检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
机构地区:[1]中国科学院长春光学精密机械与物理研究所光学系统先进制造技术中国科学院重点实验室,吉林长春130033
出 处:《中国光学》2014年第2期315-319,共5页Chinese Optics
基 金:国家自然科学基金资助项目(No.60507003)
摘 要:为了完成飞行器导引头目标识别与探测任务,以短焦距、大视场进行搜索并确认目标,以长焦距、小视场进行高精度目标识别。通过选择正组补偿的机械补偿法,采用3种普通光学材料,在长焦距位置,将前固定组、变倍组的组合设计为远摄型,使得系统结构紧凑,满足导引头小型化的要求。利用CODEV光学设计软件,优化设计了焦距为30~150mm,视场角为12.90°×10.25°~2.59°×2.07°,筒长仅为174mm的变焦距光学系统,得到成像质量优良的设计结果。各焦距、全视场平均传递函数值在50lp/mm时为0.695,测试结果为0.562,满足系统的性能要求。In order to complete recognition and detection tasks of the aircraft seeker, a high precision, minia- turization of the zoom optical system is designed. Targets are searched and identified at short focal length, wide field, and recognized at long focal length, narrow field. The mechanical compensation method is selected using three kinds of common optical materials. At the location of the long focal length, combinatorial design of the front group and the zoom group can make the system compact, and meet seeker miniaturization require- ments. The zoom optical system with optimization focal length about 12.90° x 10. 25° - 2.59° x 2. 07° and lene tube length only 174 mm is designed by using the CODE V optical design software. For the each focal length and each field of view, the average MTF is 0. 695, and tested result is 0. 562 at 50 lp/mm, which can meet performance requirements of the system.
分 类 号:V248.3[航空宇航科学与技术—飞行器设计]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:216.73.216.3