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用于深空探测快速反射镜的电磁驱动

Research on electromagnetic drive of fast steering mirror for deep space detection

  • 摘要: 为了实现深空探测系统对成像光束的高速和高精度控制, 以⌀50 mm×4 mm的单晶硅反射镜作为负载, 采用理论和仿真分析相结合的方法, 对音圈电机驱动的快速反射镜进行了理论分析和实验验证。给出了该快速反射镜的一般构成、工作原理及数学模型, 采用有限元法分析计算了音圈电机线圈、永磁体和气隙尺寸对驱动力矩的影响, 最后设计、制作了快速反射镜样机, 并进行了测试。结果表明, 快速反射镜的转角范围大于±1°, 带宽(3 dB)大于500 Hz。该研究结果有助于推广光学快速反射镜在深空探测、激光通信、光电对抗等领域的应用。

     

    Abstract: In order to realize the high speed and high precision control of the imaging beam for the deep space detection system, the theoretical analysis and experimental verification of the fast steering mirror (FSM) driven by the voice coil actuators (VCA) were carried out with a ⌀50 mm×4 mm silicon mirror as the load. At first, the drive mechanism, configuration, and mathematical model of the FSM were presented. Then the finite element method was used to study the influence of the coil, permanent magnet and air gap size of the VCA on the driving torque. Finally, a prototype of abovementioned FSM was designed, produced, and tested, respectively. The result indicates that, the angular stroke of the FSM is greater than ±1°, and the 3 dB bandwidth is greater than 500 Hz. The procedure disclosed here is helpful for FSM to be applied in the fields of deep space detection, laser communication, photoelectric countermeasure, etc.

     

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