Closed loop power control for low earth orbit satellite communications system

• US 6,097,752 A
• Filed: 04/04/1997
• Issued: 08/01/2000
• Est. Priority Date: 06/06/1995
• Status: Expired due to Term

• Current Assignee: Globalstar Incorporated
• Original Assignee: Globalstar Incorporated
• Inventors: Sites, Michael J., Wiedeman, Robert A.
• Primary Examiner(s): Vo, Don N.
• Application Number:
  US08/832,644
• Time in Patent Office: 1,215 Days
• Field of Search: 375/200, 375/211, 375/221, 375/358, 455/10, 455/13.4, 455/69, 455/522, 370/318
• US Class Current: 375/130
• CPC Class Codes: H04B 7/18543 for adaptation of transmission parameters, e.g. power control for detecting or preventing errors in the information received H04L1/00

Abstract

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.

Claims

1. A method for operating a satellite communication system, comprising the steps of:

transmitting at least one reference signal to a satellite on a feederlink, the at least one reference signal being transmitted by a terrestrial gateway in conjunction with communication signals that are transmitted to a plurality of user terminals;

repeating the at least one reference signal with the satellite to provide at least one downlink reference signal having a frequency that is less than the feederlink frequency;

receiving the at least one downlink reference signal with a reference signal receiver;

deriving an estimate of feederlink losses from the at least one received downlink reference signal; and

controlling a transmitted power of the feederlink to compensate for the estimated feederlink losses.

2. A method as in claim 1, wherein the at least one reference signal is transmitted on the feederlink with a predetermined spreading code by the gateway, and wherein the downlink reference signal is received, despread, and demodulated by the reference signal receiver.

3. A method as in claim 1, wherein the gateway transmits a plurality of feederlinks to a plurality of satellites, each feederlink containing at least one reference signal, wherein a distinct spreading code is assigned to each reference signal, and wherein the reference signal receiver simultaneously receives and despreads a plurality of the downlink reference signals.

4. A method as in claim 1, wherein the gateway simultaneously transmits a plurality of feederlinks to a plurality of satellites, each feederlink containing at least one reference signal, wherein a distinct spreading code is assigned to each reference signal, and wherein the reference signal receiver receives and despreads individual ones of the downlink reference signals in a time-multiplexed manner.

5. A method as in claim 1, wherein the satellite is one satellite of a constellation of low earth orbit satellites.