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一种基于固体火箭发动机的悬浮火箭弹道建模与仿真研究

  • 高乔 ,
  • 杨军 ,
  • 李晓晖 ,
  • 张兵峰
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  • 西安航天动力技术研究所,西安 710025

高乔(1997—),女,陕西西安人,硕士研究生,研究方向:导弹总体设计。

收稿日期: 2021-10-26

  网络出版日期: 2025-05-29

Research on Trajectory Modeling and Simulation of Suspended Rocket Based on Solid Rocket Motor

  • GAO Qiao ,
  • YANG Jun ,
  • LI Xiaohui ,
  • ZHANG Bingfeng
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  • Xi’an Aerospace Propulsion Technology, Xi’an 710025, China

Received date: 2021-10-26

  Online published: 2025-05-29

摘要

针对舰船在海面受到反舰导弹攻击的问题,采用悬浮火箭将导弹导引至舰船外安全区域的方法进行规避。对于悬浮火箭的工作过程,提出一种控制方案,首先是利用仿真软件搭建悬浮火箭的六自由度仿真模型,为使悬浮火箭在爬升段、平飞段进行可控飞行,对姿态采用阻尼回路、姿态回路双回路反馈控制,对高度采用“高度+速度”的双回路反馈控制,同时对速度采用“速度+加速度”的双回路反馈控制。仿真结果表明,这种控制方案是可行的,悬浮火箭在悬浮阶段能够保持稳定的姿态,并能够控制高度与速度进行稳定飞行,弹道特性基本满足要求。

本文引用格式

高乔 , 杨军 , 李晓晖 , 张兵峰 . 一种基于固体火箭发动机的悬浮火箭弹道建模与仿真研究[J]. 弹箭与制导学报, 2022 , 42(2) : 100 -104 . DOI: 10.15892/j.cnki.djzdxb.2022.02.018

Abstract

Aiming at the problem that the ship is attacked by anti-ship missiles on the sea, the suspension rocket is used to guide the missile to the safe area outside the ship. For the working process of suspension rocket, a control scheme is proposed.The first is to use the simulation software to build the six degree of freedom simulation model of the suspension rocket.In order to make the suspension rocket conduct controllable flight in the climbing phase and level flight phase, the dual loop feedback control of damping loop and attitude loop is adopted for the attitude, the dual loop feedback control of “height + speed” is adopted for the altitude, and the dual loop feedback control of “speed + acceleration” is adopted for the speed. The simulation results show that this control scheme is feasible.The suspension rocket can maintain a stable attitude in the suspension stage, and can control the altitude and speed for stable flight. The ballistic characteristics basically meet the requirements.

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[1]
张剑锋, 杨静, 李晓军. 舰载舷外有源雷达诱饵技术研究[J]. 舰船电子对抗, 2013, 36(1):7-12.

[2]
胡海, 孙玉明, 隋先辉. 舷外有源诱饵装备发展及作战使用现状[J]. 舰船科学技术, 2011, 33(2):14-17.

[3]
钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学[M]. 北京: 北京理工大学出版社, 2006.

[4]
关世义, 张克, 涂震飚, 等. 反舰导弹突防原理与突防技术探讨[J]. 战术导弹技术, 2010(4):1-6.

[5]
孙胜, 王钦伟, 曹洁, 等. 反舰导弹研究现状与发展趋势综述[J]. 航天控制, 2017, 35(3):79-84.

[6]
邢世其, 刘业民, 李永祯, 等.

箔条在现代海战场中的应用及现状[J]. 航天电子对抗, 2021, 37(2):58-64.

[7]
石长安, 李为民, 付强, 等. 舷外诱饵及其战术使用方式分析[J]. 飞航导弹, 2004(11):59-62.

[8]
罗兰, 杨澍, 刘忠. 舰外有源诱饵及其战术使用[J]. 弹箭与制导学报, 2003(增刊5):157-159.

[9]
臧子默, 蒋琪. 更多战舰装备Nulka诱饵[J]. 飞航导弹, 2010(5):17.

[10]
侯学隆, 曾家有, 赵遇春. 纳尔卡舷外有源诱饵作战使用研究[J]. 飞航导弹, 2021,(11):64-70.

[11]
李健. 舷外有源诱饵的现状和发展趋势[J]. 海军装备, 2016(2):43-45.

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