摘要
针对弹翼展开机构中燃气作动筒的应用研究,运用数学归纳拟合分析及建模分析的方法,提出了燃气作动筒活塞的运动计算模型。该模型用于弹翼展开装置中燃气作动筒的产品研制设计中,为燃气作动筒的设计计算提供理论指导依据。
In view of the application reseach of gas actuated roller in missile wing unfolding mechanism,a motion model was proposed by using mathematical inductive fitting method and model analysing method.This model can be used in production design of gas actuated roller in missile wing unfolding mechanism for providing theoretical basis.
出处
《弹箭与制导学报》
CSCD
北大核心
2012年第5期48-50,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
弹翼展开机构
燃气作动筒
活塞
运动方程
分析研究
missile wing unfolding mechanism
gas actuated roller
piston
equation of motion
analysis and research
