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. The satellite communication system further includes a closed loop power control system (80) having a plurality of inner loops (84), individual ones of which operate to compensate one of the user links for communication signal impairments occurring at least between the user terminal and the at least one satellite communication repeater, and an outer loop (82) which operates to compensate all of the user links for feeder link impairments occurring between the at least one ground station and the at least one satellite communication signal repeater.
申请公布号 US5619525(A) 申请公布日期 1997.04.08
申请号 US19950467209 申请日期 1995.06.06
申请人 GLOBALSTAR L.P. 发明人 WIEDEMAN, ROBERT A.;SITES, MICHAEL J.
分类号 H04B7/26;H04B1/38;H04B7/005;H04B7/15;H04B7/185;H04B7/195;H04B7/216;(IPC1-7):H04B15/00;H04K1/00;H04L27/30 主分类号 H04B7/26
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