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计算机工程 ›› 2010, Vol. 36 ›› Issue (23): 246-248. doi: 10.3969/j.issn.1000-3428.2010.23.083

• 工程应用技术与实现 • 上一篇    下一篇

一种航天器对接姿态校正参数测量方法

辛勤,李双勋,粘永健   

  1. (国防科技大学电子科学与工程学院, 长沙 410073)
  • 出版日期:2010-12-05 发布日期:2010-12-14
  • 作者简介:辛勤(1973-),男,副教授、博士,主研方向:图形图像处理;李双勋,讲师、博士;粘永健,博士研究生

Measurement Method for Position and Pose Adjustment Parameter of Spacecraft Rendezvous

XIN Qin,LI Shuangxun,NIAN Yongjian   

  1. (College of Electronic Science and Engineering, National Univ. of Defense Technology, Changsha 410073, China)
  • Online:2010-12-05 Published:2010-12-14

摘要: 利用圆环投影推导三维空间中航天器相互姿态关系的数学模型,对圆环投影的检测方法进行初步讨论,提出一种基于圆环投影检测的航天器对接校正参数测量方法。该方法能直观地获取航天器对接过程中跟踪航天器的姿态校正角度参数,且不必在目标航天器布设特征光点,为实现空间航天器准确对接提供了实用、有效的解决方案。

关键词: 航天器, 对接, 分割, 投影

Abstract: This paper draws the threedimension mathematical model to estimate the position and pose parameters between spacecrafts by utilizing both circular projection and the method for circular projection detection. An approach for adjustment parameter measurement for spacecraft rendezvous based on circular projection detection is proposed. The adjustment parameter for the tracking spacecraft can be acquired directly, avoiding the arrangement for the special reference light point on the target spacecraft. It is more practical and feasible for spacecraft docking.

Key words: spacecraft, rendezvous, segmentation, projection

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