DocumentCode
2933289
Title
Synchronous Detonation Control Technique on Rocket Based on Induction Setting
Author
Bo, Li ; Ya, Zhang
Author_Institution
Mech. & Electron. Eng. Inst., North Univ. of China, Taiyuan, China
Volume
3
fYear
2009
fDate
21-22 Nov. 2009
Firstpage
471
Lastpage
472
Abstract
Taking the breaking obstacle warfare as background, according to the maximum delay time and the error of synchronous detonation of rocket, based on the dynamic setter system with a unified timing starting point, it is discussed the working principle of the muzzle inductive setting system, and the transmission principle of the setting data is analyzed, then coding and decoding principle of the grouping pulse are designed, furthermore the circuit of grouping pulse encoding and the scheme of decoding are given, which would improve the broken-barrier ability of the rocket.
Keywords
detonation; military systems; rockets; decoding principle; dynamic setter system; grouping pulse encoding; induction setting; muzzle inductive setting system; obstacle warfare; rocket; synchronous detonation control; Coils; Control systems; Data communication; Decoding; Design engineering; Error correction; Frequency; Pulse circuits; Rockets; Timing; Rocket; circuit design; grouping pulse coding; muzzle induction setting; synchronous detonation;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Information Technology Application, 2009. IITA 2009. Third International Symposium on
Conference_Location
Nanchang
Print_ISBN
978-0-7695-3859-4
Type
conf
DOI
10.1109/IITA.2009.477
Filename
5370360
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