发明名称 Rapid satellite acquisition device
摘要 A system and method for acquiring a satellite with an antenna using a computing portion which determines the variation between the actual orientation of the antenna and an optimum orientation to acquire a satellite. The deviation is computed by: determining the actual orientation of the antenna with respect to true North and producing a first signal indicative thereof; determining the location of the antenna on the Earth and producing a second signal indicative thereof; determining the elevation of the satellite with respect to the location of the antenna and producing a third signal indicative thereof; determining the azimuth of the satellite with respect to the location of the antenna and producing a fourth signal indicative thereof; and using log data for the satellite along with the first, second, third, and fourth signals to compute the position of the satellite relative to the antenna and produce a signal indicative of the deviation. A display is used for illustrating the deviation and can be used as a coarse adjustment device. A second display provides information as to the received signal strength from the satellite to the antenna and can be used as a fine adjustment device. The coarse and the fine adjustment devices interact to provide an effective technique to acquire the satellite.
申请公布号 US5583514(A) 申请公布日期 1996.12.10
申请号 US19940337754 申请日期 1994.11.14
申请人 LORAL AEROSPACE CORP. 发明人 FULOP, DONALD G.
分类号 H01Q1/12;(IPC1-7):H01Q3/00 主分类号 H01Q1/12
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