Numerical simulation of missile vertical launching procedure based on VPT

Yue Xu; Ai Mei Tian; Zhen Peng Zhang; Xiao Qing Chen

Numerical simulation of missile vertical launching procedure based on VPT

Yue Xu^*
, Ai Mei Tian
, Zhen Peng Zhang
, Xiao Qing Chen

^*此作品的通讯作者

宇航学院

科研成果: 期刊稿件 › 文章 › 同行评审

3 引用（Scopus）

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.

源语言	英语
页（从-至）	491-494
页数	4
期刊	Binggong Xuebao/Acta Armamentarii
卷	28
期	4
出版状态	已出版 - 4月 2007

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引用此

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title = "Numerical simulation of missile vertical launching procedure based on VPT",

abstract = "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.",

keywords = "Missile, Multibody dynamics, Simulation, Spacecraft structure and design, Vertical launching, Virtual prototype",

author = "Yue Xu and Tian, \{Ai Mei\} and Zhang, \{Zhen Peng\} and Chen, \{Xiao Qing\}",

year = "2007",

month = apr,

language = "英语",

volume = "28",

pages = "491--494",

journal = "Binggong Xuebao/Acta Armamentarii",

issn = "1000-1093",

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T1 - Numerical simulation of missile vertical launching procedure based on VPT

AU - Xu, Yue

AU - Tian, Ai Mei

AU - Zhang, Zhen Peng

AU - Chen, Xiao Qing

PY - 2007/4

Y1 - 2007/4

N2 - 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.

AB - 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.

KW - Missile

KW - Multibody dynamics

KW - Simulation

KW - Spacecraft structure and design

KW - Vertical launching

KW - Virtual prototype

UR - https://www.scopus.com/pages/publications/34249987925

M3 - 文章

AN - SCOPUS:34249987925

SN - 1000-1093

VL - 28

SP - 491

EP - 494

JO - Binggong Xuebao/Acta Armamentarii

JF - Binggong Xuebao/Acta Armamentarii

IS - 4

ER -

Numerical simulation of missile vertical launching procedure based on VPT

摘要

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