Spacecraft Relative Attitude Determination

被引：0
|
作者：
Goh, Shu Ting [1 ]
Passerello, Chris E. [1 ]
Abdelkhalik, Ossama [1 ]
机构：
[1] Michigan Tech Univ, Mech Engn Engn Mech, Houghton, MI 49931 USA
来源：
2010 IEEE AEROSPACE CONFERENCE PROCEEDINGS | 2010年
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A method to determine the relative attitudes between three spacecraft is developed. (12)The method requires four direction measurements between the three spacecraft. The simulation results and covariance analysis show that the method's error falls within a three sigma boundary without exhibiting any singularity issues. A study of the accuracy of the proposed method with respect to the shape of the spacecraft formation is also presented.
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页数：6
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