发明名称 Sensor system and method for determining yaw orientation of a satellite
摘要 A first pair of antennas are mounted on a satellite spaced along a first axis and a second pair of antennas are spaced along a second axis for receiving signals from another satellite in orbit with the satellite, the first and second axes being orthogonal to a yaw axis that points toward the centroid of the celestial body about which the satellite orbits. Each pair of antennas are used to derive phase angle and signal strength differences, and these differences are used for deducing a yaw orientation of the satellite about the yaw axis.
申请公布号 US2002140606(A1) 申请公布日期 2002.10.03
申请号 US20010824190 申请日期 2001.04.02
申请人 THE BOEING COMPANY 发明人 DAVIS JOHN E.;LIAO HENRY H.
分类号 G01S3/14;G01S3/28;G01S3/38;G01S5/02;G01S19/19;(IPC1-7):G01S5/04 主分类号 G01S3/14
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