Satellite uplink power control

• US 7,043,200 B2
• Filed: 06/06/2002
• Issued: 05/09/2006
• Est. Priority Date: 06/06/2001
• Status: Expired due to Fees

• Current Assignee: Telenor Asa (Government of Norway)
• Original Assignee: Telenor Asa (Government of Norway)
• Inventors: Andenæs, Jens
• Primary Examiner(s): Corsaro, Nick
• Assistant Examiner(s): Aminzay, Shaima Q
• Application Number:
  US10/162,888
• Publication Number:
  US 20030008615A1
• Time in Patent Office: 1,433 Days
• Field of Search: 455/13.4, 455/522, 455/69, 455/67.11, 455/430, 455/12.1, 455/427, 455/3.02, 455/67
• US Class Current: 455/13.4
• CPC Class Codes: H04B 7/18517 Transmission equipment in earth stations

Abstract

A method and system for Uplink Power Control in a satellite communication system comprising a geostationary satellite (2) communicating with a gateway station (3) applying the invention and at least two other gateway station (4) is described. The invention utilizes the existing communication signals in the satellite communication system to compensate for atmospheric distortion as scintillation and rain fading effects. The method is symmetric with regard to which gateway that utilizes the invention in a communication system thereby increasing the regulation of all communication signals in the system.

Claims

1. Method for up-link power control in a first gateway earth station (3) in a satellite communication system comprising a geostationary satellite (2), a least two other geographically dispersed earth gateway stations (4) communicating signal carriers (30) via said satellite (2) and a plurality of user stations (5), comprising the steps of:

transmitting a first outbound signal (11) to said satellite from a first gateway (3);

receiving said first outbound signal (11) looped back from said satellite (2) in first said gateway (3) determining the said first outbound signal (11) power level;

wherein;

receiving signal carriers (30) from at least a second gateway station (4) and at least a third gateway station (4) in the same said communication system from said satellite (2) in the first said gateway station (3), determining the signal power level of a signal (30) from said second gateway (4) and the signal power level from a signal (30) from said third gateway (4);

replacing the signal power level of any received signal (30) from said second gateway (4) or from said third gateway (4) in said first gateway (3) with a predefined nominal power value level if one of said signals (30) are below a first predefined threshold value for that said signal power level;

computing a mean value of the signal power level of the outbound signals (30) from said second gateway station (4) and said third gateway station (4) in said first gateway station (3);

computing a first difference between said first signal (11) power level of said first outbound signal (11) from first said gateway (3) and a nominal signal power level of an outbound signal looped back from said satellite (2) to first said gateway (3);

computing a second difference between said mean signal power level of said second signal (30) from said second gateway (4) and said third signal (30) from said third

gateway (4) and a nominal mean power level of a signal from said second gateway (4) and a signal from said third gateway (4);

computing an error signal formed by the difference of the first said difference and the second said difference;

adjusting the power level of said first gateway stations (3) outbound signals an amount based on said error signal within the permissible range of said power level.

2. Method according to claim 1 wherein the step of:

filtering all said received signal levels of signals (30) in said first gateway (3) that are above said first predefined threshold value with a high-pass filter of the form;

TMP_t=K₁*P+(1−

K₁)*TMP_t-1

P′

_t=P−

TMP_t

where TMP_t is a temporary variable at a current time t, K₁ is a coefficient set to be between 0 and 1, P is the current measured power of signal (11,30) the gateway (3) is receiving at time t, TMP_t-1 is the previous sample value of the temporary variable TMP and P′

_t is the desired high-pass filter value of said signal power level (30).

3. Method according to claim 2 wherein the step of:

replacing the output of the said high-pass filter with zero if said received level of signal (30) is below said first threshold value.

4. Method according to claim 1 wherein the step of:

replacing the current received signal power level (30) with a constant nominal value in the averaging process if the received signal power level (30) deviates from the current average signal power level of said second received power level signal (30) and said third power level signal (30) with more than a second predefined threshold value.

5. Method according to claim 1 wherein the step of:

low-pass filtering the mean value of the signal level of said second signal (30) from said second gateway (4) and the signal level of said third signal (30) from the said third gateway (4) with a low-pass filter of the form;

D′

_t=K₂*D+(1−

K₂)*D′

_t-1

if a third difference between said current mean value and the said mean value of one processing step earlier is below a third threshold value; and

where D′

_t is the filter output at the current sample time t;

K₂ is a parameter set to a first value of two different values between 0 and 1 depending on the absolute rate of change of the third difference being above or below the said predefined third threshold value;

D is the prevailing said third difference and D′

_t-1 is the mean value of one processing step earlier.

6. Method according to claim 5 wherein the step of:

replacing said parameter K₂ with a second value between 0 and 1 if said mean value exceeds said third threshold value to enable tracking of scintillations.

7. Method according to claim 1, further comprising the steps of:

computing a fourth difference between an injected reference signal level and said signals nominal value of the signal level; and

computing an error signal formed by the difference between said low-pass filtered signals said third difference and said fourth difference; and

adjusting the power level of said first gateway stations (3) outbound signals an amount based on said error signal within the permissible range of said power level.

8. Device for up-link power control in a first gateway earth station (3) in a satellite communication system comprising a geostationary satellite (2), a least two other geographically dispersed earth gateway stations (4) communicating signal carriers (30) via said satellite (2) and a plurality of user stations (5), comprising:

means for transmitting a first outbound signal (11) to said satellite from a first gateway (3);

means for receiving said first outbound signal (11) looped back from said satellite (2) in first said gateway (3) determining the said first outbound signal (11) power level;

comprising;

means for receiving signal carriers (30) from at least a second gateway station (4) and at least a third gateway station (4) in the same said communication system from said satellite (2) in the first said gateway station (3), determining the signal power level of a signal (30) from said second gateway (4) and the signal power level from a signal (30) from said third gateway (4);

means for replacing the signal power level of any received signal (30) from said second gateway (4) or from said third gateway (4) in said first gateway (3) with a predefined nominal power value level if one of said signals (30) are below a first predefined threshold value for that said signal power level.

means for computing a mean value of the signal power level of the outbound signals (30) from said second gateway station (4) and said third gateway station (4) in said first gateway station (3);

means for computing a first difference between said first signal (11) power level of said first outbound signal (11) from first said gateway (3) and a nominal signal power level of an outbound signal looped back from said satellite (2) to first said gateway (3);

the said nominal value is determined on a day with a clear sky;

means for computing a second difference between said mean signal power level of said second signal (30) from said second gateway (4) and said third signal (30) from said third gateway (4) and a nominal mean power level of a signal from said second gateway (4) and a signal from said third gateway (4);

the nominal value is determined on a day with a clear sky;

means for computing an error signal formed by the difference of the first said difference and the second said difference;

means for adjusting the power level of said first gateway stations (3) outbound signals an amount based on said error signal within the permissible range of said power level.

9. Device according to claim 8 comprising:

means for filtering all said received signal levels of signals (30) in said first gateway (3) that are above said first predefined threshold value with a high-pass filter of the form;

TMP_t=K₁*P+(1−

K₁)*TMP_t-1

P′

_t=P−

TMP_t

where TMP_t is a temporary variable at a current time t, K₁ is a coefficient set to be between 0 and 1, P is the current measured power of signal (11,30) the gateway (3) is receiving at time t, TMP_t-1 is the previous sample value of the temporary variable TMP and P′

_t is the desired high-pass filter value of said signal power level (30).

10. Device according to claim 9 further comprising:

means for replacing the output of the said high-pass filter with zero if said received level of signal (30) is below said first threshold value.

11. Device according to claim 8 comprising:

means for replacing the current received signal power level (30) with a constant nominal value in the averaging process if the received signal power level (30) deviates from the current average signal power level of said second received power level signal (30) and said third power level signal (30) with more than a second predefined threshold value.

12. Device according to claim 8 comprising:

means for low-pass filtering the mean value of the signal level of said second signal (30) from said second gateway (4) and the signal level of said third signal (30) from the said third gateway (4) with a low-pass filter of the form;

D′

_t=K₂*D+(1−

K₂)*D′

_t-1

if a third difference between said current mean value and the said mean value of one processing step earlier is below a third threshold value; and

where D′

_t is the filter output at the current sample time t;

K₂ is a parameter set to a first value of two different values between 0 and 1 depending on the absolute rate of change of the third difference being above or below the said predefined third threshold value;

D is the prevailing said third difference and D′

_t-1 is the mean value of one processing step earlier.

13. Device according to claim 11 further comprising:

means for replacing said parameter K₂ with a second value between 0 and 1 if said mean value exceeds said third threshold value to enable tracking of scintillations.

14. Device according to claim 8, further comprising:

means for computing a fourth difference between an injected reference signal level and said signals nominal value of the signal level; and

means for computing an error signal formed by the difference between said low-pass filtered signals said third difference and said fourth difference; and

means for adjusting the power level of said first gateway stations (3) outbound signals an amount based on said error signal within the permissible range of said power level.

15. Method for up-link power control in a first gateway earth station (3) in a satellite communication system comprising a geostationary satellite (2), a least two other geographically dispersed earth gateway stations (4) communicating signal carriers (30) via said satellite (2) and a plurality of user stations (5), comprising the steps of:

transmitting a first outbound signal (11) to said satellite from a first gateway (3);

receiving said first outbound signal (11) looped back from said satellite (2) in first said gateway (3) determining the said first outbound signal (11) power level;

wherein;

receiving signal carriers (30) from at least a second gateway station (4) and at least a third gateway station (4) in the same said communication system from said satellite (2) in the first said gateway station (3), filtering any received signal in an individual high pass filter of the form of subtracting a low pass filtered version of the signal from the signal itself producing an instantaneous change level signal;

compute an absolute change level signal by subtracting the said instantaneous change level signal from a mean of changes from other signals thereby producing a low pass filtered current variance signal;

compute a weight for each signal by taking the inverse of said variance such that when multiplied by the weight, each signal contributes the same variance;

compute a normalized weight for each said signals such that the sum of said normalized weights equal 1;

compute a downlink estimate by first multiplying said instantaneous change level signal with the associated normalized weight and sum all said products to form an instantaneous downlink estimate;

compute an error signal formed as a difference between said instantaneous downlink estimate and a received beacon signal and a RF reference signal;

adjusting the power level of sa first gateway stations (3) outbound signals an amount based on said error signal within the permissible range of said power level.

16. Device for up-link power control in a first gateway earth station (3) in a satellite communication system comprising a geostationary satellite (2), a least two other geographically dispersed earth gateway stations (4) communicating signal carriers (30) via said satellite (2) and a plurality of user stations (5), comprising:

mans for transmitting a first outbound signal (11) to said satellite from a first gateway (3);

means for receiving said first outbound signal (11) looped back from said satellite (2) in first said gateway (3) determining the said first outbound signal (11) power level;

comprising;

means for receiving signal carriers (30) from at least a second gateway station (4) and at least a third gateway station (4) in the same said communication system from said satellite (2) in the first said gateway station (3), filtering any received signal in an individual high pass filter of the form of subtracting a low pass filtered version of the signal from the signal itself producing an instantaneous change level signal;

means for computing a change level signal by subtracting the said instantaneous change level signal from a mean of changes from other signals thereby producing a low pass filtered current variance signal;

means for computing a weight for each signal by taking the inverse of said variance such that when multiplied by the weight, each signal contribute the same variance;

means for computing a normalized weight for each said signals such that the sum of said normalized weights equal 1;

means for computing a downlink estimate by first multiplying said instantaneous change level signal with the associated normalized weight and sum all said products to form an instantaneous downlink estimate;

means for computing an error signal formed as a difference between said instantaneous downlink estimate and a received beacon signal and a RF reference signal;

means for adjusting the power level of said first gateway stations (3) outbound signals an amount based on said error signal within the permissible range of said power level.