系统仿真学报 ›› 2021, Vol. 33 ›› Issue (11): 2742-2752.doi: 10.16182/j.issn1004731x.joss.21-FZ0739

• 国家安全仿真 • 上一篇    下一篇

拦截临近空间滑翔目标的衰减记忆滤波中制导方法

凡永华1, 皇甫逸伦1,*, 郭晓雯1,2, 李辰璐1, 李国飞1   

  1. 1.西北工业大学 航天学院,陕西 西安 710072;
    2.西安航天动力研究所,陕西 西安 710000
  • 收稿日期:2021-06-13 修回日期:2021-08-09 出版日期:2021-11-18 发布日期:2021-11-17
  • 通讯作者: 皇甫逸伦(1998-),男,硕士生,研究方向为飞行器制导与控制。E-mail:hugh239@163.com
  • 作者简介:凡永华(1975-),男,博士,教授,研究方向为飞行器制导与控制。E-mail:fanyonghua@nwpu.edu.cn
  • 基金资助:
    国家自然科学基金(62003021)

Midcourse Guidance Method Based on Fading Memory Filter for Intercepting Near-space Gliding Target

Fan Yonghua1, Huangfu Yilun1,*, Guo Xiaowen1,2, Li Chenlu1, Li Guofei1   

  1. 1. School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China;
    2. Xi'an Aerospace Propulsion Institute, Xi'an 710000, China
  • Received:2021-06-13 Revised:2021-08-09 Online:2021-11-18 Published:2021-11-17

摘要: 针对临近空间高超声速滑翔目标的拦截问题,提出了基于衰减记忆滤波算法的滑模中制导律。基于当前统计模型衰减记忆EKF(Extended Kalman Filte)算法获取精确的高超声速目标运动参量;基于滤波信息和滑模控制理论,设计了随目标机动规律在线调节拦截弹道的滑模中制导律。仿真结果表明,该衰减记忆滤波算法可以对滑翔目标进行有效跟踪且滤波精度较高;针对滑翔目标的多种机动模式,所设计的中制导律可以实现在稳定跟踪目标的同时避免始终紧随目标机动,降低过载需求。所提出方法具有良好的制导性能和较强的鲁棒性。

关键词: 衰减记忆滤波, 中制导, 临近空间, 高超声速滑翔目标

Abstract: Aiming at the interception of hypersonic gliding target in near space, a sliding mode guidance law based on fading memory filtering algorithm is proposed. The accurate motion parameters of the hypersonic target are obtained based on the current statistical model fading memory EKF(Extended Kalman Filter) algorithm. Based on the filtering information and sliding mode control theory, a sliding mode guidance law is designed to adjust the interception trajectory online according to the target maneuver law. The simulation results show that the proposed fading memory filtering algorithm can effectively track the gliding target with high filtering accuracy. For a variety of maneuvering modes of the gliding target, the designed midcourse guidance law can achieve stable tracking of the target while avoiding always following the target maneuver to reduce overload requirements. Monte Carlo results show that the proposed method has good guidance performance and strong robustness.

Key words: fading memory filter, midcourse guidance, near space, hypersonic gliding target

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