首页> 外国专利> SPACECRAFT METHODS AND SYSTEMS FOR AUTONOMOUS CORRECTION OF STAR TRACKER CHARGE-TRANSFER-EFFICIENCY ERRORS

SPACECRAFT METHODS AND SYSTEMS FOR AUTONOMOUS CORRECTION OF STAR TRACKER CHARGE-TRANSFER-EFFICIENCY ERRORS

机译:自动校正星型跟踪器电荷转移效率误差的空间工艺方法和系统

摘要

Structures and methods are provided for deriving corrected star coordinates Ccrctd from measured star coordinates Cms that include star tracker charge transfer efficiency (CTE) errors. The structures and methods are based on a recognition that measured star coordinates Cms of star image centroids include CTE errors which are functions of the CCD path lengths over which the associated electrical charges traveled. In particular, the errors are substantially a product of a respective path length and a star-coordinate error factor which, in turn, is a function of the star image magnitudes msi. Information contained in different measured star coordinates Cms is organized to facilitate the derivation of an estimate * of the star-coordinate error factor with conventional estimation processes. The measured star coordinates Cms are then corrected with the error factor estimate * to realize the corrected star coordinates Ccrctd and, thereby, improve the accuracy of spacecraft attitude control.
机译:提供了用于从测得的星坐标C ms 导出校正星坐标C crctd 的结构和方法,其中包括星跟踪器电荷转移效率(CTE)误差。该结构和方法基于以下认识:所测量的恒星像质心的恒星坐标C ms 包括CTE误差,该误差是相关电荷在其上行进的CCD路径长度的函数。特别地,误差基本上是相应的路径长度和星坐标误差因子的乘积,该星坐标误差因子又是星图像大小m si 的函数。组织包含在不同的测量星坐标C ms 中的信息,以利于使用常规估算过程推导星坐标误差因子的估算*。然后用误差因子估计*校正测得的星坐标C ms ,以实现校正后的星坐标C crctd ,从而提高航天器姿态控制的精度。

著录项

  • 公开/公告号US2002125375A1

    专利类型

  • 公开/公告日2002-09-12

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US20010769637

  • 发明设计人 YEONG-WEI WU;RONGSHENG LI;JAMES H. GREEN;

    申请日2001-01-25

  • 分类号B64G1/24;B64G1/36;

  • 国家 US

  • 入库时间 2022-08-22 00:53:14

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