Multi-band/multi-mode satellite radiotelephone communications systems and methods

• US 7,181,161 B2
• Filed: 08/22/2002
• Issued: 02/20/2007
• Est. Priority Date: 09/14/2001
• Status: Expired due to Term

• Current Assignee: ATC Technology Corporation (FedEx Corporation)
• Original Assignee: ATC Technology Corporation (FedEx Corporation)
• Inventors: Karabinis, Peter D.
• Primary Examiner(s): Urban; Edward F.
• Assistant Examiner(s): Dean; Raymond S.
• Application Number:
  US10/225,613
• Publication Number:
  US 20030054762A1
• Time in Patent Office: 1,643 Days
• Field of Search: 455/7, 455 121- 134, 455427-430, 455/436, 455/447, 455/448, 370/316, 370320-321
• 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 7/216 Code division or spread-spectrum multiple access [CDMA, SSMA]

Abstract

Satellite radiotelephone systems and communications methods include a space-based component that is configured to communicate with radiotelephones in a satellite footprint that is divided into satellite cells. The space-based component is configured to communicate with a first radiotelephone in a first satellite cell over a first frequency band and/or a first air interface, and to communicate with a second radiotelephone in the first or a second satellite cell over a second frequency band and/or a second air interface. An ancillary terrestrial network also is provided that is configured to communicate terrestrially with the first radiotelephone over substantially the first frequency band and/or substantially the first air interface, and to communicate terrestrially with the second radiotelephone over substantially the second frequency band and/or substantially the second air interface.

Claims

1. A satellite radiotelephone system comprising:

a space-based component that is configured to communicate with first and second radiotelephones using respective first and second air interfaces;

wherein the first and second radiotelephones are within a geographic area associated with a single cell of the space-based component, the first and second radiotelephones communicate with the space-based component using respective first and second frequencies that are different, at least one of the first and second air interfaces is based upon a terrestrial cellular air interface, and either one or both of forward and reverse feeder links used by the space-based component to communicate with a gateway is/are individually segmented into first and second bands that are used to transport carriers associated respectively with the first and second air interfaces.

3. A satellite radiotelephone system according to claim 1 wherein a circuit-switched mode is provided by a ground-based connection to a public switched telephone network and/or a public data network, and a packet-switched mode is provided by a ground-based connection to a general packet radio service.

4. A satellite radiotelephone system according to claim 1 wherein the terrestrial cellular air interface is a GSM air interface.

5. A satellite radiotelephone system according to claim 1 wherein the terrestrial cellular air interface is a CDMA air interface.

6. A satellite radiotelephone system according to claim 3 wherein the packet-switched mode is based upon GPRS and/or EDGE.

7. A satellite radiotelephone system according to claim 6 wherein the circuit-switched mode is a voice mode and/or data mode.

8. A satellite radiotelephone system according to claim 7 wherein the voice mode uses a vocoder of approximately 4 kbps.

15. A satellite radiotelephone system according to claim 1 wherein the space-based component is further configured to apply first and second channel increments to the respective first and second bands of the forward and/or reverse feeder link;

the first and second channel increments corresponding respectively to first and second sets of carriers associated respectively with the first and second air interfaces.

17. A first radiotelephone that is configured to communicate with the space-based component of claim 1.

18. A second radiotelephone that is configured to communicate with the space-based component of claim 1.

19. A gateway that is configured to communicate with the space-based component of claim 1.

20. A gateway that is configured to communicate with the space-based component of claim 15.

21. A system according to claim 1 wherein a ratio of carrier/channel bandwidth between the first and second air interfaces is greater than 4.

43. A satellite radiotelephone system according to claim 1 wherein the first and/or second bands change with time.

45. A satellite radiotelephone system according to claim 15 wherein the first and/or second channel increments are programmable.

49. A satellite radiotelephone system according to claim 1 wherein the first and second air interfaces differ in a carrier/channel bandwidth, a circuit-switched mode and a packet-switched mode.

50. A satellite radiotelephone system according to claim 49 wherein one of the first and second air interfaces does not include a packet-switched mode and the other one of the first and second air interfaces includes a packet-switched mode.

51. A satellite radiotelephone system according to claim 50 wherein the packet-switched mode provides a forward link data rate that is greater than a return link data rate.

75. A satellite radiotelephone system according to claim 1 wherein both the forward feeder link and the reverse feeder link are individually segmented into first and second bands that are used to transport carriers associated respectively with the first and second air interfaces.

2. A satellite radiotelephone communications method comprising:

communicating between a space-based component and first and second radiotelephones using respective first and second air interfaces;

wherein the first and second radiotelephones are within a geographic area associated with a single cell of the space-based component, the first and second radiotelephones communicate with the space-based component using respective first and second frequencies that are different, and at least one of the first and second air interfaces is based upon a terrestrial cellular air interface; and

communicating between the space-based component and a gateway using forward and reverse feeder links, either one or both of which is/are individually segmented into first and second bands that arc used to transport carriers associated respectively with the first and second air interfaces.

9. A method according to claim 2 wherein a circuit-switched mode is provided by a ground-based connection to a public switched telephone network and/or a public data network, and a packet-switched mode is provided by a ground-based connection to a general packet radio service.

10. A method according to claim 2 wherein the terrestrial cellular air interface is a GSM air interface.

11. A method according to claim 2 wherein the terrestrial cellular air interface is a CDMA air interface.

12. A method according to claim 9 wherein the packet-switched mode is based upon GPRS and/or EDGE.

13. A method according to claim 12 wherein the circuit-switched mode is a voice mode and/or data mode.

14. A method according to claim 13 wherein the voice mode uses a vocoder of approximately 4 kbps.

16. A method according to claim 2 further comprising:

applying first and second channel increments to the respective first and second bands of the forward and/or reverse feeder link;

the first and second channel increments corresponding respectively to first and second sets of carriers associated respectively with the first and second air interfaces.

22. A first radiotelephone that is configured to communicate with the space-based component according to the method of claim 2.

23. A second radiotelephone that is configured to communicate with the space-based component according to the method of claim 2.

24. A gateway that is configured to communicate with the space-based component according to the method of claim 2.

25. A gateway that is configured to communicate with the space-based component according to the method of claim 16.

26. A space-based component that is configured to communicate according to the method of claim 2.

27. A method according to claim 2 wherein a ratio of carrier/channel bandwidth between the first and second air interfaces is greater than 4.

44. A method according to claim 2 wherein the first and/or second bands change with time.

46. A method according to claim 16 wherein the first and/or second channel increments are programmable.

52. A method according to claim 2 wherein the first and second air interfaces differ in a carrier/channel bandwidth, a circuit-switched mode and a packet-switched mode.

53. A method according to claim 52 wherein one of the first and second air interfaces does not include a packet-switched mode and the other one of the first and second air interfaces includes a packet-switched mode.

54. A method according to claim 53 wherein the packet-switched mode provides a forward link data rate that is greater than a return link data rate.

76. A method according to claim 2 wherein communicating between the space-based component and a gateway comprises communicating between the space-based component and a gateway using forward and reverse feeder links, both of which are individually segmented into first and second bands that are used to transport criers associated respectively with the first and second air interfaces.

28. A satellite radiotelephone system comprising:

a space-based component that is configured to communicate with first and second radiotelephones using respective first and second air interfaces;

wherein the space-based component is further configured to communicate with a gateway over forward and reverse feeder links, either one or both of which is/are individually partitioned into first and second bands that are used to transport respective first and second sets of carriers associated respectively with the first and second air interfaces.

29. A satellite radiotelephone system according to claim 28 wherein the first air interface is a GSM air interface.

30. A satellite radiotelephone system according to claim 28 wherein the second air interface is a CDMA air interface.

31. A first radiotelephone that is configured to communicate with the space-based component of claim 28.

32. A second radiotelephone that is configured to communicate with the space-based component of claim 28.

33. A gateway that is configured to communicate with the space-based component of claim 28.

41. A satellite radiotelephone system according to claim 28 wherein the space-based component is further configured to apply first and second channel increments to the respective first and second bands of the forward and/or reverse feeder link;

the first and second channel increments corresponding respectively to first and second sets of carriers associated respectively with the first and second air interfaces.

47. A satellite radiotelephone system according to claim 41 wherein the first and/or second channel increments are programmable.

55. A satellite radiotelephone system according to claim 28 wherein a circuit-switched mode is provided by a ground-based connection to a public switched telephone network and/or a public data network, and a packet-switched mode is provided by a ground-based connection to a general packet radio service.

56. A satellite radiotelephone system according to claim 55 wherein the packet-switched mode is based upon GPRS and/or EDGE.

57. A satellite radiotelephone system according to claim 56 wherein the circuit-switched mode is a voice mode and/or data mode.

58. A gateway that is configured to communicate with the space-based component of claim 41.

59. A system according to claim 28 wherein a ratio of carrier/channel bandwidth between the first and second air interfaces is greater than 4.

67. A satellite radiotelephone system according to claim 28 wherein the first and/or second bands change with time.

69. A satellite radiotelephone system according to claim 28 wherein the first and second air interfaces differ in a carrier/channel bandwidth, a circuit-switched mode and a packet-switched mode.

70. A satellite radiotelephone system according to claim 69 wherein one of the first and second air interfaces does not include a packet-switched mode and the other one of the first and second air interfaces includes a packet-switched mode.

71. A satellite radiotelephone system according to claim 70 wherein the packet-switched mode provides a forward link data rate that is greater than a return link data rate.

77. A satellite radiotelephone system according to claim 28 wherein both the forward feeder link and the reverse feeder link are individually partitioned into first and second bands that are used to transport first and second sets of carriers associated respectively with the first and second air interfaces.

34. A satellite radiotelephone communications method comprising:

communicating between a spaced-based component and first and second radiotelephones using respective first and second air interfaces; and

communicating between the space-based component and a gateway over forward and reverse feeder links, either one or both of which is/are individually partitioned into first and second bands that are used to transport respective first and second sets of carriers associated respectively with the first and second air interfaces.

35. A method according to claim 34 wherein the terrestrial cellular air interface is a GSM air interface.

36. A method according to claim 34 wherein the terrestrial cellular air interface is a CDMA air interface.

37. A first radiotelephone that is configured to communicate with the space-based component according to the method of claim 34.

38. A second radiotelephone that is configured to communicate with the space-based component according to the method of claim 34.

39. A gateway that is configured to communicate with the space-based component according to the method of claim 34.

40. A space-based component that is configured to communicate according to the method of claim 34.

42. A method according to claim 34 further comprising:

applying first and second channel increments to the respective first and second bands of the forward and/or reverse feeder link;

the first and second channel increments corresponding respectively to first and second sets of carriers associated respectively with the first and second air interfaces.

48. A method according to claim 42 wherein the first and/or second channel increments are programmable.

60. A method according to claim 34 wherein a circuit-switched mode is provided by a ground-based connection to a public switched telephone network and/or a public data network, and a packet-switched mode is provided by a ground-based connection to a general packet radio service.

61. A method according to claim 60 wherein the packet-switched mode is based upon GPRS and/or EDGE.

62. A method according to claim 61 wherein the circuit-switched mode is a voice mode and/or data mode.

63. A gateway that is configured to communicate with the space-based component according to the method of claim 42.

64. A space-based component that is configured to communicate according to the method of claim 34.

65. A space-based component that is configured to communicate according to the method of claim 42.

66. A method according to claim 34 wherein a ratio of carrier/channel bandwidth between the first and second air interfaces is greater than 4.

68. A method according to claim 34 wherein the first and/or second bands change with time.

72. A method according to claim 34 wherein the first and second air interfaces differ in a carrier/channel bandwidth, a circuit-switched mode and a packet-switched mode.

73. A method according to claim 72 wherein one of the first and second air interfaces does not include a packet-switched mode and the other one of the first and second air interfaces includes a packet-switched mode.

74. A method according to claim 73 wherein the packet-switched mode provides a forward link data rate that is greater than a return link data rate.

78. A method according to claim 34 wherein communicating between the space-based component and a gateway comprises communicating between the space-based component and a gateway over forward and reverse feeder links, both of which are individually partitioned into first and second bands that are used to transport respective first and second sets of carriers associated respectively with the first and second air interfaces.