发明名称 GPS gyro calibration
摘要 GPS gyro calibration methods and systems are described. In an embodiment, a ground station can receive antenna position data for a spot beam antenna from a global positioning system (GPS) platform where the antenna position data indicates a boresight direction of the spot beam antenna. GPS-enabled receiver(s) can receive scan signals transmitted via the spot beam antenna of the GPS platform, and the GPS-enabled receivers can determine signal power measurements for each of the scan signals. The ground station can receive the signal power measurements from the GPS-enabled receiver(s) and estimate a pointing error of the spot beam antenna based on the signal power measurements and the antenna position data received from the GPS platform. The ground station can then determine gyro calibration parameters from the estimated pointing error and communicate the gyro calibration parameters to the GPS platform to calibrate for gyro drift errors.
申请公布号 US7667645(B2) 申请公布日期 2010.02.23
申请号 US20060420427 申请日期 2006.05.25
申请人 THE BOEING COMPANY 发明人 TEKAWY JONATHAN A;O'BRIEN KEVIN M
分类号 H01Q3/00 主分类号 H01Q3/00
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