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발사 시스템의 동역학 해석을 위한 수치해석 프로그램 개발A Development of Numerical Analysis Software on Dynamic Analysis for Lunching System

Other Titles
A Development of Numerical Analysis Software on Dynamic Analysis for Lunching System
Authors
채애경배대성전혁수
Issue Date
Dec-2008
Publisher
대한기계학회
Keywords
미사일 발사 시스템; 확률론적 해석; 확률 변수; Missile Lunching System; Stochastic Analysis; Random Variable
Citation
대한기계학회논문집 A, v.32, no.12, pp.1146 - 1152
Indexed
SCOPUS
KCI
Journal Title
대한기계학회논문집 A
Volume
32
Number
12
Start Page
1146
End Page
1152
URI
https://scholarworks.bwise.kr/erica/handle/2021.sw.erica/42753
DOI
10.3795/KSME-A.2008.32.12.1146
ISSN
1226-4873
Abstract
In the initial stage of guided missile launching, the dynamic stability of a missile is highly influenced by disturbances from the outside and interferences among the launching system parts. This research develops a program for guided missile launching system analysis. Random variables are used to analyze quantitatively the missile characteristic response. An example of results with the program applied into a specific System is presented to demonstrate the effectiveness of the propose method
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COLLEGE OF ENGINEERING SCIENCES > DEPARTMENT OF MECHANICAL ENGINEERING > 1. Journal Articles

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