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The Study of Generalized Dynamical Equations for Launching System of Multiple Launch Rocket(PDF)

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

Issue:
1996年05期
Page:
41-44
Research Field:
Publishing date:

Info

Title:
The Study of Generalized Dynamical Equations for Launching System of Multiple Launch Rocket
Author(s):
Han Junli Xu Mingyou Shen Jianping
School of Dynamic Engineering,NUST,Nanjing 210094
Keywords:
rocket launching launching simulation dynamics
PACS:
TJ013
DOI:
-
Abstract:
The overall demonst ration and ov erall design of the mult iple launching ro cket system, is needed to make. In this paper , the structure of the mult iple launching rocket sy stem is analized f rom the view point of g raph theo ry, and by the analitical method of multi- rig id-body dynamics, the mult iple launching r ocket system is rig idized into four rigid part s, including ro cket, piching part , rotary part and carrier. The pro per improv ement of the dynamical augment body concept of mult i-rigid-body dynamics makes it more suitable to launching dynamics analy sis of mult iple launching rocket system. In the end, the g eneralized launching dynamics equations of matr ix fo rm w ith tensor and vector for mult iple launching rocket system is set up. It makes it co nvenienk to make launching dy namics analysis.

References:

1 Co chr an J E. Investig ation o f factor s w hich co nt ribute to mallaunch of free r ockets, AD - A 024 570, 1976
2 Co chr an J E , Gunnels Jr R T , Mccut chen Jr R K. Ro cket laucher s a s passive co ntro ls, AD - A 112 571, 1981
3 徐直军. 多管火箭弹道系统理论研究及软件开发: [ 博士学位论文] , 南京: 南京理工大学, 1993

Memo

Memo:
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Last Update: 2013-04-11