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Study on the Compilation of Firing Tables and Rapid Firing Elements Binding of Rocket Gun System(PDF)

《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

Issue:
2004年03期
Page:
333-336
Research Field:
Publishing date:

Info

Title:
Study on the Compilation of Firing Tables and Rapid Firing Elements Binding of Rocket Gun System
Author(s):
XU Jin xiangQI Zai kangLIN De fuSONG Jin wu
School of Mechatronics Engineering,Beijing Institute of Technology,Beijing 100081,China
Keywords:
rocket gun system f iring tables complilat ion fit calculation firing elements bind drag coef ficient ident ificat ion
PACS:
TJ012.35;TJ393
DOI:
-
Abstract:
T his paper researches the compilat ion of firing tables of rocket gun system and analyzes data processing of f iring tables test , such as drag coefficient ident ification, rocket muzzle velocity calculation, data processing of terminal elements of ascent t rajectory and dy namic thrust data acquisit ion.A 6- DOF rigid body trajectory model of firing tables is established for rocket g un system by using a developed 6- DOF t rajectory simulat ion program. T he simulat ion of a long-distance rocket w as implemented.Aiming at the problems in firing elements caused by t radit ional methods, this paper brings out a method of rapid f iring element s binding on f ire cont rol computers, and the rapid binding f low chart also has been put forw ard.

References:

[ 1] Qi Zaikang, Chen Yangquan. A six degree of freedom pr ojectiles model on progr am LOB6[ R] . Brussels: SRC, 1987.
[ 2] 闫章更, 祁载康. 射表技术[ M] . 北京: 国防工业出版社, 2000.
[ 3] Pierre W, Volker F. Application o f ar tificial intelligence techniques to 6 DOF trajector y analysis[ A] . 14th Inter national Symposium on Ballistics[ C] . Quebec Canad: ISB, 1993.

Memo

Memo:
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Last Update: 2013-03-11