弹箭与制导学报

弹箭与制导学报 >

2014 , Vol. 34 >Issue 3: 175 - 178

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2014.03.030

相关技术

基于ADAMS 弹射发射装置实时动态仿真分析

  • 景凤理
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  • 中国空空导弹研究院,河南洛阳 471009

景风理(1978-),男,辽宁瓦房店人,工程师,硕士,研究方向:弹射发射技术。

收稿日期: 2013-06-12

  网络出版日期: 2025-05-30

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Real-time Dynamic Simulation Analysis of an Eject Launcher on ADAMS Software

  • JING Fengli
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  • China Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2013-06-12

  Online published: 2025-05-30

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摘要

为了分析影响导弹分离参数的因素,建立某弹射发射装置的动力系统数学模型和发射装置动力学模型,将动力系统数学方程嵌入到ADAMS软件中,实现动力系统与弹射发射装置的实时仿真。对仿真结果进行分析后,结果表明,通过改变活塞直径和导气管直径能够使导弹产生低头分离角速度,满足分离参数要求。

关键词： 弹射发射装置; 实时仿真; 虚拟样机

本文引用格式

景凤理 . 基于ADAMS 弹射发射装置实时动态仿真分析[J]. 弹箭与制导学报, 2014 , 34(3) : 175 -178 . DOI: 10.15892/j.cnki.djzdxb.2014.03.030

Abstract

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

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参考文献

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