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Journal of Projectiles, Rockets, Missiles and Guidance >
Real-time Dynamic Simulation Analysis of an Eject Launcher on ADAMS Software
Received date: 2013-06-12
Online published: 2025-05-30
To analyze the factors that influence missile's separation parameters, a mathematic model of dynamical system of an eject launcher and the dynamical model of it were built, during the process, the mathematical equations were embedded to the ADAMS software, real-time simulation was realized between the dynamic system and the eject launcher. According to analysis of the simulation results, it shows that by means of changing the diameter of piston and airway, the missile can get a minus angular speed which satisfies the requirements of the separation parameters.
Key words： eject launcher; real-time simulation; virtual prototype
JING Fengli . Real-time Dynamic Simulation Analysis of an Eject Launcher on ADAMS Software[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014 , 34(3) : 175 -178 . DOI: 10.15892/j.cnki.djzdxb.2014.03.030
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