冯婕, 李豫东, 文林, 郭旗. CMOS图像传感器辐射损伤导致星敏感器性能退化机理[J]. 红外与激光工程, 2020, 49(5): 20190555. DOI: 10.3788/IRLA20190555
引用本文: 冯婕, 李豫东, 文林, 郭旗. CMOS图像传感器辐射损伤导致星敏感器性能退化机理[J]. 红外与激光工程, 2020, 49(5): 20190555. DOI: 10.3788/IRLA20190555
Feng Jie, Li Yudong, Wen Lin, Guo Qi. Degradation mechanism of star sensor performance caused by radiation damage of CMOS image sensor[J]. Infrared and Laser Engineering, 2020, 49(5): 20190555. DOI: 10.3788/IRLA20190555
Citation: Feng Jie, Li Yudong, Wen Lin, Guo Qi. Degradation mechanism of star sensor performance caused by radiation damage of CMOS image sensor[J]. Infrared and Laser Engineering, 2020, 49(5): 20190555. DOI: 10.3788/IRLA20190555

CMOS图像传感器辐射损伤导致星敏感器性能退化机理

Degradation mechanism of star sensor performance caused by radiation damage of CMOS image sensor

  • 摘要: 为了分析恶劣空间辐射环境导致星敏感器性能退化、姿态测量精度降低的原因,深入研究了辐射环境下互补金属氧化物半导体(Complementary Metal Oxide Semiconductor, CMOS)图像传感器辐射损伤对星敏感器性能退化的影响。该方法通过建立空间辐射和CMOS图像传感器辐射损伤敏感参数、星敏感器性能参数之间的相关性,揭示了CMOS 图像传感器器件参数退化到星敏感器系统参数退化的传递机制。60Co-γ辐照试验表明:辐照后,系统信噪比的降低导致星敏感器星等探测灵敏度的降低,信噪比是联系CMOS图像传感器和星敏感器系统之间的桥梁。质子辐照试验表明:当辐照注量大于3.68×1010 p/cm2时,已无法正确提取星点质心。该研究结果为星敏感器在轨姿态测量误差预测和修正技术的研究奠定了一定的基础,更可以为高精度星敏感器的设计提供一定的理论依据。

     

    Abstract: In order to analyze the reasons for star sensor performance degradation and the decrease of attitude measurement accuracy, performance degradation mechanisms of star sensor caused by Complementary Metal Oxide Semiconductor (CMOS) image sensor radiation damage were mainly studied. By establishing the correlation among the spatial radiation, radiation sensitive parameters of CMOS image sensor and the performance parameters of star sensor, the transmission mechanism from CMOS image sensor device parameters degradation to star sensor system parameters degradation was revealed. The 60Co-γ irradiation test showed that the decrease of signal-to-noise ratio led to the decrease of star sensor detection sensitivity after irradiation, and the signal-to-noise ratio was the bridge between the CMOS image sensor and the star sensor system. The proton irradiation test showed that when the irradiation fluence was more than 3.68×1010 p/cm2, the star point centroid could not be extracted correctly. The results lay a certain foundation for the research of star sensor attitude measurement error and correction technology, and also provide some theoretical basis for the design of high-precision star sensor.

     

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