发明名称 Lost-in-space stellar attitude acquisition using multiple star trackers
摘要 A method, apparatus, article of manufacture for determining the attitude of a spacecraft having at least one star sensor. The method comprises the steps of selecting a first reference star sensor from among the star sensors; designating two stars observed by the first reference star sensor as a primary star pair; identifying a candidate star pair corresponding to the primary star pair, wherein the candidate star pair is selected from a star catalog having a plurality of entries; estimating an inertial orientation of the first star sensor at least in part from the identified candidate star pair; and determining the spacecraft attitude from the estimated inertial orientation of a reference star sensor selected from a group comprising the first star sensor.
申请公布号 US6470270(B1) 申请公布日期 2002.10.22
申请号 US20000708132 申请日期 2000.11.07
申请人 THE BOEING COMPANY 发明人 NEEDELMAN DAVID D.;WU YEONG-WEI A.;LI RONGSHENG;BURKETT, JR. WILLIAM L.
分类号 B64G1/26;B64G1/28;B64G1/32;B64G1/36;B64G1/42;G01C21/02;G01S5/16;G05D1/08;(IPC1-7):G01C21/24 主分类号 B64G1/26
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