Method and system for transmitting radio signals between a fixed terrestrial station and user mobile terminals via a network of satellites

• US 5,765,098 A
• Filed: 07/08/1996
• Issued: 06/09/1998
• Est. Priority Date: 01/02/1995
• Status: Expired due to Fees

• Current Assignee: Agence Spatiale Europeenne
• Original Assignee: Agence Spatiale Europeenne
• Inventors: Bella, Luigi
• Primary Examiner(s): Urban, Edward F.
• Application Number:
  US08/676,802
• Time in Patent Office: 701 Days
• Field of Search: 455/12.1, 455/13.1, 455/13.2, 455/13.3, 455/25, 455/33.1, 455/62, 455/63, 455/428, 455/429, 455/430, 342/352, 370/319, 370/320
• US Class Current: 455/13.3
• CPC Class Codes: H04B 7/18539 Arrangements for managing radio, resources, i.e. for establishing or releasing a connection
• CPC Class Codes: H04B 7/2041 Spot beam multiple access

Abstract

The invention concerns a method and a system for transmitting radio signals between a fixed terrestrial station and mobile user terminals via a network of satellites in inclined circular orbits having a radius less than that of geostationary orbits. The beams generated are divided into pencil beams each associated with a continuous sub-band of frequencies in increasing frequency or decreasing frequency order. The instantaneous transmission frequency is offset progressively during the call towards the frequency subband of the adjacent pencil beam, at a rate proportional to the orbital rotation speed, to enable switching between pencil beams or between satellites. Applications include transmission via satellites in non-geostationary orbit.

Claims

1. Method of transmitting radio signals via a satellite network between at least one fixed terrestrial station and user terminals, wherein the satellite network comprises a plurality of satellites rotating about a terrestrial globe in a circular orbit and at a particular rotation speed, wherein the orbits are inclined to an equator and have a radius less than that of geostationary orbits, wherein the satellites are triply geosynchronous, and wherein each satellite comprises an arrangement of antennas for generating at least one beam with a radiation pattern directed towards a surface of the terrestrial globe and associated with a frequency band of frequencies of particular bandwidth, the method comprising at least the following steps:

dividing said beam into a particular number of contiguous pencil beams, wherein said each of said pencil beams is associated with a frequency sub-band and wherein said frequency sub-band is a subdivision of said particular bandwidth;

setting up a communication link in at least one direction between said one fixed terrestrial terminal station and a first user terminal of said user terminals via a first satellite of said satellite network, wherein a first portion of said communication link between said first satellite and said first user terminal is set up by using an instantaneous transmission frequency in a first frequency sub-band associated with a first pencil beam which illuminates said first user terminal when said first satellite flies over said first user terminal and wherein a second portion of said communication link is set up between said first satellite and said one fixed terrestrial terminal station; and

progressively shifting said transmission frequency during a period of the first portion of said communication link towards a second frequency sub-band associated with an adjacent pencil beam and at a rate proportional to said particular rotation speed so as to compensate said rotation and to enable tracking of said satellite.

2. Method according to claim 1, wherein said frequency sub-bands have equal width and said frequency sub-bands form a continuous spectrum so that contiguous pencil beams are associated with contiguous frequency sub-bands evolving in a particular direction.

3. Method according to claim 2, wherein, in said frequency shifting step, said instantaneous transmission frequency jumps from an initial frequency in said first frequency sub-band to a final frequency in the second frequency sub-band associated with said adjacent pencil beam so as to achieve switching between pencil beams without blocking.

4. Method according to claim 2, wherein said frequency sub-bands associated with said pencil beams of said first satellite are in an opposite direction from frequency sub-bands associated with pencil beams of a second satellite so that when a last pencil beam of a first satellite associated with a particular freauency sub-band ceases to illuminate said first user terminal, the first user terminal is illuminated by a first pencil beam of the second satellite and wherein said first pencil beam of the second satellite is associated with said particular frequency sub-band so as to achieve switching between satellites without blocking.

5. Method according to claim 4, wherein footprints of said last pencil beam of said first satellite and said first pencil beam of said second satellite at least partially overlap at the surface of the terrestrial globe so that switching between satellites is progressive.

6. Method according to claim 1, wherein said pencil beams are highly elliptical and each have a major axis which is orthogonal to a direction of movement of the first satellite of said satellite network illuminating said user terminals during a call.

7. Method according to claim 6, wherein each pencil beam is divided into a particular number of sub-pencil beams.

8. Method according to claim 1, wherein said communication link is a full duplex link and in that "out" and "return" transmissions have mutually orthogonal crossed polarizations.

9. Method according to claim 1, wherein a frequency-division multiple access protocol is used to distinguish between said pencil beams and a direct sequence code-division multiple access protocol is used to distinguish data within said pencil beams.

10. Method according to claim 1, wherein pencil beams from said satellites of said satellite network illuminating an area of the terrestrial globe between two latitudes of a particular value on either side of the equator of said terrestrial globe are momentarily interrupted in order to prevent interference with geostationary satellite systems operating in transmission frequency bands including said instantaneous transmission frequency.

11. Method according to claim 10, wherein said area of said terrestrial globe is located between +9°

latitude and -9°

latitude.

12. A method of transmitting radio signals between a first user terminal and a satellite network comprising a first satellite which rotates around a terrestrial body at a particular rotation speed, the method comprising the steps of:

(a) dividing a frequency beam generated by said satellite into a predetermined number of contiguous pencil beams, wherein said frequency beam is associated with a frequency band having a particular bandwidth, wherein said pencil beams are respectively associated with frequency sub-bands, and wherein said frequency sub-bands respectively relate to subdivisions of said particular bandwidth;

(b) setting up a communication link between said first user terminal and said first satellite by using an instantaneous transmission frequency in a first frequency sub-band associated with a first pencil beam which illuminates said first user terminal when said first satellite flies over said first user terminal; and

(c) progressively shifting said instantaneous transmission frequency during a period of the communication link towards a second frequency sub-band associated with an adjacent pencil beam, wherein said instantaneous transmission frequency is shifted at a rate proportional to said particular rotation speed of said first satellite.

13. The method according to claim 12, wherein said frequency sub-bands form a continuous spectrum so that contiguous pencil beams are associated with contiguous frequency sub-bands evolving in a particular direction.

14. The method according to claim 13, wherein said step (c) comprises the step of:

(c1) shifting said instantaneous transmission frequency from an initial frequency in said first frequency sub-band to a final frequency in the second frequency sub-band associated with said adjacent pencil beam so as to achieve switching between said first pencil beam and said adjacent pencil beam without blocking.

15. The method according to claim 13, wherein said frequency sub-bands associated with said pencil beams of said first satellite are arranged in an opposite direction from frequency sub-bands associated with pencil beams of a second satellite in said satellite network,

wherein a last pencil beam of said first satellite and a first pencil beam of said second satellite are both associated with a particular frequency sub-band, and

wherein said last pencil beam of said first satellite and said first pencil beam of said second satellite illuminate said first user terminal so as to achieve switching between satellites without blocking.

16. The method according to claim 15, wherein footprints of said last pencil beam of said first satellite and said first pencil beam of said second satellite at least partially overlap at a surface of the terrestrial body so that switching between satellites is progressive.

17. A system comprising a satellite network, at least one fixed terrestrial station, and user terminals, for transmitting radio signals via said satellite network between said at least one fixed terrestrial station and said user terminals, wherein the satellite network comprises a plurality of satellites rotating about a terrestrial globe in a circular orbit and at a particular rotation speed, wherein the orbits are inclined to an equator and have a radius less than that of geostationary orbits, wherein the satellites are triply geosynchronous, and wherein each satellite comprises an arrangement of antennas for generating at least one beam with a radiation pattern directed towards a surface of the terrestrial globe and associated with a frequency band of frequencies of particular bandwidth, the system comprising:

means for dividing said beam into a particular number of contiguous pencil beams, wherein said each of said pencil beams is associated with a frequency sub-band and wherein said frequency sub-band is a subdivision of said particular bandwidth;

means for setting up a communication link in at least one direction between said one fixed terrestrial terminal station and a first user terminal of said user terminals via a first satellite of said satellite network, wherein a first portion of said communication link between said first satellite and said first user terminal is set up by using an instantaneous transmission frequency in a first frequency sub-band associated with a first pencil beam which illuminates said first user terminal when said first satellite flies over said first user terminal and wherein a second portion of said communication link is set up between said first satellite and said one fixed terrestrial terminal station; and

means for progressively shifting said transmission frequency during a period of the first portion of said communication link towards a second frequency sub-band associated with an adjacent pencil beam and at a rate proportional to said particular rotation speed so as to compensate said rotation and to enable tracking of said satellite.

18. The system according to claim 17, wherein said first satellite and said first user terminal comprise scanning antennas for providing said communication link.

19. The system according to claim 17, wherein said satellites and said user terminals comprise scanning antennas for establishing communication paths for said radio signals.

20. The system according to claim 17, wherein said antennas are of the frequency scanning type.

21. The system according to claim 20, wherein each of said pencil beams are divided into a particular number of sub-pencil beams,

wherein said satellites each comprise a first set of N transmit antennas and a second set of N receive antennas for "out" and "return" communication links between said satellites and said user terminals,

wherein N equals said particular number,

wherein each transmit and receive antenna is associated with one of said sub-pencil beams,

wherein each satellite further comprises an additional transmit antenna and an additional receive antenna for "out" and "return" communication links between said satellites and said at least one terrestrial terminal stations, and

wherein said transmit antennas, said receive antennas, said additional transmit antenna, and said additional receive antennas are frequency scanning antennas.

22. The system according to claim 20, wherein said user terminals are provided with deployable antennas which have an active state and a passive state,

wherein said antennas are deployed and communication links can be provided during said active state,

wherein said antennas are folded up and the user terminals only can be called during said passive state, and

wherein said antennas are frequency scanning antennas.