Handover between ATC and satellite component of an integrated MSS/ATC system

• US 8,463,178 B2
• Filed: 06/05/2006
• Issued: 06/11/2013
• Est. Priority Date: 06/05/2006
• Status: Active Grant

• Current Assignee: Globalstar Incorporated
• Original Assignee: Globalstar Incorporated
• Inventors: Monte, Paul A., Gallagher, Vijaya, Shah, Brinda T.
• Primary Examiner(s): Nguyen, David Q
• Application Number:
  US11/446,992
• Publication Number:
  US 20070281609A1
• Time in Patent Office: 2,563 Days
• Field of Search: 455/427, 455/430
• US Class Current: 455/12.1
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: H04B 7/18563 Arrangements for interconnecting multiple systems data switching networks H04L12/00
• CPC Class Codes: H04B 7/19 Earth-synchronous stations

Abstract

A communications system comprising a first transceiver and a second transceiver, which system employs a device that measures power over a frequency band from sources other than those monitoring downlink radiation received at a radio terminal from the satellite, and a controller that receives these power measurements to determine on which frequency channel within a band a transmitter is to transmit.

Claims

1. A communication system comprising:

at least a first radio terminal comprising a first transceiver including at least a first receiver and at least a first transmitter that communicates by way of a satellite using a satellite frequency band;

at least a second radio terminal comprising a second transceiver including at least a second receiver and at least a second transmitter that communicates by way of the satellite using the satellite frequency band and that selectively communicates with the first radio terminal via a wireless terrestrial link using a portion of the satellite frequency band so as to terrestrially reuse the portion of the satellite frequency band;

a device, collocated with the first transceiver, that measures power received by the satellite over a frequency band from all sources including the wireless terrestrial link, and transmitted from the satellite to the first receiver; and

a controller that receives and processes said measurements to determine in which frequency channel within the satellite frequency band the second transmitter is to transmit.

2. The communication system as defined in claim 1 wherein the power measurements are transmitted over a control channel.

3. The communication system as defined in claim 1 wherein said first transceiver communicates with a plurality of a second set of transceivers.

4. The communication system as defined in claim 3 wherein the first transceiver measures the interference or power from each transceiver in the second set of transceivers.

5. A communication system comprising:

at least a first radio terminal comprising a first transceiver including at least a first receiver and at least a first transmitter that communicates by way of a satellite using a satellite frequency band;

at least a second radio terminal comprising a second transceiver including at least a second receiver and at least a second transmitter that communicates by way of the satellite using the satellite frequency band and that selectively communicates with the first radio terminal via a wireless terrestrial link using a portion of the satellite frequency band so as to terrestrially reuse the portion of the satellite frequency band;

said at least first transceiver communicating to said at least second transceiver power measurements received by the satellite over a frequency band from all sources including the wireless terrestrial link, and transmitted from the satellite to the first receiver; and

a controller in said at least second transceiver that receives and processes said measurements to determine on which frequency channel within a band the at least second transmitter is to transmit.