing sequence testing system; actual missile instant flight; driver design; equivalent device instant flight; firmware design; gesture controller; missile timing sequence testing system; sequence circuit; tail boot; Computers; Field programmable gate arrays; Instruments; Missiles; Software; Testing; Timing; CPCI; FPGA; Timing sequence test;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electronic Measurement & Instruments (ICEMI), 2013 IEEE 11th International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4799-0757-1
Type :
conf
DOI :
10.1109/ICEMI.2013.6743217
Filename :
6743217
Link To Document :
بازگشت