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奇妙的星空
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作者 千千晚星 《计算机应用文摘》 2002年第8期75-75,共1页
关键词 立体星图 软件 速度 实用工具 设置
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Auto-compensation of velocity-height ratio for Chang’E-2 satellite CCD stereo camera 被引量:4
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作者 XUE Bin ZHAO BaoChang +7 位作者 YANG JianFeng GAO Weit QIAO WeiDong MA XiaoLong ZHANG Bo LIU JiaHang ZHAO Wei JING Juan Juan 《Science China(Technological Sciences)》 SCIE EI CAS 2011年第9期2243-2246,共4页
The TDI-CCD imaging method using auto-compensation of velocity-height ratio (VHR) was applied to Chang’E-2 satellite CCD stereo camera.Factors that influence the image quality of the camera were discussed,among which... The TDI-CCD imaging method using auto-compensation of velocity-height ratio (VHR) was applied to Chang’E-2 satellite CCD stereo camera.Factors that influence the image quality of the camera were discussed,among which the mismatch error in VHR was found to be the main cause.An auto-compensation scheme for VHR was developed.The validity and effectiveness were proved by the on-orbit high quality images. 展开更多
关键词 Chang'E-2 satellite CCD stereo camera TDI-CCD velocity-height ratio auto-compensation scheme
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Overall scheme and on-orbit images of Chang’E-2 lunar satellite CCD stereo camera 被引量:8
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作者 ZHAO BaoChang YANG JianFeng +5 位作者 WEN DeSheng GAO Wei CHANG LingYing SONG ZongXi XUE Bin ZHAO Wei 《Science China(Technological Sciences)》 SCIE EI CAS 2011年第9期2237-2242,共6页
The goals of engineering and scientific missions for Chang'E-2 lunar satellite require high detection sensitivity and large imaging dynamic range for the onboard CCD cameras. The TDI CCD image sensor was adopted for ... The goals of engineering and scientific missions for Chang'E-2 lunar satellite require high detection sensitivity and large imaging dynamic range for the onboard CCD cameras. The TDI CCD image sensor was adopted for the two linear CCD stereo cameras for the first time in the lunar reconnaissance of the world. The design argumentation is described in this paper. The analysis shows that the imagers meet the mission requirements. The satellite was launched on 1 October 2010 at zero window. The cameras obtained images of 7 m resolution on the 100 km orbit for the first time on 24 October 2010, and operated once again on 27 October 2010 to take stereo images of the Sinus Iridum with the resolution better than 1.5 m. On the near-moon-arc of 15 kmxl00 km elliptical orbit, the images are very clear and rich of grey scales, indicating successful completion of the Chang'E-2 engineering mission. At the present the cameras are acquiring the full lunar surface stereo images with 7 m resolution on the 100 km circular orbit to complete their scientific mission. 展开更多
关键词 lunar satellite Chang'E -2 CCD stereo camera engineering and scientific target Sinus lridum image
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