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Aircraft's large attitude angles' usage in image motion compensation calculation of space camera
Yan D.; Li W.; Wu W.; Wang D.
2014
发表期刊Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering
ISSNISBN/10072276
卷号43期号:4页码:1200-1205
摘要In order to achieve image motion velocity accurate calculation, the method was put forward when using aerocraft attitude parameters in big attitude angle. According to the transition matrix that was from orbit coordinate to aerocraft coordinate, the relationship between coordinate system attitude angular in orbit and attitude angle, attitude angular velocity in vehicle coordinate system was derived in the big attitude angle. By calculation, when the scroll angle was 30, the maximum relative error of S1, S2 and S3 that were caused by scroll angle were 1.175%, 50% and 13.223%; when the pitch angle was 30, the maximum relative error of S1, S2 and S3 that were caused by pitch angle were 63.397%, 0.1745% and 63.397%. According to the high calculation precision of space camera image motion velocity, in a certain attitude angle, the method of using aerocraft attitude parameters was identified. This proposed method is simple and easy to implement, which is suitable for the research of image motion compensation of space camera.
收录类别EI
语种中文
文献类型期刊论文
条目标识符http://ir.ciomp.ac.cn/handle/181722/43717
专题中科院长春光机所知识产出
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GB/T 7714
Yan D.,Li W.,Wu W.,et al. Aircraft's large attitude angles' usage in image motion compensation calculation of space camera[J]. Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering,2014,43(4):1200-1205.
APA Yan D.,Li W.,Wu W.,&Wang D..(2014).Aircraft's large attitude angles' usage in image motion compensation calculation of space camera.Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering,43(4),1200-1205.
MLA Yan D.,et al."Aircraft's large attitude angles' usage in image motion compensation calculation of space camera".Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering 43.4(2014):1200-1205.
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