DING Chuanbing, HU Yifeng, TAO Yong. 舰载火箭弹弹道重构与模型验证[J]. Chinese Journal of Ship Research, 2012, 7(6): 107-111. DOI: 10.3969/j.issn.1673-3185.2012.06.017
Citation: DING Chuanbing, HU Yifeng, TAO Yong. 舰载火箭弹弹道重构与模型验证[J]. Chinese Journal of Ship Research, 2012, 7(6): 107-111. DOI: 10.3969/j.issn.1673-3185.2012.06.017

舰载火箭弹弹道重构与模型验证

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  • Corresponding author:

    DING Chuanbing

  • Received Date: February 07, 2012
  • Revised Date: July 31, 2012
© 2012 The Authors. Published by Editorial Office of Chinese Journal of Ship Research. Creative Commons License
This is an Open Access article distributed under the terms of the Creative Commons Attribution 4.0 International License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
  • 为了验证火箭弹系统六自由度仿真模型的可信性,建立用于弹道重构的系统状态模型和基于GPS观测数据的量测模型,运用无迹卡尔曼滤波(UKF)算法和TIC不等式系数法,探讨仿真模型静、动态性能的验证方法。以某型舰载火箭弹系统为研究对象,通过重构火箭弹飞行状态的误差参数,对其仿真模型进行定量验证。仿真结果表明,利用弹道重构方法对六自由度弹道仿真模型进行验证是有效的。

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