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 ).
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 代理人
主权项
地址