一种小型非正交三轴吊舱设计与实现

Design and Implementation of a Small Non-Orthogonal Three-axis Pod

  • 摘要: 针对无人机光电吊舱面临的体积限制与跟踪精度不足问题,本研究提出通过非正交结构设计缩减设备尺寸,并对比分析Proportional-Integral跟踪控制器、滑模跟踪控制器、YouLa参数化跟踪控制器3种控制器的低频目标跟踪性能,为轻量化高精度吊舱开发提供解决方案。建立非正交三轴吊舱(倾斜角45°)的几何模型,通过运动学分析推导该模型下的三轴陀螺与三轴电机的解耦关系,使用YouLa参数化控制器作为跟踪控制算法,提高了光电吊舱低频段跟踪目标的响应速度和跟踪精度。采用非正交设计使吊舱水平回转半径减小约30%,采用YouLa控制器表现最优,0.5 Hz正弦扰动下相角较PI控制器超前65°左右,脱靶量幅值减小50%左右。非正交结构有效解决无人机对负载吊舱的尺寸限制,结合YouLa控制器可实现快速精准跟踪。该方案为小型化光电吊舱设计提供了结构-控制协同优化的新思路,可适用于跟踪低慢小目标的实际应用中。

     

    Abstract: To address the challenges of compact size and tracking accuracy in Unmanned Aerial Vehicle (UAV) electro-optical (EO) pods, this study proposes a co-optimization approach that integrates non-orthogonal structural design with advanced control algorithms. A 45°-tilted non-orthogonal three-axis pod model was established, and kinematic analysis revealed decoupled dynamics between gyroscopic sensors and motors. Comparative evaluations of three tracking controllers—proportional-integral (PI), sliding mode, and YouLa parameterized—demonstrated the superior performance of the YouLa controller, achieving a 65° phase lead and a 50% reduction in off-target amplitude under 0.5 Hz sinusoidal perturbations. The non-orthogonal architecture reduces the horizontal footprint by 30% while maintaining precision and effectively addressing UAV payload constraints. This structural-control synergy enables rapid and accurate tracking of slow-moving small targets, offering a novel paradigm for lightweight EO pod development with potential scalability to multitarget scenarios.

     

/

返回文章
返回