Optical system design of visible Camera for Space Debris

被引:0
作者
Wang, Hu [1 ]
Luo, Jianjun [1 ]
机构
[1] Northwestern Polytech Univ, Sch Astronaut, Xian 710072, Peoples R China
来源
INTERNATIONAL SYMPOSIUM ON PHOTOELECTRONIC DETECTION AND IMAGING 2013: IMAGING SPECTROMETER TECHNOLOGIES AND APPLICATIONS | 2013年 / 8910卷
关键词
Space debris; rendezvous and docking; visible camera;
D O I
10.1117/12.2032431
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
In order to detect the space debris, a visible camera for space debris was proposed. The visible camera was mainly consisted of primary mirror, secondary mirror. In order to balance aberration, six correcting lens were used in the optical system. To reduce the visible camera system size, two mirrors were joined, which could fold the system and shorten the overall length. The focal length was 12000 mm, field of view was 1.0 and the f-number was 10.0. The imaging quafity of the optical system in visible camera approached to diffraction limit.
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收藏
页数:5
相关论文
共 2 条
[1]  
WILSON J R, 2007, AEROSPACE AM, V302-315, P563
[2]  
YOSHIDA K., 2003, INT J ROBOT RES, V321-335, P3079