An Alignment Method of Ultraviolet Lunar Sensor Based on Lens Centering

Han Juan; Chen Jianjun; Li Zhiyong; Li Xiaoyan; Duan Jiayou

doi:10.3788/lop53.012203

[1] Huang Xin, Wang Li, Lu Xin. An ultraviolet lunar sensor for CE- 1 spacecraft[J]. Aerospace Control and Application, 2008, 34(1): 51-55

[2] Geng Jianzhong, Xiao Yelun, Han Chao. Satellite automomous navigation based on ultraviolet sensors. [J]. Aerospace Control, 2007, 25(2): 47-51.

[3] Wang Li, Hao Yuncai. Attitude determination algorithm used by lunar satellite’s imaging sensor[J]. Chinese Space Science and Technology, 2006, 12(6): 14-17.

[4] Hao Yuncai, Wang Li. Several critical problems about ultra- violet lunar sensor for lunar exploration mission[J]. Aerospace Control, 2005, 23(1): 87-91.

[5] Ye Shenglong, Wei Xinguo, Fan Qiaoyun, et al.. Operation mode design of multi-FOV star sensor[J]. Journal of Beijing University of Aeronautics and Astronauticsm 2010, 36(10): 1244-1247.

[6] Wei Chunling, Li Yong, Chen Yiqing. Spacecraft autonomous navigation based on ultraviolet sensors[J]. Aerospace Control, 2004, 22(3): 35-39.

[7] Zhou Fengli, Xu Zhaodong. Research and application of lens centering technology[J]. Infrared and Laser Engineering, 2006, 35(S2): 135-138.

[8] Yang Licheng, Ling Ning. Development of a high precision eccentricity error measurement with a thrust- shaft system [J]. Opto-electronic Engineering, 2005, 32(6): 39-42.

[9] Han Juan, Duan Jiayou, Chen Jianjun, et al.. An alignment of primary and secondary mirror for optical system in large telescopic[J]. Chinese J Lasers. 2012, 39(7): 0716001.