发明名称 Closed loop power control for low earth orbit satellite communications system
摘要 A satellite communication system (10) includes at least one satellite communication signal repeater (12); at least one ground station (18) for transmitting a feeder link comprised of a plurality of communication signals to the at least one satellite communication signal repeater; and a plurality of user terminals (13) each receiving one of the communication signals over a user link from the at least one satellite communication signal repeater. A method includes steps of measuring a quality of at least one reference signal received by the user terminal, via the satellite; transmitting the measured quality of the reference signal received by the user terminal to the ground station; comparing the measured quality with a predetermined reference; and adjusting a transmit power of the ground station in response to a difference between the predetermined reference and measured quality. The transmit power of the ground station is adjusted so that a flux density of a downlink beam is substantially constant at the user terminal independent of the location of the user terminal in the beam.
申请公布号 US6240124(B1) 申请公布日期 2001.05.29
申请号 US19990432301 申请日期 1999.11.02
申请人 GLOBALSTAR L.P. 发明人 WIEDEMAN ROBERT A.;SITES MICHAEL J.
分类号 H04B7/15;H04B7/185;(IPC1-7):A61F2/06 主分类号 H04B7/15
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