发明名称 Sun sensor alignment compensation system
摘要 A method for correcting differences in measurements between sensors. Misalignment of a roll error of a sun sensor alignment is estimated with respect to a reference roll value measured by an earth sensor. Sun sensor assembly elevation angle residual is calculated utilizing the estimated sun sensor assembly roll misalignment. A yaw attitude of the spacecraft is updated based upon the calculated sun sensor assembly elevation residual.
申请公布号 US6629672(B1) 申请公布日期 2003.10.07
申请号 US20020092636 申请日期 2002.03.08
申请人 LOCKHEED MARTIN CORPORATION 发明人 GOODZEIT NEIL EVAN;LI XIPU
分类号 B64G1/36;G05D1/08;(IPC1-7):B64G1/36 主分类号 B64G1/36
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