发明名称 |
A digitally controlled beam former for a spacecraft. |
摘要 |
<p>A digitally controlled beam former for a spacecraft which includes means for periodically calibrating the feed paths of the spacecraft's antenna array by measuring the apparent movement of the centre of a reference signal and a nominal signal and utilising the measured data to compensate for at least the phase drift in the antenna feed paths. The measured data may also be used to compensate for amplitude and phase drift in the antenna feed paths. <IMAGE></p> |
申请公布号 |
EP0642191(A1) |
申请公布日期 |
1995.03.08 |
申请号 |
EP19940303163 |
申请日期 |
1994.04.29 |
申请人 |
MATRA MARCONI SPACE UK LIMITED |
发明人 |
SHAWYER, ROGER JOHN |
分类号 |
H01Q3/26;(IPC1-7):H01Q3/26 |
主分类号 |
H01Q3/26 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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