发明名称 |
Real-time refinement method of spacecraft star tracker alignment estimates |
摘要 |
A method of estimating the alignment of a star sensor ( 20 ) for a vehicle ( 12 ) includes generating star tracker data. A vehicle attitude and a star sensor attitude are determined in response to the star tracker data. A current alignment sample is generated in response to the vehicle attitude and the star sensor attitude. A current refined estimate alignment signal is generated in response to the current alignment sample and a previously refined estimate alignment signal via a vehicle on-board filter ( 38 ).
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申请公布号 |
US2006149474(A1) |
申请公布日期 |
2006.07.06 |
申请号 |
US20050028094 |
申请日期 |
2005.01.03 |
申请人 |
NEEDELMAN DAVID D;LI RONGSHENG;WU YEONG-WEI A |
发明人 |
NEEDELMAN DAVID D.;LI RONGSHENG;WU YEONG-WEI A. |
分类号 |
G01C21/26 |
主分类号 |
G01C21/26 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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