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
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;
Conference_Titel :
Intelligent Information Technology Application, 2009. IITA 2009. Third International Symposium on
Conference_Location :
Nanchang
Print_ISBN :
978-0-7695-3859-4
DOI :
10.1109/IITA.2009.477