Cost effective geosynchronous mobile satellite communication system

• US 5,589,834 A
• Filed: 04/22/1994
• Issued: 12/31/1996
• Est. Priority Date: 04/22/1994
• Status: Expired due to Term

• Current Assignee: Exelis Incorporated (L3Harris Technologies, Inc.)
• Original Assignee: Stanford Telecommunications, Inc. (Nokia Corporation)
• Inventors: Weinberg, Aaron
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US08/231,711
• Time in Patent Office: 984 Days
• Field of Search: 342/353, 342/354, 342/356, 455/12.1, 455/13.1, 455/13.3
• US Class Current: 342/354
• CPC Class Codes: H04B 7/19 Earth-synchronous stations
• CPC Class Codes: Y02D 30/70 in wireless communication networks

Abstract

A satellite communication system including one or more satellites in geosynchronous orbit and inclined at a predetermined angle greater than 0° relative to earth, a preferred angle being about 28.5° for full earth coverage, there is a constellation of satellites. Each satellite has a multi-element phased array antenna and transmit and receive circuits selectively connected to said multi-element phased array antenna for providing spatially discriminated spot radiation beams on the earth'"'"'s surface, and a steerable spaced/ground antenna and transmitter-receiver circuitry connected thereto. At least one gateway ground terminal having means for performing all spacecraft command and control, including uplink phasing of said phased array antenna for directive satellite transmissions to desired user locations. Tracking the moving satellites via combination of range and doppler tracking, steering said space/ground antenna in accordance with satellite motion, performing all ground-beamforming associated with user inbound transmissions, performing all user signal modulation and demodulation, providing the necessary ground interfaces with the external cellular and terrestrial networks. A plurality of earth-based low power transceivers are provided for one and two-way communications via selected elements of said phased array antenna.

Claims

1. A satellite communication system for providing communication links between a plurality of earth-based low power transceivers and external cellular and terrestrial networks comprising:

one or more satellites in geosynchronous orbit and inclined at a predetermined angle greater than 0 relative to earth, each satellite having a multi-element phased array antenna and transmit and receive circuits selectively connected to said multi-element phased array antenna for providing spatially discriminated spot radiation beams on the earth'"'"'s surface, and a steerable spaced-to-ground antenna and transmitter-receiver circuitry connected thereto,

at least one gateway ground terminal having means for;

(1) performing uplink phasing of said phased array antenna for directive satellite transmissions to desired user locations,

(2) tracking the moving satellites via combination of range and doppler tracking,

(3) steering said space-to-ground antenna in accordance with satellite motion,

(4) performing all ground-beamforming associated with user inbound transmissions,

(5) performing all user signal modulation and demodulation,

(6) providing the necessary ground interfaces with the external cellular and terrestrial networks, and

a plurality of earth-based low power transceiver means for one and two-way communications via said selected elements of said phased array antenna.

2. The satellite communication system defined in claim 1 wherein said predetermined angle is about 28.5°

.

3. The satellite communication system defined in claim 1 or 2 wherein there is a constellation of satellites and the number of satellites in said constellation is six or less.

4. A satellite communication system for providing communication links between a plurality of earth-based low power transceivers and external cellular and terrestrial networks comprising:

a constellation of satellites in geosynchronous orbit and inclined at a predetermined angle greater than 0°

relative to earth, each satellite having a multi-element phased array antenna and transmit and receive circuits selectively connected to said multi-element phased array antenna for providing spatially discriminated spot radiation beams on the earth'"'"'s surface, and a steerable space-to-ground antenna and transmitter-receiver circuitry connected thereto,

at least one gateway ground terminal for;

(1) performing uplink phasing of said phased array antenna for directable satellite transmissions to desired user locations,

(2) tracking the moving satellites via combination of range and doppler tracking,

(3) steering said space-to-ground antenna in accordance with satellite motion,

(4) performing all ground-beamforming associated with user inbound transmissions,

(5) performing all user signal modulation and demodulation,

(6) providing the necessary ground interfaces with the external cellular and terrestrial networks, and

a plurality of earth-based low power transceiver means for one and two-way communications via said selected elements of said phased array antenna.

5. A satellite communication method for providing communication links between a plurality of earth-based low power transceivers and external cellular and terrestrial networks comprising, providing a constellation of geosynchronous satellites, inclined at about 28.5°

, each satellite having multi-element phased array antennas for providing spot beams on the earth surface to provide spatial discrimination and high gain, at least one gimballed space-to-ground antenna means and receiver and transmitter circuitry therefor, providing at least three gateway ground terminals, each said gateway ground terminal;

(1) performing uplink phasing of the phased array for directive satellite transmissions to desired user locations,

(2) tracking the moving satellites via combination of range and doppler tracking,

(3) steering the gimballed space/ground antennas in accordance with satellite motion,

(4) performing all ground-beamforming associated with user inbound transmissions,

(5) performing all user signal modulation and demodulation,

(6) providing the necessary ground interfaces with the external cellular and terrestrial networks, and

a plurality of earth-based low-power transceiver means for connecting via the multi-element phased array antenna on said constellation of satellite.

6. A data collection system for collecting data from a large number of earth-based sites and directing collected data to a central earth site, comprising:

a satellite in geosynchronous orbit, said satellite is inclined at a predetermined angle greater than 0°

relative to earth having;

multi-element phased array antenna, transmit and receive circuits selectively connected to said multi-element phased array antennas to provide a large number of simultaneous, high quality spot beams, a steerable space-to-ground antenna means and transmitter/receiver circuit connected thereto for receiving collected data from said phased array antenna and transmitting collected data to said central earth site,

a plurality of earth-based field user remote data source terminals, one data source terminal at each of said earth-based site,

each said earth-based field user remote data source terminal having means for collecting said data and transmitting collected data to a selected element to said phase array antenna, and

said central earth site including at least one gateway ground terminal for communicating with said satellite through said steerable space to ground antenna to receive said collected data from said satellite and transmit antenna control signals to said satellite to dynamically configure said phased array antenna for given areas of the earth.

7. The data collection system defined in claim 6 wherein said plurality of field user remote data source terminals are adapted to perform one or more of the following data collection services:

1) meter reading,

2) remote mobile tracking,

3) scientific data collection,

4) search and rescue,

5) aircraft traffic surveillance.

8. The data collection system defined in claim 6 wherein there is a constellation of said satellites in geosynchronous orbit and each satellite is inclined at a predetermined angle greater than 0°

relative to earth.

9. The data collection system defined in claim 8 wherein said predetermined angle is about 28.5°

.

10. The data collection system defined in claim 9 wherein the number of satellites in said constellation is six or less.