Burst signal transmission from an earth station to an orbiting satellite with a short guard time

• US 5,991,598 A
• Filed: 08/11/1997
• Issued: 11/23/1999
• Est. Priority Date: 06/30/1993
• Status: Expired due to Fees

• Current Assignee: NEC Corporation
• Original Assignee: NEC Corporation
• Inventors: Nawata, Hizuru
• Primary Examiner(s): Chin, Wellington
• Assistant Examiner(s): SOBUTKA, PHILIP
• Application Number:
  US08/907,866
• Time in Patent Office: 834 Days
• Field of Search: 455/13.2, 455/13.1, 455/12.1, 455/427, 455/428, 455/429, 455/430, 370/252, 370/253, 370/324, 370/503, 370/508
• US Class Current: 455/13.1
• CPC Class Codes: H04B 7/18532 Arrangements for managing transmission, i.e. for transporting data or a signalling message
• CPC Class Codes: H04B 7/2041 Spot beam multiple access
• CPC Class Codes: H04B 7/2125 Synchronisation

Abstract

Radiated from each orbiting satellite of a satellite communication network to M cells (M representing an integer, such as thirty-seven) covered with a predetermined solid angle on the earth, M spot beams are identified by M identification codes. In an earth station which may be a portable unit, a burst signal transmitter device (31) comprises a receiver part (35) receiving one of the spot beams as a received beam at a reception time, to recognize as a recognized code one of the identification codes that identifies the received beam, and a transmitter part (45) for transmitting burst signals at a transmission time delayed from the reception time by an offset amount selected by the recognized code from M offset amounts predetermined for the identification codes. Preferably, the M offset amounts are stored in a memory (43).

Claims

1. A burst signal transmitting method of transmitting a burst signal from an earth station of a satellite communication network including a predetermined number of orbiting satellites, comprising the steps of;

beam transmitting from each of said satellites M spot beams with M identification codes superposed on said spot beams, respectively, where M represents an integer which is equal to at least two, said identification codes being individually specific to said spot beams and for identification and recognition of said spot beams;

beam receiving in said earth station one of said spot beams as a received beam at a reception time instant from one of said satellites;

beam recognizing said one of said spot beams by one of said identification codes that is superposed on said received beam; and

a signal transmitting said burst signal to said one of said satellites at a transmission time instant following said reception time instant by an offset amount selected from M offset amounts predetermined for said identification codes, respectively, said offset amount being selected by said earth station in response to said one of said identification codes.

2. A burst signal transmitting method as claimed in claim 1, wherein said beam transmitting step comprises the steps of:

superposing said identification codes on M carrier signals to produce superposed signals;

modulating each of superposed signals by modulating signals into a modulated signal; and

transmitting said modulated signal as one of said spot beams.

3. A burst signal transmitting method as claimed in claim 2, said carrier signals being in one-to-one correspondence to said identification codes, wherein:

said superposing step comprises the step of superposing each identification code one corresponding one of said carrier signals at predetermined superposition time instants to provide a superposed signal;

said modulating step comprising the step of modulating said superposed signal by said modulating signals with reference to said superposition time instants.

4. A burst signal transmitting method as claimed in claim 1, wherein:

said beam receiving step comprises the steps of;

receiving said one of spot beams as said received beam at said reception time instant; and

demodulating said received beam into a demodulated signal including said one of identification codes;

said beam recognizing step comprising the step of recognizing said one of spot beams by locating said one of identification codes in said demodulated signal.

5. A burst signal transmitting method as claimed in claim 4, wherein said signal transmitting step comprises the step of:

storing said offset amounts as stored amounts; and

selecting one of said stored amounts as said offset amount in response to said demodulated signal.

6. A burst signal transmitter device of an earth station of a satellite communication network including a predetermined number of orbiting satellites, each satellite radiating M spot beams identified by M identification codes, respectively, where M represents an integer which is equal at least to two, said identification codes being individually specific to said spot beams and for identification and recognition of said spot beams, said burst signal transmitter device transmitting a burst signal to one of said satellites that irradiates said earth station by one of said spot beams, said burst signal transmitter device comprising:

receiver means for receiving said one of said spot beams from said one of said satellites as a received signal at a reception time instant;

recognizing means for recognizing said one of said spot beams by one of said identification codes that identifies said received signal; and

transmitter means for transmitting said burst signal to said one of said satellites at a transmission time instant following said reception time instant by an offset amount selected from M offset amounts predetermined for said identification codes, respectively, said offset amount being selected by said earth station in response to said one of said identification codes.

7. A burst signal transmitter device as claimed in claim 6, wherein:

said receiver means comprises demodulator means for demodulating said one of spot beams into a demodulated signal used as said received signal;

said recognizing means recognizing, to produce a recognition signal indicative of said one of identification codes, that said demodulated signal is derived from said one of spot beams with said one of identification codes included in said demodulated signal.

8. A burst signal transmitter device as claimed in claim 7, said one of spot beams being modulated by a burst signal carrying data information directed to said earth station, wherein said demodulator means further demodulates said demodulated signal into said data information.

9. A burst signal transmitting device as claimed in claim 7, wherein said transmitter means comprises:

memory means in which said offset amounts are stored as stored amounts;

selecting means responsive to said recognition signal for selecting said offset amount from said stored amount as a selected amount; and

delay means for delaying transmission of said burst signal by said selected amount from said reception time instant.

10. A burst signal transmitter device as claimed in claim 9, wherein said burst signal is supplied to said delay means with data information carried thereby.

11. A transponder mounted on an orbiting satellite of a satellite communication network including a plurality of earth stations, wherein said transponder comprises transmitter means for transmitting M spot beams to said earth stations with M identification codes superposed on said spot beams, respectively, where M represents an integer which is equal at least to two, said identification codes being individually specific to said spot beams and for identification and recognition of said spot beams, each said earth station transmitting a burst signal to said transponder with a guard time based on which of said spot beams was transmitted to said earth station, to achieve alignment of said burst signal in time slots on said transponder with burst signals transmitted to said transponder from others of said earth stations.

12. A transponder as claimed in claim 11, wherein said transmitter means comprises:

carrier generating means for generating M carrier signals;

superposing means for superposing said identification codes on said carrier signals, respectively, to produce M code superposed signals; and

spot beam transmitting means for transmitting said code superposed signals as said spot beams, respectively.

13. A transponder as claimed in claim 12, wherein said spot beam transmitting means comprises means for time division modulating each of said code superposed signals by at least one modulating signal into a modulated signal for transmission as one of said spot beams.

14. A transponder as claimed in claim 13, said satellite communication network including a prescribed number of adjacent satellites having a substantially predetermined positional relationship to said orbiting satellite, said transponder covering a solid angle by said spot beams and further comprising receiver means for receiving intersatellite link signals from said adjacent satellites and at least one uplink signal from at least one of said earth stations that is currently present in said solid angle, said receiving means detecting in said intersatellite link and said uplink signals at least one received signal for use as said at least one modulating signal for transmission into said solid angle.

15. A transponder as claimed in claim 11, wherein said transmitter means comprises:

carrier generating means for generating M carrier signals;

modulator means for time division modulating each of said carrier signals by at least one modulating signal to produce M modulated signals from said carrier signals; and

superposing means for superposing said identification codes on said modulated signals, respectively, to produce M code superposed signals for transmission as said spot beams, respectively.

16. A transponder as claimed in claim 15, said satellite communication network including a prescribed number of adjacent satellites having a substantially predetermined positional relationship to said orbiting satellite, said transponder covering a solid angle by said spot beams and further comprising receiver means for receiving intersatellite link signals from said adjacent satellites and at least one uplink signal from at least one of said earth stations that is currently present in said solid angle, said receiving means detecting in said intersatellite link and said uplink signals at least one received signal for transmission as said at least one modulating signal for transmission into said solid angle.

17. A transponder as claimed in claim 11, wherein said transmitter means comprises:

superposing means for superposing said identification codes on a modulating signal to produce M code superposed modulating signals;

modulator means for modulating a carrier signal by said code superposed modulating signal to produce M code superposed and modulated signals, respectively; and

means for transmitting said code superposed and modulated signals as said spot beams, respectively.

18. A transponder as claimed in claim 17, said satellite communication network including a prescribed number of adjacent satellites having a substantially predetermined positional relationship to said orbiting satellite, said transponder covering a solid angle by said spot beams and further comprising receiver means for receiving intersatellite link signals from said adjacent satellites and at least one uplink signal from at least one of said earth stations that is currently present in said solid angle, said receiving means detecting in said intersatellite link and said uplink signals a received signal for transmission as said modulating signal into said solid angle.

19. A burst signal transmitter device of an earth station of a satellite communication network including a predetermined number of orbiting satellites, each satellite radiating M spot beams identified by M identification codes, respectively, where M represents an integer which is equal at least to two, said identification codes being individually specific to said spot beams and for identification and recognition of said spot beams, said burst signal transmitter device transmitting a burst signal to one of said satellites that irradiates said earth station by one of said spot beams, said burst signal transmitter device comprising:

a receiver for receiving said one of said spot beams from said one of said satellites as a received signal at a reception time instant;

a transmitter for transmitting said burst signal to said one of said satellites at a transmission time instant following said reception time instant by an offset amount selected from M offset amounts predetermined for said identification codes, respectively, said offset amount being selected by said earth station in response to said one of said identification codes;

wherein said burst signal transmitter device recognizes said one of said spot beams by one of said identification codes that identifies said received signal.

20. A burst signal transmitter device as claimed in claim 19, wherein:

said receiver comprises a demodulator for demodulating said one of spot beams into a demodulated signal used as said received signal; and

wherein said burst signal transmitter device recognizes, to produce a recognition signal indicative of said one of identification codes, that said demodulated signal is derived from said one of spot beams with said one of identification codes included in said demodulated signal.

21. A burst signal transmitter device as claimed in claim 20, said one of spot beams being modulated by a burst signal carrying data information directed to said earth station, wherein said demodulator further demodulates said demodulated signal into said data information.

22. A burst signal transmitting device as claimed in claim 20, wherein said transmitter comprises:

a memory in which said offset amounts are stored as stored amounts;

a selector responsive to said recognition signal for selecting said offset amount from said stored amount as a selected amount; and

a delay for delaying transmission of said burst signal by said selected amount from said reception time instant.

23. A burst signal transmitter device as claimed in claim 22, wherein said burst signal is supplied to said delay with data information carried thereby.

24. A transponder mounted on an orbiting satellite of a satellite communication network including a plurality of earth stations, wherein said transponder comprises a transmitter for transmitting M spot beams to said earth stations with M identification codes superposed on said spot beams, respectively, where M represents an integer which is equal at least to two, said identification codes being individually specific to said spot beams and for identification and recognition of said spot beams, each said earth station transmitting a burst signal to said transponder with a guard time based on which of said spot beams was transmitted to said earth station, to achieve alignment of said burst signal in time slots on said transponder with burst signals transmitted to said transponder from others of said earth stations.

25. A transponder as claimed in claim 24, wherein said transmitter comprises:

a carrier generator for generating M carrier signals;

a superposing circuit for superposing said identification codes on said carrier signals, respectively, to produce M code superposed signals; and

a spot beam transmitter for transmitting said code superposed signals as said spot beams, respectively.

26. A transponder as claimed in claim 25, wherein said spot beam transmitter time division modulates each of said code superposed signals by at least one modulating signal into a modulated signal for transmission as one of said spot beams.

27. A transponder as claimed in claim 26, said satellite communication network including a prescribed number of adjacent satellites having a substantially predetermined positional relationship to said orbiting satellite, said transponder covering a solid angle by said spot beams and further comprising a receiver for receiving intersatellite link signals from said adjacent satellites and at least one uplink signal from at least one of said earth stations that is currently present in said solid angle, said receiver detecting in said intersatellite link and said uplink signals at least one received signal for use as said at least one modulating signal for transmission into said solid angle.

28. A transponder as claimed in claim 24, wherein said transmitter comprises:

a carrier generator for generating M carrier signals;

a modulator for time division modulating each of said carrier signals by at least one modulating signal to produce M modulated signals from said carrier signals; and

a superposing circuit for superposing said identification codes on said modulated signals, respectively, to produce M code superposed signals for transmission as said spot beams, respectively.

29. A transponder as claimed in claim 28, said satellite communication network including a prescribed number of adjacent satellites having a substantially predetermined positional relationship to said orbiting satellite, said transponder covering a solid angle by said spot beams and further comprising a receiver for receiving intersatellite link signals from said adjacent satellites and at least one uplink signal from at least one of said earth stations that is currently present in said solid angle, said receiver detecting in said intersatellite link and said uplink signals at least one received signal for use as said at least one modulating signal for transmission into said solid angle.

30. A transponder as claimed in claim 24, wherein said transmitter comprises:

a superposing circuit for superposing said identification codes on a modulating signal to produce M code superposed modulating signals;

a modulator for modulating a carrier signal by said code superposed modulating signal to produce M code superposed and modulated signals, respectively, wherein

said transmitter transmits said code superposed and modulated signals as said spot beams, respectively.

31. A transponder as claimed in claim 30, said satellite communication network including a prescribed number of adjacent satellites having a substantially predetermined positional relationship to said orbiting satellite, said transponder covering a solid angle by said spot beams and further comprising a receiver for receiving intersatellite link signals from said adjacent satellites and at least one uplink signal from at least one of said earth stations that is currently present in said solid angle, said receiver detecting in said intersatellite link and said uplink signals a received signal for transmission as said modulating signal into said solid angle.