自旋导弹的分布式捷联激光导引系统设计

    Design of distributed strapdown laser guidance system for spinning missiles

    • 摘要: 为了解决自旋导弹实时锁定目标的难题,提出了一种分布式捷联激光导引头光学系统。通过调整系统布局方式和镜头偏转角度,使4组镜头对应的独立视场相互耦合,形成系统视场。通过辐射计算和几何光学分析,确定镜头参数并设计镜头光路,并利用Zemax和Tracepro对镜头进行光学仿真和性能评价。详细介绍了目标探测原理,将目标反射光斑映射为二维平面视场上的动态目标,建立了具有自适应优先权重的分层加权势场模型,解决了导弹姿态调整与光学探测之间的多约束冲突。提出了自旋导弹反应式导航机制,在光斑-视场重叠面积减少时,执行正交重定向规则。开发了优先级驱动路径规划算法,并在Matlab中进行仿真验证。通过蒙特卡洛仿真对系统的稳定性和准确性进行了验证。

       

      Abstract: To address the challenge of real-time target locking for spinning missiles, a distributed strapdown laser seeker optical system was proposed. By adjusting the system layout and lens deflection angles, the independent fields of view (FOVs) corresponding to the four lens groups were coupled to form the system-level FOV. Through radiation calculation and geometric optical analysis, the lens parameters were determined and the optical path was designed, followed by optical simulation and performance evaluation of the lenses using Zemax and Tracepro. The target detection principle was elaborated, the target-reflected light spot was mapped to a dynamic target in the two-dimensional planar FOV, and hierarchical weighted potential field model with adaptive priority weights was established to resolve multi-constraint conflicts between missile attitude adjustment and optical detection. Additionally, reactive navigation mechanism for spinning missiles was proposed, which enforced the orthogonal redirection rule when the overlap area between the light spot and the FOV decreased. A priority-driven path planning algorithm was developed and validated via simulation in Matlab. Finally, the stability and accuracy of the system were verified through Monte Carlo simulations.

       

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