期刊文献+

宽视场大相对孔径星敏感器光学系统设计 被引量:29

Optical System Design of Star Sensor with wide-view field and Small F-number
在线阅读 下载PDF
导出
摘要 介绍了一种用于卫星姿态控制的星敏感器光学系统,该光学系统焦距为51mm,相对孔径为1/1.1,视场角为21°×21°(圆视场2ω=30°),光谱范围为0.5~0.85μm,采用了复杂化双高斯结构.与普通成像系统不同的是,该系统要求对不同光谱的恒星所采集到的点像能量中心是一致的,且星像点像的弥散圆须控制在一定的范围内.具有倍率色差小、轴上和轴外能量分布比较一致的特点. This paper presented an optical system of star sensor. The lens system was a complicated double- Gauss configuration which had an effective focal length of 51 mm, an F-number of F/1.1, a field of view of 21°×21°(2ω=30°) ,and a working wavelength rang of 0.5-0. 85 μm. The difference from common lens used in imaging system was that this lens system was required to have a high resolving power in the geometric pattern of stars. It was required to deliver the geometric spot dispersion in the specific rang at its focal surface and lower difference of displacements of centroids from thief ray in the interesting spectral range.
出处 《光子学报》 EI CAS CSCD 北大核心 2005年第12期1822-1824,共3页 Acta Photonica Sinica
关键词 星敏感器 光学设计 倍率色差 Star sensor Optical system Design Lateral color
  • 相关文献

参考文献5

  • 1黄欣.星敏感器光学系统参数的确定[J].航天控制,2000,18(1):44-50. 被引量:10
  • 2Carl Christian Liebe.Accuracy performance of star tracking-tutorial.IEEE Transactions on Aerospace and Electronic Systems,2002,38:587~599.
  • 3Carl Christian Liebe.Star trackers for attitude determination.IEEE AES Systems Magazines,1995,(6):10~16.
  • 4Kazuhide Noguchi,Koshi Sato,et al.CCD star tracker for attitude determination and control of satellite for space VLBI mission.SPIE,1996,2810:190~200.
  • 5Warren J Smith.Modern Lens Design.Genesee Optics Software,Inc.,1992,303~340.

二级参考文献4

共引文献9

同被引文献207

引证文献29

二级引证文献181

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部