Optimize the Space Combinations of Measure-vectors of the Integrated Star-sensor/Gyro Systems for Spacecrafts

著录项

• 来源
  《Space missions and technologies》|2010年|P.76910P.1-76910P.11|共11页
• 会议地点 Orlando FL(US)
• 作者

  Xiujian Li; rnJuncai Yang; rnJiankun Yang; rnHui Jia; rnYuanyuan Jiao; rnYisheng Yang; rnShaofeng Guo; rnMengfei Yang; rnDayi Wang; rnQingchun Fan;

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• 作者单位

  Science College, National University of Defense Technology, Changsha, Hunan, 410073, China;

  rnScience College, National University of Defense Technology, Changsha, Hunan, 410073, China;

  rnScience College, National University of Defense Technology, Changsha, Hunan, 410073, China;

  rnScience College, National University of Defense Technology, Changsha, Hunan, 410073, China;

  rnScience College, National University of Defense Technology, Changsha, Hunan, 410073, China;

  rnScience College, National University of Defense Technology, Changsha, Hunan, 410073, China;

  rnScience College, National University of Defense Technology, Changsha, Hunan, 410073, China;

  rnChina Academy of Space Technology, Beijing, 100094, China;

  rnChina Academy of Space Technology, Beijing, 100094, China;

  rnChina Academy of Space Techno;

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• 会议组织
• 原文格式 PDF
• 正文语种 eng
• 中图分类 航天（宇宙航行）;
• 关键词

  navigation system; integrated star-sensor/gyro system; measure-vector; space combination; determination precision;

  机译：导航系统;集成星敏感器/陀螺仪系统；测量向量空间组合；测定精度;