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An analytical approach to star identification reliability

机译:恒星识别可靠性的分析方法

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摘要

The problem of real-time, on-board star pattern identification is considered which must precede any spacecraft attitude estimation algorithm based on measured line of sight directions to stars. Following the use of the search-less k-vector method to access feasible candidate stars (detailed in a previous paper) a tiered logical structure is introduced in which inter-star angles for pairs, triples and general elementary star configurations are used to match measured patterns to corresponding patterns in a star catalog. Analytical expressions are developed for the expected frequency of matching an observed star pattern with an incorrect pattern in the star catalog due to measurement error. Such knowledge of erroneous match frequencies can be used to rigorously terminate the star identification process with a virtually certain match, while obviating the need for expensive Monte Carlo simulations. Developments shown are supported with a few simulation results.
机译:考虑了实时的机载星型识别问题,该问题必须先于任何基于测得的对星的视线方向的航天器姿态估计算法进行。在使用无搜索k矢量方法访问可行的候选恒星之后(在先前的论文中有详细介绍),引入了分层逻辑结构,其中使用成对,三重和一般基本恒星配置的星际角度来匹配测得的模式到星形目录中的相应模式。针对由于测量误差而使观测到的星型与星型目录中的错误星型匹配的预期频率,开发了解析表达式。这种错误的匹配频率知识可用于以几乎确定的匹配条件严格终止恒星识别过程,同时又不需要昂贵的蒙特卡洛模拟。一些仿真结果支持所示的开发。

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