DocumentCode
3388456
Title
Data transmission of inductive setting for fuze in hard target penetrating rocket during muzzle
Author
Li Bo ; Zhang Ya ; Zhang Hongxiang
Author_Institution
Mech. & Electron. Eng. Inst., North Univ. of China, Taiyuan, China
Volume
2
fYear
2009
fDate
19-20 Dec. 2009
Firstpage
401
Lastpage
402
Abstract
Hard target penetrating fuzes can effectively enhance the penetrating effect for rockets from gun-launched platform, one of the key technologies for the fuzes is inductive setting. In this paper, the form of data code, the method of data transmission and the error control in transmission are discussed. Furthermore, the data transmission practical scheme to set the fuzes during muzzle is also given, which can make fuzes receive more than 5 frame data in muzzle setting windows by asynchronous serial communication with 16-bit binary encoding, and can reduce the error by out of step of the clock caused by high mechanical overload.
Keywords
aircraft communication; binary codes; data communication; rockets; 16-bit binary encoding; asynchronous serial communication; data transmission; hard target penetrating fuzes; hard target penetrating rocket; high mechanical overload; inductive setting; muzzle setting; muzzles; Coils; Data communication; Demodulation; Electronic mail; Electrons; Fires; Frequency shift keying; Fuses; Intelligent transportation systems; Rockets; Hard target penetrating fuzes; data transmission; inductive setting;
fLanguage
English
Publisher
ieee
Conference_Titel
Power Electronics and Intelligent Transportation System (PEITS), 2009 2nd International Conference on
Conference_Location
Shenzhen
Print_ISBN
978-1-4244-4544-8
Type
conf
DOI
10.1109/PEITS.2009.5406756
Filename
5406756
Link To Document