多巡飞弹三维分布式协同制导律研究
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1.南京航空航天大学自动化学院;2.南京航空航天大学航空学院

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TJ765.3??

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Research on three-dimensional distributed cooperative guidance law of multiple loitering munition
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Nanjing University of Aeronautics and Astronautics

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    摘要:

    针对多巡飞弹末端打击问题,为实现各巡飞弹的攻击时间协同,提出一种新型的偏置比例导引律。在综合考虑弹目距离及弹目接近速度的收敛要求下,基于二阶系统的一致性理论,将协同变量进行归一化处理,设计带饱和奇函数和快速收敛奇函数的一致性算法,采用李雅普诺夫函数证明其收敛性;结合弹目相对运动模型,通过速视平面中的横向误差方程推出偏置比例导引律,并将制导指令投射至参考坐标系。仿真结果表明,所设计的协同制导律落点误差保持在一米范围内,对通信邻接矩阵切换和噪声干扰情况具有很好的鲁棒性,可实现多巡飞弹的协同打击任务。

    Abstract:

    In order to achieve synchronized attack timing, a novel bias proportional guidance(BPG) law is proposed to address the terminal strike problem encountered by multiple loitering munition(LM). Drawing upon the consistency theory of second-order systems, a consistency algorithm incorporating saturation odd function and fast convergence odd function is devised, with its convergence being proven through Lyapunov function analysis. By leveraging the relative motion model of LM-target, the BPG law is derived from the lateral error equation in the Speed-LOS axes and subsequently projected onto the reference coordinate system. Simulation results demonstrate that this designed guidance law maintains drop point errors within one meter while exhibiting robustness against communication adjacency matrix switching and noise interference, thereby enabling successful cooperative strike missions for multiple LM.

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历史
  • 收稿日期:2023-10-26
  • 最后修改日期:2023-12-08
  • 录用日期:2023-12-01
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