An All-Day Attitude Sensor Integrating Stars and Sun Measurement Based on Extended Pixel Response of CMOS APS Imager

被引:2
|
作者
Cao, Hongjing [1 ,2 ]
Zhan, Haiyang [1 ,2 ]
Li, Jingdong [1 ,2 ]
Rao, Qilong [3 ]
Xing, Fei [1 ,2 ]
You, Zheng [1 ,2 ]
机构
[1] Tsinghua Univ, Beijing Adv Innovat Ctr Integrated Circuits, Dept Precis Instrument, Beijing 100084, Peoples R China
[2] Tsinghua Univ, State Key Lab Precis Measurement Technol & Instrum, Beijing 100084, Peoples R China
[3] Shanghai Inst Satellite Engn, Shanghai 201109, Peoples R China
基金
中国国家自然科学基金;
关键词
Sun; Stars; Optical sensors; Optical imaging; Optical variables measurement; Optical saturation; Optical polarization; Attitude measurement; optical instrumentations; optical measurement; space instrumentations; PINNED PHOTODIODE; NAVIGATION METHOD; ORIENTATION; ACCURACY; DESIGN; CCD;
D O I
10.1109/TIM.2023.3265092
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
For celestial measurement, it is difficult to enable a single optical system to image and measure both stars and the sun due to the vastly different light intensity of targets and the limited response capability of the image sensor pixel. Here, we develop an all-day optical attitude sensor integrating stars and the sun measurement based on the extended pixel response model of the CMOS active-pixel sensor (APS) imager. For extremely large light intensity, we extend the conventional pixel response model to the oversaturated stage where the pixel values reverse and drop below the saturation value. Based on this, the integration of the star sensor and the sun sensor is realized. The pixels image the starry sky with linear response, and make use of the oversaturation response to image the sun and obtain a black spot on the bright background. This principle enables the capability of all-day high-precision attitude measurement using a single miniaturized sensor. An integrated optical attitude sensor is designed and manufactured. Ground-based observation results show that the orientation accuracy from sun measurement is better than 9" (3s), and the attitude accuracy from star measurement is better than 5" (3s) for pointing and 11" (3s) for rolling. The sensor can be applied to high-precision all-day navigation systems for miniaturized spacecraft and aircraft.
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页数:11
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