现代防御技术 ›› 2018, Vol. 46 ›› Issue (3): 146-151.DOI: 10.3969/j.issn.1009-086x.2018.03.022

• 探测跟踪技术 • 上一篇    下一篇

无动力滑翔高超声速飞行器轨迹预测方法

韩春耀, 熊家军, 张凯   

  1. 空军预警学院, 湖北 武汉 430019
  • 出版日期:2018-05-30 发布日期:2020-10-22
  • 作者简介:韩春耀(1989-), 男, 河北冀州人。博士生, 主要从事预警情报分析与应用研究。
    通信地址:430019 湖北省武汉市江岸区黄浦大街288号 E-mail:hanchunyaoc@163.com

Method of Trajectory Prediction for Unpowered Gliding Hypersonic Vehicle

HAN Chun-yao, XIONG Jia-jun, ZHANG Kai   

  1. Air Force Early Warning Academy, Hubei Wuhan 430019, China
  • Online:2018-05-30 Published:2020-10-22

摘要: 针对无动力滑翔高超声速飞行器轨迹预测问题及其应用需求,提出了基于动力学模型简化的轨迹预测方法。阐述了无动力滑翔高超声速飞行器预警探测面临的难点及轨迹预测在预警探测中的作用,说明了轨迹预测的必要性。分析了无动力滑翔高超声速飞行器的受力情况,通过合理的化简,得到简化的动力学模型,获得了运动轨迹的解析形式。设计了轨迹预测算法流程和轨迹预测精度的评价指标,通过仿真实验验证轨迹预测算法的有效性,并分析了引起轨迹预测误差的主要原因。

关键词: 轨迹预测, 无动力滑翔高超声速飞行器, 模型简化, 运动模型, 动力学模型, 临近空间

Abstract: Aiming at trajectory prediction of unpowered gliding hypersonic vehicle and its application requirements, a trajectory prediction algorithm is proposed based on kinetic model. The difficulties of unpowered gliding hypersonic vehicle defense and the function of trajectory prediction are expounded providing a basis for trajectory prediction. The simplified kinetic model is acquired on the basis of force analysis and reasonable shortcutting. The analytical trajectory equations are derived from kinetic model. The framework of trajectory prediction algorithm and the evaluation index are designed. To test and verify the efficiency of the trajectory prediction algorithm, simulation experiments are performed, and the main reasons causing prediction error are analyzed.

Key words: trajectory prediction, unpowered gliding hypersonic vehicle, model simplification, dynamic model, kinetic model, near space

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