Numerical simulation of missile vertical launching procedure based on VPT

被引：0
|
作者：
School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China [1 ]
不详 [2 ]
机构：
来源：
Binggong Xuebao/Acta Armamentarii | 2007年 / 28卷 / 04期
关键词：
Computer simulation - Design - Dynamics - Mathematical models - Missiles - Spacecraft - Structures (built objects) - Virtual reality;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
A dynamic simulation model of missile vertical launching procedure was built by use of virtual prototype technology (VPT). The constitution of vertical launching system, the simplified model and the method of dynamic simulation were proposed. Dynamic simulations for several launching conditions were conducted and the adaptability and interference of various parts were analyzed. As a result, the trajectory and attitude parameters during launching were gained and the security of missile vertical launching was verified.
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页码：491 / 494
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