发明名称 SATELLITE ANTENNA DIRECTION SYSTEM
摘要 PROBLEM TO BE SOLVED: To reduce weight and improve reliability of a satellite antenna direction system without requiring reflector position adjustment mechanism. SOLUTION: This system is provided with a satellite main body 13, a reflector antenna 20 fixed on the satellite main body 13, a reflector direction error sensor 24 generating direction error signals, a reflector adjustment device 31 positioning the satellite main body 13 in response to generated reflector direction error signal, a phased array assembly 22 mounted on the reflector antenna 20, an array direction error sensor 35 mounted on the phased array assembly 22, and a phased array control device 40 adjusting direction of the phased array assembly 22 in response to generated array direction error signals.
申请公布号 JP2001097300(A) 申请公布日期 2001.04.10
申请号 JP20000242517 申请日期 2000.08.10
申请人 HUGHES ELECTRONICS CORP 发明人 LANE STEVEN O
分类号 B64G1/66;B64G1/28;G01S19/25;H01Q1/28;H01Q3/02;H01Q3/08;H01Q3/26;H01Q3/30;H01Q19/17;H01Q21/30;H01Q25/00;H04B7/08;H04B7/10;H04B7/195;(IPC1-7):B64G1/66 主分类号 B64G1/66
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