Satellite up-link fade control

• US 6,947,741 B2
• Filed: 04/24/2002
• Issued: 09/20/2005
• Est. Priority Date: 04/27/2001
• Status: Expired due to Fees

• Current Assignee: Ericsson AB (Telefonaktiebolaget LM Ericsson)
• Original Assignee: Tandberg Telecom AS (Cisco Systems, Inc.)
• Inventors: Beech, Brian Herbert, Edwards, David G.
• Primary Examiner(s): Trinh, Sonny
• Assistant Examiner(s): DOAN, PHUOC HUU
• Application Number:
  US10/131,696
• Publication Number:
  US 20020160795A1
• Time in Patent Office: 1,245 Days
• Field of Search: 455/430, 455/13.4, 455/63.1, 455 69- 70, 455/12.1, 455/427, 455/505, 455/501, 375/298, 375/278, 375/296, 375/297
• US Class Current: 455/430
• CPC Class Codes: H04B 7/18517 Transmission equipment in earth stations
• CPC Class Codes: H04L 27/367 using predistortion

Abstract

A method up-link fade control for a satellite not having AGC, includes the steps of determining characteristics for correcting channel non-linearity, each characteristic being determined for a different value of up-link fade. A signal representative of up-link fade is determined by a beacon receiver and the signal is associated with a correction characteristic for the up-link fade. The correction characteristic associated with the signal is applied to a corrector of a modulator such that the corrector changes the modulator characteristics to modify constellation parameters at a satellite receiver.

Claims

1. A method of providing up-link fade control to a satellite not having AGC, said up-link having a modulator in a transmitting station, including the steps of:

(a) determining plural characteristics for correcting channel non-linearity, each characteristic being determined for a different value of up-link fade,

(b) determining a signal representative of up-link fade by beacon receiver means,

(c) associating said signal with a correction characteristic for said up-link fade,

(d) applying said correction characteristic associated with said sign to corrector means of said modulator, wherein said corrector means changes the modulator characteristics to modify constellation parameters at a satellite receiver.

2. A method as claimed in claim 1 wherein said step (a) of determining plural characteristics includes the steps of detecting the received constellation parameters with the satellite operating at substantially saturation level, calculating correction parameters for various values of satellite input back-off corresponding to values of up-link fade and storing said characteristics.

3. A method as claimed in claim 1 wherein said plural characteristics are stored in store means at said transmitting station.

4. A method as claimed in claim 1 wherein said plural characteristics are stored at a receiving station which includes a satellite receiver demodulator coupled with display means for displaying the receiver constellation characteristics, and processor means for storing said plural characteristics and to select one of said characteristics for correcting said receiver constellation in dependence upon up-link fade, said processor means being coupled with said transmitter modulator to apply correction to the modulator to correct the received constellation parameters.

5. A method as claimed in claim 2 wherein the increments of satellite back-off are non-linear.

6. A method as claimed in claim 2 wherein the increments of satellite back-off are linear.

7. A method as claimed in claim 4 wherein the processor means is connected to said modulator by a digital communication channel.

8. A method as claimed in claim 1 wherein the signal representative of up-link fade is determined by beacon receiver means which is polled such that, as the up-link fades, so a revised characteristics is used to modify the modulator so that the constellation parameters at the receiver are maintained substantially undistorted.

9. A method as claimed in claim 1 wherein the corrector means performs dynamic pre-correction by pre-distorting a signal which has been modulated to carry signals representative of digital data so as to reduce non-linear distortion in a signal channel containing root Nyquist bandpass filters in transmission and reception portions of said channel, there being provided a series connection of a static pre-distortion section configured to represent an inverse function of magnitude and phase distortion estimated to occur in said channel, and at least one dynamic pre-distortion section, the or each dynamic pre-distorting section including a forward model configured to represent magnitude and phase distortion in said channel, said signal being passed through cascaded sections whereby each successive dynamic pre-distorting section receives input from an output of a preceding dynamic pre-distorting section so that distortion in said channel is successively reduced to zero with each successive dynamic pre distorting section.

10. A method as claimed claim 9 wherein said channel includes a satellite having a cascaded input multiplexer filter, a power amplifier and an output multiplexer filter, and said forward model further comprises a model of magnitude responds of said input multiplexer filter and output multiplexer filter, whereby magnitude response of said channel may be corrected.

11. A method as claimed in claim 9 wherein said dynamic pre-distorting sections are substantially identical to one another.

12. A method as claimed in claim 9 wherein said forward model comprises a series connection of an up-sampler, a model representative of magnitude and phase of:

a transmission side root Nyquist filter;

a transmission side high power amplifier;

a satellite input multiplexer filter;

a satellite power amplifier;

a satellite output multiplexer filter;

a receiver side root Nyquist filter;

and a down-sampler.

13. A method as claimed in claim 10 wherein said power amplifier is one a travelling wave and a solid state power amplifier.

14. A method as claimed in claim 9 wherein said signal is modulated in accordance with one of 16 QAM, 32 QAM, 8 PSK and 16 PSK.

15. A method of providing up-link fade control to a satellite not having AGC, said up-link having a modulator in a transmitting station, including the steps of determining plural characteristics for correcting channel non-linearity, each characteristic being determined for a different value of up-link fade, determining a signal representative of up-link fade by beacon receiver means, associating said signal with a correction characteristic for said up-link fade, applying said correction characteristic associated with said signal to corrector means of said modulator, wherein said corrector means changes the modulator characteristics to modify constellation parameters at a satellite receiver, and said corrector means performs dynamic pre-correction by pre-distorting a signal which has been modulated to carry signals representative of digital data so as to reduce non-linear distortion in a signal channel containing root Nyquist bandpass filters in transmission and reception portions of said channel, there being provided a series connection of a static pre-distortion section configured to represent an inverse function of magnitude and phase distortion estimated to occur in said channel, and at least one dynamic pre-distortion section, the or each dynamic pre-distorting section including a forward model configured to represent magnitude and phase distortion in said channel, said signal being passed through cascaded sections whereby each successive dynamic pre-distorting section receives input from an output of a preceding dynamic pre-distorting section so that distortion in said channel is successively reduced to zero with each successive dynamic pre-distorting section.

16. A system for providing up-link fade control to a satellite not having AGC, said system including a modulator in a transmitting station of said up-link, means for determining plural characteristics for correcting channel non-linearity, each characteristic being determined for a different value of up-link fade, means for determining signal representative of up-link fade by beacon receiver means, means for associating said signal with a correction characteristic for said up-link fade, and means for applying said correction characteristic associated with said signal to corrector means of said modulator, wherein said corrector means changes the modulator characteristics to modify constellation parameters at a satellite receiver.

17. A system as claimed in claim 16 wherein said means for determining plural characteristics includes means for detecting the received constellation parameters with the satellite operating at substantially saturation level, and means for calculating correction parameters for various values of satellite input back-off corresponding to values of up-link fade and storing said characteristics.

18. A system as claimed in claim 16 wherein said plural characteristics are stored in store means at said transmitting station.

19. A system as claimed in claim 16 wherein said plural characteristics are stored at a receiving station which includes a satellite receiver demodulator coupled with display means for displaying the receiver constellation characteristics, and processor means for storing said plural characteristics and to select one of said characteristics for correcting said receiver constellation in dependence upon up-link fade, said processor means being coupled with said transmitter modulator to apply correction to the modulator to correct the received constellation parameters.

20. A system as claimed in claim 17 wherein the increments of satellite back-off are non-linear.

21. A method as claimed in claim 17 wherein the increments of satellite back-off are linear.

22. A method as claimed in claim 19 wherein the processor means is connected to said modulator by a digital communication channel.

23. A system as claimed in claim 16 wherein the signal representative of up-link fade is determined by beacon receiver means which is polled such that, as the up-link fades, so a revised characteristics is used to modify the modulator so that the constellation parameters at the receiver are maintained substantially undistorted.

24. A system as claimed in claim 16 wherein the corrector means performs dynamic pre-correction by pre-distorting a signal which has been modulated to carry signals representative of digital data so as to reduce non-linear distortion in a signal channel containing root Nyquist bandpass filters in transmission and reception portions of said channel, there being provided a series connection of a static pre-distortion section configured to represent an inverse function of magnitude and phase distortion estimated to occur in said channel, and at least one dynamic pre-distortion section, the or each dynamic pre-distorting section including a forward model configured to represent magnitude and phase distortion in said channel, said signal being passed through cascaded sections whereby each successive dynamic pre-distorting section receives input from an output of a preceding dynamic pre-distorting section so hat distortion in said channel is successively reduced to zero with each successive dynamic pre-distorting section.

25. A system as claimed claim 16 wherein said channel includes a satellite having a cascaded input multiplexer filter, a power amplifier and an output multiplexer filter, and said forward model further comprises a model of magnitude response of said input multiplexer filter and output multiplexer filter, whereby magnitude response of said channel may be corrected.

26. A system as claimed in claim 24 wherein said dynamic pre-distorting sections are substantially identical to one another.

27. A system as claimed in claim 24 wherein said forward model comprises a series connection of an up-sampler, a model representative of magnitude and phase of:

a transmission side root Nyquist filter;

a transmission side high power amplifier;

a satellite input multiplexer filter;

a satellite power amplifier;

a satellite output multiplexer filter;

a receiver side root Nyquist filter;

and a down-sampler.

28. A system as claimed in claim 25 wherein said power amplifier is one of a travelling wave and a solid state power amplifier.

29. A system as claimed in claim 24 wherein said signal is modulated in accordance with one of 16 QAM, 32 QAM, 8 PSK and 16 PSK.

30. A system for providing up-link fade control to a satellite not having AGC, said system including a modulator in a transmitting station of said up-link, means for determining plural characteristics for correcting channel non-linearity, each characteristic being determined for a different value of up-link fade, means for determining a signal representative of up-link fade by beacon receiver means, means for associating said signal with a correction characteristic for said up-link fade, means for applying said correction characteristic associated with said signal to corrector means of said modulator, wherein said corrector means changes the modulator characteristics to modify constellation parameters at a satellite receiver, and said corrector means performs dynamic pre-correction by pre-distorting a signal which has been modulated to carry signals representative of digital data so as to reduce non-linear distortion in a signal channel containing root Nyquist bandpass filters in transmission and reception portions of said channel, there being provided a series connection of static pre-distortion section configured to represent an inverse function of magnitude and phase distortion estimated to occur in said channel, and at least one dynamic pre-distortion section, the or each dynamic pre-distorting section including a forward model configured to represent magnitude and phase distortion in said channel, said signal being passed through cascaded sections whereby each successive dynamic pre-distorting section receives input from an output of a preceding dynamic pre-distorting section so that distortion in said channel is successively reduced to zero with each successive dynamic pre-distorting section.

31. A method of providing up-link fade control to a satellite not having AGC, said up-link having a modulator in a transmitting station, including the steps of:

(a) determining plural characteristics for correcting channel non-linearity, each characteristic being determined for a different value of up-link fade,

(b) determining a signal representative of up-link fade by beacon receiver means,

(c) associating said signal with a correction characteristic for said up-link fade,

(d) applying said correction characteristic associated with said sign to corrector means of said modulator, wherein the beacon receiver means is polled such that, as the up-link fades, so a revised correction characteristic is used to modify the modulator so that the constellation parameters at a satellite receiver are maintained substantially undistorted.

32. A system for providing up-link fade control to a satellite not having AGO, said system including a modulator in a transmitting station of said up-link, means for determining plural characteristics for correcting channel non-linearity, each characteristic being determined for a different value of up-link fade, means for determining a signal of up-link fade by beacon receiver means, means for association said signal with a correction characteristic for said up-link fade, and means for applying said correction characteristic associated with said signal to corrector means of said modulator, wherein the signal representative of up-link fade is determined by beacon receiver means which is polled such that, as the up-link fades, so a revised characteristic is used to modify the modulator so that the constellation parameters at the receiver are maintained substantially undistorted.

33. A method of compensating up-link fade in a system having a modulator in a transmitting station, an up-link to a satellite having a transponder not having a AGC, and a down-link from a beacon of the satellite to a receiving station having a beacon receiver, the method including the steps of:

determining a plurality of characteristics representative of up-link fade values indicated by a signal transmitted from the beacon transmitter of the satellite to the receiving station beacon receiver;

storing said plurality of characteristics to provide correction parameters for said modulator;

determining an up-link fade value by said beacon receiver and in dependence thereon selecting a stored characteristic, and

applying the selected characteristic to a corrector means of said modulator, wherein the modulation of a transmitted signal from the transmitting station is pre-corrected such that the signal received by the receiving station has a constellation pattern that is substantially undistorted by channel non-linearities and up-link fading.

34. A method as claimed in claim 33 wherein said step of determining the plurality of characteristics includes the steps of transmitting a modulated signal from the satellite transponder when it is operating at its saturation point, detecting a constellation pattern of the modulated signal received at the receiving station, determining and storing the modulator correction parameters required to obtain a “

corners at saturation”

constellation pattern for he received signal, and repeating process for various values of satellite transponder input back-off, which values correspond to values of up-link fade.

35. A method as claimed in claim 33 wherein said characteristics are stored in store means coupled to the modulator at said transmitting station.

36. A method as claimed in claim 33 wherein said characteristics are stored at a receiving station which includes a satellite receiver demodulator coupled with display means for displaying the receiver constellation characteristics, and processor means for storing said plurality of characteristics and to select one of said characteristics for correcting said receiver constellation in dependence upon up-link fade, said processor means being coupled with said transmitter modulator to apply the pre-correction to the modulator to correct the received constellation parameters.

37. A method as claimed in claim 34 wherein the increments of satellite back-off are non-linear.

38. A method as claimed in claim 34 wherein the increments of satellite back-off are linear.

39. A method as claimed in claim 36 wherein the processor means is connected to said modulator by a digital communication channel.

40. A method as claimed in claim 33 wherein the beacon receiver means is polled such that, as the up-link fades, so a revised characteristic is selected to apply to the corrector means of the modulator so that the constellation parameters at the receiver are maintained substantially undistorted.

41. A method as claimed in claim 33 wherein the corrector means performs dynamic pre-correction by pre-distorting a signal which has been modulated to carry signals representative of digital data so as to reduce non-linear distortion in a signal channel containing root Nyquist bandpass filters in transmission and reception portions of said channel, there being provided a series connection of a static pre-distortion section configured to represent an inverse function of magnitude and phase distortion estimated to occur in said channel, and at least one dynamic pre-distortion section, the or each dynamic pre-distorting section including a forward model configured to represent magnitude and phase distortion in said channel, said signal being passed through cascaded sections whereby each successive dynamic pre-distorting section receives input from an output of a preceding dynamic pre-distorting section so that distortion in said channel is successively reduced to zero with each successive dynamic pre-distorting section.

42. A method as claimed in claim 41 wherein the satellite has a cascaded input multiplexer filter, a power amplifier and an output multiplexer filter, and said forward model comprises a model of magnitude response of said input multiplexer filter and output multiplexer filter, whereby magnitude response of said system may be corrected.

43. A method as claimed in claim 41 wherein said dynamic pre-distorting sections are substantially identical to one another.

44. A method as claimed in claim 41 wherein said forward model comprises a series connection of an up-sampler, a model representative of magnitude and phase of:

a transmission side root Nyquist filter;

a transmission side high power amplifier;

a satellite input multiplexer filter;

a satellite power amplifier;

a satellite output multiplexer filter;

a receiver side root Nyquist filter;

and a down-sampler.

45. A method as claimed in claim 42 wherein said power amplifier is one of a travelling wave and a solid state power amplifier.

46. A method as claimed in claim 33 wherein said signal is modulated in accordance with one of 16 QAM, 32 QAM, 8 PSK and 16 PSK.

47. A method as claimed in claim 33 wherein the received constellation pattern is displayed by a display means.

48. A satellite communication system to compensate up-link fade, said system including:

a modulator in a transmitting station,

an up-link to a satellite having a transponder not having a AGC,

a down-link from a beacon of the satellite to a receiving station having beacon receiver,

determining means to provide a plurality of characteristics representative of up-link fade values indicated by a signal transmitted from the beacon transmitter of the satellite to the receiving station beacon receiver,

storing means to store said plurality of characteristics to provide correction parameters for said modulator,

wherein said beacon receiver determines an up-link fade value and in dependence thereon selects a stored characteristic, and applies the selected characteristic to a corrector means of said modulator, and the modulation of a transmitted signal from the transmitting station is pre-corrected such that the signal received by the receiving station has a constellation pattern that is substantially undistorted by channel non-linearities and up-link fading.

49. A system as claimed in claim 48 wherein said determining means is to transmit a modulated signal from the satellite transponder when it is operating at its saturation point, detect a constellation pattern of the modulated signal received at the receiving station, determine and store the modulator correction parameters required to obtain a “

corners at saturation”

constellation pattern for the received signal, and repeat for various values of satellite transponder input back-off, which values correspond to values of up-link fade.

50. A system as claimed in claim 48 wherein said store means are coupled to the modulator at said transmitting station.

51. A method as claimed in claim 48 wherein said store means are at the receiving station which includes a satellite receiver demodulator coupled with display means for displaying the receiver constellation characteristics, and processor means for storing said plurality of characteristics and to select one of said characteristics for correcting said receiver constellation in dependence upon up-link fade, said processor means being coupled with said transmitter modulator to apply the pre-correction to the modulator to correct the received constellation parameters.

52. A system as claimed in claim 49 wherein the increments of satellite back-off are non-linear.

53. A method as claimed in claim 49 wherein the increments of satellite back-off are linear.

54. A system as claimed in claim 51 wherein the processor means is connected to said modulator by a digital communication channel.

55. A system as claimed in claim 48 wherein the beacon receiver means is polled such that, as the up-link fades, a revised characteristic is selected to be applied to the corrector means of the modulator so that the constellation parameters at the receiver are maintained substantially undistorted.

56. A system as claimed in claim 48 wherein the corrector means is to perform dynamic pre-correction by pre-distorting a signal which has been modulated to carry signals representative of digital data so as to reduce non-linear distortion in a signal channel containing root Nyquist bandpass filters in transmission and reception portions of said channel, there being provided a series connection of a static pre-distortion section configured to represent an inverse function of magnitude and phase distortion estimated to occur in said channel, and at least one dynamic pre-distortion section, the or each dynamic pre-distorting section including a forward model configured to represent magnitude and phase distortion in said channel, said signal being passed through cascaded sections whereby each successive dynamic pre-distorting section receives input from an output of a preceding dynamic pre-distorting section so that distortion in said channel is successively reduced to zero with each successive dynamic pre-distorting section.

57. A system as claimed in claim 56 wherein the satellite has a cascaded input multiplexer filter, a power amplifier and an output multiplexer filter, and said forward model comprises a model of magnitude response of said input multiplexer filter and output multiplexer filter, whereby magnitude response of said system may be corrected.

58. A system as claimed in claim 56 wherein said dynamic pre-distorting sections are substantially identical to one another.

59. A system as claimed in claim 56 wherein said forward model comprises a series connection of an up-sampler, a model representative of magnitude and phase of:

a transmission side root Nyquist filter;

a transmission side high power amplifier;

a satellite input multiplexer filter;

a satellite power amplifier;

a satellite output multiplexer filter,

a receiver side root Nyquist filter,

and a down-sampler.

60. A system as claimed in claim 57 wherein said power amplifier is one of a travelling wave and a solid state power amplifier.

61. A system as claimed in claim 48 wherein said signal is modulate in accordance with one of 16 QAM, 32 QAM, 8 PSK and 16 PSK.

62. A system as claimed in claim 48 wherein the received constellation pattern is displayed by a display means.