Infrared Earth sensor with a large field of view for low-Earth-orbiting micro-satellites

被引:7
|
作者
Wang, Hao [1 ]
Wang, Zhi-yuan [1 ]
Wang, Ben-dong [1 ]
Jin, Zhong-he [1 ]
Crassidis, John L. [2 ]
机构
[1] Zhejiang Univ, Sch Aeronaut & Astronaut, Hangzhou 310027, Peoples R China
[2] SUNY Buffalo, Dept Mech & Aerosp Engn, Buffalo, NY 14260 USA
关键词
Infrared Earth sensor; Micro-satellite; Attitude determination system; V447;
D O I
10.1631/FITEE.1900358
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Infrared Earth sensors are widely used in attitude-determination and control systems of satellites. The main deficiency of static infrared Earth sensors is the requirement of a small field of view (FOV). A typical FOV for a static infrared Earth sensor is about 20 degrees to 30 degrees, which may not be sufficient for low-Earth-orbiting micro-satellites. A novel compact infrared Earth sensor with an FOV of nearly 180 degrees is developed here. The Earth sensor comprises a panoramic annular lens (PAL) and an off-the-shelf camera with an uncooled complementary-metal-oxide-semiconductor (CMOS) infrared sensor. PAL is used to augment FOV so as to obtain a complete infrared image of the Earth from low-Earth-orbit. An algorithm is developed to compensate for the distortion caused by PAL and to calculate the vector of the Earth. The new infrared Earth sensor is compact with low power consumption and high precision. Simulated images and on-orbit infrared images obtained via the micro-satellite ZDPS-2 are used to assess the performance of the new infrared Earth sensor. Experiments show that the accuracy of the Earth sensor is about 0.032 degrees.
引用
收藏
页码:262 / 271
页数:10
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