Frequency and polarization allocation for satellite telecommunication systems

• US 6,374,104 B1
• Filed: 03/01/2000
• Issued: 04/16/2002
• Est. Priority Date: 06/26/1997
• Status: Expired due to Fees

• Current Assignee: Alcatel SA (Nokia Corporation)
• Original Assignee: Alcatel SA (Nokia Corporation)
• Inventors: Casasoprana, Didier, Dolmeta, Florence, Croq, Frédéric, Voisin, Philippe
• Primary Examiner(s): Chang, Vivian
• Assistant Examiner(s): Nguyen, Duc
• Application Number:
  US09/446,424
• Time in Patent Office: 776 Days
• Field of Search: 455/12.1, 455/13.1, 455/13.2, 455/13.3, 455/427, 455/428, 455/429, 455/446, 455/447, 455/450, 455/451, 455/452, 370/316, 370/322, 370/329
• US Class Current: 455/427
• CPC Class Codes: H04B 7/2041 Spot beam multiple access

Abstract

The invention concerns a telecommunications system in which the Earth is divided into areas (26) within which communications are effected by means of transmit and receive means on a spacecraft, such as a satellite, allocated to communication for a plurality of areas. Areas (26₁₀, 26₁₁, 26₁₂) of a first category (28) are allocated signals having respective polarizations (P_D, P_G) and carrier frequencies (ΔF₁, ΔF₂) such that two adjacent areas of the first category are allocated signals having different polarizations or carrier frequencies. Each area of a second category (30) is allocated signals having all the available polarizations and all the available carrier frequencies.

Claims

1. A telecommunications system in which the Earth is divided into a plurality of areas, the system comprising a spacecraft including a transmit and receive system allocated to said areas for effecting communications within said areas, wherein each of said areas is designated as a first category or a second category, said areas of said first category are allocated signals having respective polarizations and carrier frequencies such that two adjacent areas of the first category are allocated signals having different polarizations or carrier frequencies, and said areas of said second category are allocated signals having all available polarizations and all available carrier frequencies.

2. A system according to claim 1, wherein the polarization of the signals is circular.

3. A system according to claim 1, wherein at least two separate bands of carrier frequencies are provided for the signals, and the widths of the separate bands being equal or unequal.

4. A system according to claim 1, wherein the areas of the first category are allocated to low call densities and in that the areas of the second category are allocated to higher call densities.

5. A system according to claim 1, wherein in each of said areas, the signals are transmitted and received by users and by at least one connection station.

6. A system according to claim 5, wherein the separate areas communicate via terrestrial links between connection stations.

7. A system according to claim 1, wherein said transmit and receive system comprises a plurality of transmit and receive antennas allocated to said areas of the first category transmit for receiving and transmitting only signals having the polarization and the frequencies provided for said areas of the first category.

8. A system according to claim 1, wherein the spacecraft comprises a satellite in low Earth orbit, said transmit and receive system comprises a plurality of transmit and receive antennas provided for each of said areas, and each of said transmit and receive antennas is pointed towards an associated area for as long as the satellite remains in view of the associated area.

9. A system according to claim 8, wherein said transmit and receive antennas which are associated with said areas of the first category employ electronic pointing and reconfiguration.

10. A system according to claim 9, wherein said transmit and receive antennas comprise a set of radiating elements.

11. A system according to claim 5, wherein for areas of the first category, said transmit and receive system comprises a plurality of active transmit and receive antennas which employ electronic pointing and reconfiguration, and said transmit and receive antennas comprise sets of radiating elements for receiving signals from the connection station and from the users.

12. A system according to claim 5, wherein for areas of the first category, said transmit and receive system includes a plurality of active transmit and receive antennas which employ electronic pointing and reconfiguration, and said transmit and receive antennas comprise radiating elements for transmitting to users and radiating elements for transmitting to connection stations.

13. A system according to claim 8, wherein each of said transmit and receive antennas which are associated with said areas of the second category include mechanical means for pointing the antenna towards the area.

14. A system according to claim 13, wherein each of the said transmit and receive antennas includes means for modifying the radiation pattern as a function of the relative position of the spacecraft and the corresponding area in order to match the pattern to the shape of the area as seen by the antenna.

15. A system according to claim 14, wherein said transmit and receive antennas include radiating elements and the means for modifying the radiation pattern modify the pattern by modifying the amplitudes of the signals fed to the radiating elements.

16. A system according to claim 14, wherein said transmit and receive antennas include radiating elements and the means for modifying the radiation pattern modify the pattern by modifying the amplitudes and the phases of the signals fed to the radiating elements.

17. A system according to claim 15, a plurality of said radiating elements receive the same amplitude.

18. A system according to claim 13, said transmit and receive antennas have a surface that can be oriented by means of an azimuth motor and an elevation motor.

19. A system according to claim 13, wherein said transmit and receive antennas include a transmit part and a receive part which are separate.

20. A system according to claim 13, wherein said transmit and receive antennas include a ferrite-based beam-forming circuit is provided for transmission.

21. A system according to claim 13, the transmit and receive antennas include a set of radiating elements arranged on an elongate surface.

22. A transmit-receive system on a spacecraft for use in a telecommunications system in which the Earth is divided into a plurality of areas within which communications are effected via the transmit-receive system, the areas being designated as a first category having low call densities or a second category having high call densities, the transmit-receive system comprising:

a first transmit-receive antenna allocated to one of the areas of the first category; and

a second transmit-receive antenna allocated to one of the areas of the second category, said fist and second transmit-receive antenna being different antenna types transmit-receive antenna, wherein said areas of said first category are allocated signals having respective polarizations and carrier frequencies such that two adjacent areas of the first category are allocated signals having different polarizations or carrier frequencies, and said areas of said second category are allocated signals having all available polarizations and all available carrier frequencies.

23. A transmit-receive system according to claim 22, wherein the spacecraft is a satellite in low Earth orbit and said first and second transmit-receive antennas are pointed towards the areas respectively associated with the first and second transmit-receive antennas as long as the satellite remains in view of that area, the first transmit-receive antenna includes means for electronic pointing and reconfiguration and the second antenna includes means for mechanically pointing the antenna towards the area.

24. A system according to claim 23, wherein the second antenna includes means for electronically reconfiguring a shape of the transmit and receive pattern.

25. A telecommunication method in which the Earth is divided into a plurality of areas within which communications are effected by transmit and receive means on a spacecraft allocated to communication within said areas, wherein each of the areas is designated as being a first category or a second category, the method comprising:

allocating to the areas of the first category signals having respective polarizations and carrier frequencies such that two adjacent areas of the first category are allocated signals having different polarizations or carrier frequencies, and

allocating to the areas of the second category signals having all available polarizations and all available carrier frequencies.

26. A method according to claim 25, wherein the areas of the first category are allocated to low call densities and the areas of the second category are allocated to higher call densities.