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http://dx.doi.org/10.3795/KSME-A.2008.32.12.1146

A Development of Numerical Analysis Software on Dynamic Analysis for Lunching System  

Chae, Ae-Kyung (LG 전자 DAC 연구소)
Bae, Dae-Sung (한양대학교 기계정보경영공학부)
Jeon, Hyuck-Soo (국방과학연구소)
Publication Information
Transactions of the Korean Society of Mechanical Engineers A / v.32, no.12, 2008 , pp. 1146-1152 More about this Journal
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.
Keywords
Missile Lunching System; Stochastic Analysis; Random Variable;
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