Calculation of image motion velocity for agile satellite dynamic imaging to changed continuously attitude point

2012 ◽  
Vol 20 (12) ◽  
pp. 2812-2820
Author(s):  
黄群东 HUANG Qun-dong ◽  
杨芳 YANG Fang ◽  
赵键 ZHAO Jiang
2016 ◽  
Vol 24 (9) ◽  
pp. 2173-2182 ◽  
Author(s):  
路朋罗 LU Peng-luo ◽  
李永昌 LI Yong-chang ◽  
金龙旭 JIN Long-xu ◽  
李国宁 LI Guo-ning ◽  
武奕楠 WU Yi-nan ◽  
...  

2012 ◽  
Vol 32 (11) ◽  
pp. 1112002 ◽  
Author(s):  
郑丽娜 Zheng Lina ◽  
张涛 Zhang Tao ◽  
匡海鹏 Kuang Haipeng ◽  
李文明 Li Wenming ◽  
杨永明 Yang Yongming ◽  
...  

2014 ◽  
Vol 34 (7) ◽  
pp. 0728003
Author(s):  
赵嘉鑫 Zhao Jiaxin ◽  
张涛 Zhang Tao ◽  
杨永明 Yang Yongming ◽  
李昕阳 Li Xinyang ◽  
王德江 Wang Dejiang
Keyword(s):  

2016 ◽  
Vol 45 (5) ◽  
pp. 0513001 ◽  
Author(s):  
李永昌 Li Yongchang ◽  
金龙旭 Jin Longxu ◽  
武奕楠 Wu Yinan ◽  
王文华 Wang Wenhua ◽  
吕增明 Lv Zengming ◽  
...  

Sensors ◽  
2021 ◽  
Vol 21 (19) ◽  
pp. 6441
Author(s):  
Jianjun Sun ◽  
Yalin Ding ◽  
Hongwen Zhang ◽  
Guoqin Yuan ◽  
Yuquan Zheng

In order to enable the aerial photoelectric equipment to realize wide-area reconnaissance and target surveillance at the same time, a dual-band dynamic scan and stare imaging system is proposed in this paper. The imaging system performs scanning and pointing through a two-axis gimbal, compensating the image motion caused by the aircraft and gimbal angular velocity and the aircraft liner velocity using two two-axis fast steering mirrors (FSMs). The composition and working principle of the dynamic scan and stare imaging system, the detailed scheme of the two-axis FSM and the image motion compensation (IMC) algorithm are introduced. Both the structure and the mirror of the FSM adopt aluminum alloys, and the flexible support structure is designed based on four cross-axis flexural hinges. The Root-Mean-Square (RMS) error of the mirror reaches 15.8 nm and the total weight of the FSM assembly is 510 g. The IMC rate equations of the two-axis FSM are established based on the coordinate transformation method. The effectiveness of the FSM and IMC algorithm is verified by the dynamic imaging test in the laboratory and flight test.


2013 ◽  
Vol 33 (5) ◽  
pp. 0511002 ◽  
Author(s):  
王翀 Wang Chong ◽  
尤政 You Zheng ◽  
邢飞 Xing Fei ◽  
张高飞 Zhang Gaofei

2013 ◽  
Vol 6 (5) ◽  
pp. 750-758
Author(s):  
李广泽 LI Guang-ze ◽  
孔德柱 KONG De-zhu ◽  
刘金国 LIU Jin-guo

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