Zobrazeno 1 - 10
of 12
pro vyhledávání: '"李志来 Li Zhi-lai"'
Publikováno v:
Optics and Precision Engineering. 26:1287-1298
Autor:
董得义 Dong De-yi, 樊延超 Fan Yan-chao, 张学军 Zhang Xue-jun, 庞新源 Pang Xin-yuan, 薛栋林 Xue Dong-lin, 李志来 Li Zhi-lai
Publikováno v:
Optics and Precision Engineering. 24:1424-1431
Autor:
薛栋林 Xue Dong-lin, 杨利伟 Yang Li-wei, 樊延超 Fan Yan-chao, 董得义 Dong De-yi, 李志来 Li Zhi-lai, 曾雪锋 Zeng Xue-feng
Publikováno v:
Chinese Optics. 9:606-612
Publikováno v:
Optics and Precision Engineering. 24:1917-1926
Publikováno v:
Optics and Precision Engineering. 23:3357-3363
Publikováno v:
Optics and Precision Engineering. 23:2533-2539
Autor:
关英俊 Guan Ying-jun, 曹乃亮 Cao Nai-liang, 李志来 Li Zhi-lai, 徐宏 Xu Hong, 鲍赫 Bao He, 杨会生 Yang Hui-sheng
Publikováno v:
Optics and Precision Engineering. 22:3342-3347
The extraction method of kinematic formula for a drift adjusting mechanism in space cameras was researched to accurately control the drift adjusting mechanism and to improve the imaging quality. The distribution law of test data for the drift adjusti
Publikováno v:
Optics and Precision Engineering. 21:3169-3175
As the temperature adaptation effects the design process of a large aperture mirror assembly seriously,this paper researches the influence mechanism of temperature on the large aperture mirror assembly and discusses the necessity of temperature adapt
Autor:
杨会生 Yang Hui-sheng, 柴方茂 Chai Fang-mao, 徐宏 Xu Hong, 李志来 Li Zhi-lai, 张银鹤 Zhang Yin-he, 关英俊 Guan Ying-jun
Publikováno v:
Optics and Precision Engineering. 21:948-954
Space cameras are extremely vulnerable to the offset from its optimal position to the focal plane because of its complicated launch environments including shock,vibration and overload,and space operating environments,such as high vacuum,low temperatu
Autor:
刘巨 Liu Ju, 李志来 Li Zhi-lai, 吴清文 Wu Qing-wen, 于善猛 Yu Shan-meng, 江帆 Jiang Fan, 杨献伟 Yang Xian-wei
Publikováno v:
Chinese Journal of Optics and Applied Optics. 6:237-243
A thermal simulation was established according to sensor parameters and the mission requirements to accomplish the thermal design of a lightweight space remote sensor.Atomic oxygen resistant cloth was chosen as the outmost material to reduce the dama