Satellite Tracking Method and Apparatus Thereof

• US 20120013506A1
• Filed: 07/12/2011
• Published: 01/19/2012
• Est. Priority Date: 07/13/2010
• Status: Active Grant

• Current Assignee: Gilat Satellite Networks Limited
• Original Assignee: Gilat Satellite Networks Limited
• Inventors: Halavi, Moshe, Peled, Hagay, Berger, Adi
• Granted Patent: US 8,576,120 B2
• Time in Patent Office: Days
• US Class Current: 342/359
• CPC Class Codes: B64G 3/00 Observing or tracking cosmonautic vehicles
• CPC Class Codes: H01Q 1/1257 using the received signal strength
• CPC Class Codes: H01Q 3/06 over a restricted angle

Abstract

A satellite communication ground station configured for communicating over an inclined orbit geostationary satellite may include a tracking antenna having three fixed axis and one moving axis, a motor for swinging the antenna along the moving axis, a controller for controlling the motor, a receiver configured to receive a signal arriving from the satellite via the tracking antenna and an estimator configured to estimate reception quality of a signal received by the receiver. The invention described herein presents a method for tracking an inclined orbit geostationary satellite, the method comprising a learning step and a tracking step, wherein the learning step includes use of a filter for reducing alignment errors and reducing the amount of peaking required for aligning the antenna with the satellite and tracking its movement.

Claims

1. A method for tracking an inclined orbit geostationary satellite at a ground station, the method comprising a learning step and a tracking step, the learning step comprising:

performing multiple instances of a peaking process for a satellite at constant predetermined intervals over a period of a full inclination cycle;

storing results of said peaking process instances, wherein said stored peaking results are motor state values corresponding to antenna positions and to satellite positions along an inclination path;

applying a filter to the stored peaking results for reducing alignment errors; and

replacing the stored peaking results with corresponding values resulting from said filter application.

2. The method of claim 1, wherein the predetermined intervals for performing the peaking process (t) are selected so that a natural number (N) of such intervals exactly fit into an inclination cycle duration (7) using the equation T=N*t.

3. The method of claim 1, wherein performing the peaking process comprises:

commanding a motor at the ground station to change position of a tracking antenna at the ground station over a moving axis of the tracking antenna, in order to find a position of the satellite along the inclination path;

commanding the motor to point the center of a beam of the tracking antenna at the satellite once the position of the satellite is determined; and

storing the peaking process result once the center of the tracking antenna beam is pointed at the satellite.

4. The method of claim 3, wherein storing the peaking process result once the center of the tracking antenna beam is pointed at the satellite comprises:

recording a value corresponding to a state of the motor and to a position of the tracking antenna;

receiving a signal from the satellite and recording a reception quality figure for the received signal; and

recording a time stamp corresponding to the time of recording said motor state and said reception quality figure.

5. The method of claim 1, wherein the tracking step comprises:

calculating a motor state value corresponding to a determined antenna position every predetermined interval;

commanding a motor at the ground station with the calculated motor state value in order to move an antenna at the ground station to the determined antenna position;

receiving a signal from the satellite and obtaining a first reception quality figure for the received signal once the antenna is in the determined position;

comparing said first obtained reception quality figure to a second previously stored reception quality figure corresponding to the determined antenna position; and

performing the peaking process for a current satellite position if the difference between first obtained reception quality figure and the second previously stored reception quality figure exceeds a predefined threshold.

6. The method of claim 5, further comprising:

determining whether the difference between first obtained reception quality figure and the second previously stored reception quality figure exceeds a predefined threshold for a predefined number of consecutive comparisons; and

repeating the learning step based on said determination.

7. The method of claim 5, further comprising:

determining whether the peaking process of the tracking step has not completed successfully for a predetermined number of consecutive attempts; and

repeating the learning step based on said determination.

8. The method of claim 5, wherein the predetermined intervals for calculating the motor state value in the tracking step are the same as the constant predetermined intervals for performing the peaking process in the learning step.

9. The method of claim 1, wherein said peaking process comprises a process for aligning an antenna with a satellite, the peaking process comprising:

recording an initial motor state value for a motor at the ground station, the initial motor state value corresponding to an initial antenna position;

receiving a signal from the satellite and recording a reception quality figure for the received signal; and

driving the antenna exactly one step from the initial antenna position by commanding the motor with a state value one unit either higher or lower than the initial motor state value;

determining whether the new value commanded to the motor is higher or lower than the initial motor state value; and

based on said determination, determining a starting direction for said peaking process.

10. The method of claim 1, wherein said peaking process comprises a process for aligning an antenna with a satellite, the peaking process comprising:

recording an initial motor state value for a motor at the ground station and an initial reception quality figure of a signal received from the satellite, both corresponding to an initial antenna position;

driving the antenna to positions within a scanning range around the initial position, first to one direction and then to the opposite direction, wherein at each step in the same direction the antenna is driven exactly one step away from its previous position;

recording for each scanned position a calculated average value of multiple reception quality figures obtained in said position and a motor state value corresponding to said position;

determining that two recorded average reception quality values, one per scanned direction, are lower than the initial reception quality figure by at least a predefined tolerance;

identifying two recorded average reception quality values one per scanned direction, wherein said identified values are the lowest recorded average reception quality values with a difference between them which is lower than a predefined tolerance;

determining two motor state value corresponding to said identified reception quality values;

calculating a motor state value corresponding to an antenna position, which aligns the center of an antenna beam with the satellite, as a middle motor state value between said determined two motor state values; and

commanding the motor with said calculated middle motor state value;

11. The method of claim 10, wherein one or more resulting alignment errors are thereafter removed by applying a filter on the peaking process results.

12. A ground station configured to communicate via an inclined orbit geostationary satellite, the ground station comprising:

a tracking antenna having three fixed axis and one moving axis;

a motor configured to swing the antenna along the moving axis;

a controller configured to control the motor;

a receiver configured to receive a signal from a satellite via the tracking antenna; and

an estimator configured to estimate reception quality of a signal received by the receiver,

wherein the controller is further configured to track the satellite by performing a learning step and a tracking step, said learning step comprising;

performing multiple instances of a peaking process for the satellite at constant predetermined intervals over a period of a full inclination cycle;

storing results of said peaking process instances, wherein said stored peaking results are motor state values corresponding to antenna positions and to satellite positions along an inclination path;

applying a filter to the stored peaking results for reducing alignment errors; and

replacing the stored peaking results with corresponding values resulting from said filter application.

13. The ground station of claim 12, wherein the controller is configured to select the interval for performing the peaking process (t) so that a natural number (N) of such intervals exactly fit into an inclination cycle duration (7), using the equation T=N*t.

14. The ground station of claim 12, wherein for performing the peaking process the controller is configured to:

command the motor to change the position of the tracking antenna over the moving axis in order to find a position of the satellite along the inclination path;

command the motor to point the center of a beam of the tracking antenna at the satellite once the position of the satellite is determined; and

store the peaking process result once the center of the tracking antenna beam is pointed at the satellite.

15. The ground station of claim 14, wherein once the center of the beam of the tracking antenna is pointed at the satellite, the controller is further configured to:

record a value corresponding to a state of the motor and to a position of the tracking antenna;

receive a signal from the satellite and record a reception quality figure from the estimator for the signal received from the satellite; and

record a time stamp corresponding to the time of recording said motor state and said reception quality figure.

16. The ground station of claim 12, wherein the tracking step comprises:

calculating a motor state value corresponding to a determined antenna position every predetermined interval;

commanding the motor with the calculated state value in order to move the tracking antenna to the determined antenna position;

receiving a signal from the satellite and obtaining a first reception quality figure for the received signal once the tracking antenna is in the determined position;

comparing said first obtained reception quality figure to a second previously stored reception quality figure corresponding to the determined antenna position; and

performing the peaking process for a current satellite position if the difference between first obtained reception quality figure and the second previously stored reception quality figure exceeds a predefined threshold.

17. The ground station of claim 16, wherein the controller is further configured to:

determine whether the difference between first obtained reception quality figure and the second previously stored reception quality figure exceeds a predefined threshold for a predefined number of consecutive comparisons; and

repeat the learning step based on said determination.

18. The ground station of claim 16, wherein the controller is further configured to:

determine whether the peaking process of the tracking step has not completed successfully for a predetermined number of consecutive attempts; and

repeat the learning step based on said determination.

19. The ground station of claim 16, wherein the controller is configured to select the predetermined interval for calculating the motor state value in the tracking step to be the same as the constant predetermined intervals for performing the peaking process in the learning step.

20. The ground station of claim 12, wherein said peaking process comprises a process for aligning an antenna with a satellite, the peaking process comprising:

recording an initial motor state value for a motor at the ground station, the initial motor state value corresponding to an initial antenna position;

receiving a signal from the satellite and recording a reception quality figure for the received signal; and

driving the antenna exactly one step from the initial antenna position by commanding the motor with a state value one unit either higher or lower than the initial motor state value;

determining whether the new value commanded to the motor is higher or lower than the initial motor state value; and

based on said determination, determining a starting direction for said peaking process.

21. The ground station of claim 12, wherein said peaking process comprises a process for aligning an antenna with a satellite, the peaking process comprising:

recording an initial motor state value for a motor at the ground station and an initial reception quality figure of a signal received from the satellite, both corresponding to an initial antenna position;

driving the antenna to positions within a scanning range around the initial position, first to one direction and then to the opposite direction, wherein at each step in the same direction the antenna is driven exactly one step away from its previous position;

recording for each scanned position a calculated average value of multiple reception quality figures obtained in said position and a motor state value corresponding to said position;

determining that two recorded average reception quality values, one per scanned direction, are lower than the initial reception quality figure by at least a predefined tolerance;

identifying two recorded average reception quality values one per scanned direction, wherein said identified values are the lowest recorded average reception quality values with a difference between them which is lower than a predefined tolerance;

determining two motor state value corresponding to said identified reception quality values;

calculating a motor state value corresponding to an antenna position, which aligns the center of an antenna beam with the satellite, as a middle motor state value between said determined two motor state values; and

commanding the motor with said calculated middle motor state value;

22. The ground station of claim 21, wherein one or more resulting alignment errors are thereafter removed by applying a filter on the peaking process results.

23. A method for tracking an inclined orbit geostationary satellite at a ground station, the method comprising a peaking process for aligning an antenna with a satellite, the method comprising:

recording an initial motor state value for a motor at the ground station, the initial motor state value corresponding to an initial antenna position;

receiving a signal from the satellite and recording a reception quality figure for the received signal; and

driving the antenna exactly one step from the initial antenna position by commanding the motor with a state value one unit either higher or lower than the initial motor state value;

determining whether the new value commanded to the motor is higher or lower than the initial motor state value; and

based on said determination, determining a starting direction for said peaking process.

24. The method of claim 23, further comprising performing the following steps for a new antenna position within a peaking scanning range:

obtaining multiple reception quality figures over a predefined time interval;

calculating an average value of the obtained multiple reception quality figures after the predefined time interval expires;

recording the calculated average value of the obtained multiple reception quality figures and a corresponding motor state value;

determining whether the calculated average value of the obtained multiple reception quality figures is lower than an initial reception quality figure by at least a predefined tolerance; and

driving the motor exactly one step from its current position in accordance with the starting direction if the calculated average value of the obtained multiple reception quality figures is not lower than said initial reception quality figure by at least the predefined tolerance.

25. The method of claim 24, further comprising:

determining whether the calculated average value of the obtained multiple reception quality figures is lower than the initial reception quality figure by at least the predefined tolerance;

if the calculated average value of the obtained multiple reception quality figures is lower than the initial reception quality figure by at least the predefined tolerance, driving the antenna to the initial antenna position by commanding the motor with the initial motor state value;

after driving the antenna to the initial antenna position, scanning a plurality of motor steps one at a time in a direction opposite to the starting direction;

recording a calculated average reception quality figure and a corresponding motor state value for each of the plurality of motor steps scanned;

determining after scanning each of the plurality of motor steps whether the calculated average reception quality figure is lower than said initial reception quality figure by at least the predefined tolerance; and

terminating the scanning if the calculated average reception quality figure is lower than said initial reception quality figure by at least the predefined tolerance.

26. The method of claim 25, further comprising the following steps upon terminating the scanning process:

identifying within the calculated average reception quality figures a first reception quality figure recorded during scanning in the starting direction and a second reception quality figure recorded during scanning in the direction opposite to the starting direction, wherein said first and second reception quality figures are the lowest calculated average reception quality figures with a difference between them, which is lower than a predefined tolerance;

determining a first motor state value corresponding to said first reception quality figure;

determining a second motor state value corresponding to said second reception quality figure;

calculating a motor state value corresponding to an antenna position which aligns the center of an antenna beam with the satellite as a middle motor state value between said first and second motor state values; and

commanding the motor with said calculated middle motor state value.

27. The method of claim 23, wherein one or more resulting alignment errors are thereafter removed by applying a filter on the peaking process results.