系统仿真学报 ›› 2025, Vol. 37 ›› Issue (11): 2714-2723.doi: 10.16182/j.issn1004731x.joss.25-0392

• 论文 • 上一篇    

考虑攻击时间与区域封控的协同制导方法

郭征1, 李国飞1, 熊华2, 吴云洁3   

  1. 1.西北工业大学 航天学院,陕西 西安 710072
    2.北京电子工程总体研究所,北京 100854
    3.北京航空航天大学 自动化科学与电气工程学院,北京 100191
  • 收稿日期:2025-05-08 修回日期:2025-06-18 出版日期:2025-11-18 发布日期:2025-11-27
  • 通讯作者: 李国飞
  • 第一作者简介:郭征(2003-),男,硕士生,研究方向为多飞行器协同制导与编队控制。
  • 基金资助:
    国家自然科学基金(62373304);国家自然科学基金(62003021);中国科协青年人才托举工程(YESS20230443);陕西省秦创原高层次创新创业人才引用项目(QCYRCXM-2022-136);陕西省青年人才托举计划(XXJS202218);陕西省自然科学基础研究计划实验室重点项目(2025SYS-SYSZD-020)

Cooperative Guidance Method Considering Impact Time and Area Sealing

Guo Zheng1, Li Guofei1, Xiong Hua2, Wu Yunjie3   

  1. 1.School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China
    2.Beijing Institute of Electronic System Engineering, Beijing 100854, China
    3.School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China
  • Received:2025-05-08 Revised:2025-06-18 Online:2025-11-18 Published:2025-11-27
  • Contact: Li Guofei

摘要:

针对机动目标的多飞行器协同打击问题,提出了攻击时间控制与末端区域封控下的协同制导方法。利用分布式干扰观测器达到对目标机动的估计,基于构建的攻击时间一致性协同误差设计视线方向协同制导律,实现对目标的指定时间同时命中;依据目标运动状态设计末端区域封控指令,构造滑模面并设计视线法向制导律,保证滑模面及视线角的收敛。理论分析表明:所设计制导方法可实现攻击时间控制下对目标的区域封控,数值仿真验证了方法的有效性。

关键词: 多飞行器, 协同制导, 攻击时间控制, 区域封控, 机动目标

Abstract:

To address the problem of multi-vehicle cooperative strike against maneuvering targets, a cooperative guidance method considering impact time control and terminal area sealing was proposed. The distributed disturbance observer was utilized to estimate target maneuvers. Based on the consensus errors of the impact time, the cooperative guidance law in the line-of-sight direction was proposed to achieve simultaneous hits on targets at a specified time. By considering the motion states of targets, the instructions of the terminal area sealing were designed to construct the sliding mode surface and design the line-of-sight guidance law, so as to ensure the convergence of the sliding mode and the angles of line-of-sight. Theoretical analysis has indicated that the designed guidance method can achieve the area sealing of targets with impact time control. The effectiveness of the proposed method is verified through numerical simulations.

Key words: multi-vehicle, cooperative guidance, impact time control, area sealing, maneuvering target

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