舰船电子工程2025，Vol.45Issue(4)：38-40,66,4.DOI:10.3969/j.issn.1672-9730.2025.04.009
基于垂直冷弹射导弹点火失败跌落姿态分析
Analysis of Falling Attitude Based on Vertical Cold Launch Missile's Failure to Ignite
摘要
Abstract
There is a possibility of ignition failure for ship borne missiles using cold ejection ignition.If the missile falls back onto the launch platform,there is a risk of platform deformation or even engine fire.This article applies ADAMS software to conduct dynamic simulation of the ejection drop process of a missile with failed cold ejection ignition,analyzes the changes in the attitude of the missile during the drop process,and provides theoretical support for subsequent research on missile drop safety.关键词
导弹/跌落/动力学仿真/姿态Key words
missile/falling/dynamic simulation/attitude引用本文复制引用
杨明,刘丙杰,张磊,冀海燕..基于垂直冷弹射导弹点火失败跌落姿态分析[J].舰船电子工程,2025,45(4):38-40,66,4.
