现代防御技术 ›› 2022, Vol. 50 ›› Issue (4): 73-83.doi: 10.3969/j.issn.1009-086x.2022.04.009

• 测试、发射技术 • 上一篇    下一篇

高海情舰载导弹发射安全区域仿真

迟鑫鹏, 郑旺辉   

  1. 北京机械设备研究所,北京 100854
  • 收稿日期:2021-12-28 修回日期:2022-03-25 出版日期:2022-08-28 发布日期:2022-09-02
  • 作者简介:迟鑫鹏(1997-),男,黑龙江肇东人。硕士,主要研究方向为发射系统仿真。

Simulation of Launch Safety Zone of Shipborne Missile Under High Sea Conditions

Xin-peng CHI, Wang-hui ZHENG   

  1. Beijing Institute of Machinery Equipmenth,Beijing 100854,China
  • Received:2021-12-28 Revised:2022-03-25 Online:2022-08-28 Published:2022-09-02

摘要:

舰载导弹在发射时会受到舰船姿态与速度的影响,使自身的姿态、位置速度发生改变。在高海情背景下,为了避免间隔发射的2枚导弹相互干扰,对发射后初始弹道的安全区域展开了研究。依据垂直发射导弹飞行初始段的运动特性,建立了弹道发射安全区域模型;对不同发射时刻下2枚导弹的弹道进行了安全区域界定。模型解决了高海情导弹发射安全区域界定的问题,具有实际工程应用价值。

关键词: 弹道, 高海情, 发射, 包围盒, 运动规律, 安全区域

Abstract:

The ship borne missile is affected by the ship attitude and velocity during launch, which changes its attitude, position and velocity. Under the background of high sea conditions, in order to avoid the mutual interference between two missiles launched at intervals, the safety area of initial trajectory after launch is studied. According to the motion characteristics of vertical launch missile in the initial flight phase, the ballistic launch safety area model is established; the ballistic safety zone of two missiles at different launch times is defined. The model solves the problem of defining the launch safety area of high sea situation missile, and has practical engineering application value.

Key words: trajectory, high sea conditions, launch, bounding box, motion law, safe area

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