高分CMOS相机垂轨引导凝视搜索成像设计  被引量:2

Design of Pendulum Staring Search Imaging Along the Track with High Resolution CMOS Camera

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作  者:杨秀彬[1,2] 姜丽[3] 王绍举[1,2] 王旻[1,2] 范国伟[1] 王亚敏[1,4,2] 

机构地区:[1]中国科学院长春光学精密机械与物理研究所,吉林长春130039 [2]小卫星技术国家地方联合工程研究中心,吉林长春130033 [3]长春理工大学理学院,吉林长春130000 [4]中国科学院大学,北京100049

出  处:《光学学报》2017年第7期115-124,共10页Acta Optica Sinica

基  金:国家自然科学基金青年基金(61503360)

摘  要:为实现高分面阵相机对垂直轨道方向的长条带区域一定重叠率的凝视搜索成像,设计了凝视姿态与地速运动互补偿的垂轨凝视搜索模型。通过划分垂轨长条带区域与构建目标三维运动速度,设计成像实时姿态变化与地球自转互补偿的引导策略,计算垂轨自适应搜索成像参数与实时变化指向姿态,并对卫星姿控精度对成像的影响进行了分析。最后,利用姿控三轴气浮仿真系统与CMOS相机对曲面LED目标模拟系统进行等比缩放物理仿真实验。结果表明:垂轨凝视自适应搜索成像参数为0.95时,可实现垂轨方向边缘帧间重叠率为85%、中心帧间重叠率为100%的渐变垂轨长条带成像区域,比全凝视成像区域扩大近4倍,姿控精度和姿态稳定性优于0.05°与0.003(°)s^(-1)时,像移失配量小于0.9pixel,对应的调制传递函数值为0.1559。In order to realize the staring search imaging with a certain overlap of long strip area in the vertical direction of high resolution array camera,apendulum staring search imaging model is designed with the staring gesture and earth movement complement.Based on the division of the strip layer by layer and the construction of three-dimentional movement rate,the guiding strategy of real-time posture change and earth rotation compensation is designed.Besides,the pendulum adaptive search imaging parameters and real-time variation point orientation are calculated,and the effect of attitude control precision on imaging is analyzed.Finally,aground scaling simulation experiment is carried out through the CMOS prototype,the attitude control three-axis flotation simulation platform and curved LED target system.The result shows that a gradually variational strip area with the inter frame overlap ratio more than 85%can be obtained using the pendulum staring search imaging when the pendulum staring adaptive search imaging parameter is 0.95,which is enlarged by four times than the staring imaging area.When the attitude control precision is better than 0.05°and attitude stability is better than 0.003(°)s^-1,the image motion mismatching quantity is less than 0.9pixel and the corresponding modulation transfer function can reach up to 0.1559.

关 键 词:成像系统 垂轨搜索 推凝视 重叠率 像移量 调制传递函数 

分 类 号:V443.5[航空宇航科学与技术—飞行器设计]

 

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