基于微振动对成像质量影响的CMG微振动抑制方法

Isolation of micro-vibration for CMG with consideration of the influence of micro-vibration on image quality

  • 摘要: 文章以某高分辨率遥感卫星为背景,开展基于微振动对成像质量影响的CMG(controlled moment gyro,控制力矩陀螺)微振动抑制方法研究,首先分析微振动的方向、振幅、频率对成像质量的影响规律,提出微振动抑制不仅应考虑结构的动力学特性,而且应该根据微振动对成像质量的影响规律开展针对性设计;然后以某型号CMG为例,建立包括结构有限元模型、扰振源模型、隔振器模型在内的微振动分析模型,得到100 Hz频率下振动响应随隔振器弹性模量的变化规律,并在此基础上,结合隔振系统的频率要求等约束条件对隔振器参数进行优化。仿真结果表明:优化后隔振器三方向的隔振效率都在50%以上,提高了高分辨率遥感卫星的成像质量,可为后续微振动抑制研究提供参考。

     

    Abstract: With regard to the requirement of a high-resolution satellite, the isolation of the micro-vibration of the CMG(controlled moment gyro) is studied with consideration of the influence of the micro-vibration on the image quality. Firstly, it is proposed that the design of the isolator should not only consider the dynamic properties of the structure, but also consider the influence of the direction, the amplitude, and the frequency of the micro-vibration on the imaging quality. Secondly, a micro-vibration analysis model for a CMGis built and verified, including the FEM model of the structure, the disturbance model, and the isolator model. Finally, the relationship between the vibration response and the modulus of elasticity at 100Hz is obtained based on the above model, and the parameter of the isolator is optimized within the constrain of the frequency and other factors. It is shown that the isolator with the optimized parameter has an isolation efficiency of over 50% at three orthogonal directions, to ensure an increased imaging quality for the high-resolution remote sensing satellite. This method can be used in the design of the isolators.

     

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