Antenna system for satellite lock-on and method for operating the same

• US 8,290,424 B2
• Filed: 03/11/2009
• Issued: 10/16/2012
• Est. Priority Date: 06/30/2008
• Status: Expired due to Fees

• Current Assignee: Azure Shine International, Inc.
• Original Assignee: Azure Shine International, Inc.
• Inventors: Shen, Wen-Chao, Shen, Wen-Yen, Chen, Shun-Ching
• Primary Examiner(s): LE, DINH THANH
• Application Number:
  US12/401,884
• Publication Number:
  US 20090328110A1
• Time in Patent Office: 1,315 Days
• Field of Search: 34099512-99515, 340/995, 455/3.02, 455/130, 701207-209, 342/359, 342/75
• US Class Current: 455/3.02
• CPC Class Codes: H01Q 1/1257 using the received signal strength
• CPC Class Codes: H01Q 21/28 Combinations of substantially independent non-interacting antenna units or systems multiple beam H01Q25/00

Abstract

An antenna system and a corresponding method for satellite lock-on applied to vehicles automatically lock on at least one satellite in the space by means of a lock-on signal. The technique features on a scan driving signal that initiates a space scan of the antenna system so as to obtain a scan data. According to peak values of the scan data, coordinates of a plurality of satellites in the space are realized and individually recorded. Then, after receiving a lock-on signal, the satellite coordinate of the satellite to be locked is retrieved so as to drive the antenna to point at the satellite to be locked.

Claims

1. A satellite signal control box, coupled with at least one antenna unit mounted on a vehicle through a driving system to drive the antenna unit to point at at least one of a plurality of satellites in the space, comprising:

an operational interface unit generating a scan driving signal representative of a scan pattern and scan coordinates,

a processor unit coupled to said operational interface unit to receive said scan driving signal therefrom and generating an activating signal responsive thereto,

a driving control circuit coupled to said processor unit to receive said activating signal therefrom, said driving control unit being coupled to a driving unit, said driving control unit activating said driving unit to trigger an antenna unit to perform scan in the space in accordance with said scan pattern and scan coordinates,

said antenna unit, simultaneously with said space scanning, capturing satellite signals from at least one of a plurality of satellites in the scanned space upon meeting said scan coordinates, said satellite signals including scan data, wherein said scan data includes peak values of the satellite signals strength.

said processing unit being further coupled to said driving control circuit for analyzing the scan data to obtain satellite coordinates of said at least one satellite based on said peak values of said satellite signals strength in correspondence to said scan coordinates; and

a memory unit coupled to said processing unit for storing the satellite coordinates of said at least one satellite;

wherein said operational interface unit elects a target satellite to be locked on among said plurality thereof, and sends a lock-on signal to said processing unit,

wherein, upon receiving said lock-on signal from said operational interface unit, the processing unit captures the satellite coordinates of said target satellite to be locked according to the lock-on signal;

wherein, upon capturing said satellite coordinate of said target satellite from said memory unit, the processing unit sends an antenna control signal to the driving control circuit according to said satellite coordinates being captured, and the driving control circuit triggers the driving unit to point the antenna unit at the target satellite.

2. The satellite signal control box according to claim 1, wherein said antenna unit includes a digital video broadcasting-satellite (DVB-S) antenna.

3. The satellite signal control box according to claim 2, wherein said antenna unit is a dish antenna.

4. The satellite signal control box according to claim 2, wherein said antenna unit is a flat antenna.

5. The satellite signal control box according to claim 1, wherein said antenna unit has at least one DVB-S antenna and at least one digital video broadcasting-terrestrial (DVB-T)antenna.

6. The satellite signal control box according to claim 1, further including a digital video broadcasting-satellite/terrestrial (DVB-S/T) receiver coupled with said processing unit and said antenna unit.

7. The satellite signal control box according to claim 6, further including a DVB-T transmitter coupled with said DVB-S/T receiver for transmitting at least one DVB-T video signal to at least one digital television.

8. The satellite signal control box according to claim 6, further including an encoder coupled with said processing unit, said DVB-S/T receiver and said antenna unit.

9. The satellite signal control box according to claim 6, further including;

a control signal amplifier coupled with said processing unit for amplifying a control signal generated by said processing unit; and

a control signal driving circuit coupled with the control signal amplifier, said DVB-S/T receiver and said antenna unit for controlling said DVB-S/T receiver according to the control signal.

10. The satellite signal control box according to claim 1, wherein said processing unit further couples to a global positioning system (GPS), a GPS antenna being coupled to said GPS for obtaining a satellite position coordinate of said vehicle, said antenna control signal being sent according to the satellite position coordinate of said vehicle and said at least one satellite coordinate.

11. The satellite signal control box according to claim 1, wherein said processing unit further couples to a vehicle position-sensing unit for obtaining a vehicle position of said vehicle, said antenna control signal being sent according to the vehicle position and said at least one satellite coordinate.

12. The satellite signal control box according to claim 11, wherein said vehicle position further includes an azimuth angle of said vehicle and an elevation angle of said vehicle, and wherein said vehicle position-sensing unit further includes:

a gyroscope for determining the azimuth angle; and

a gravity-sensing element for determining the elevation angle.

13. The satellite signal control box according to claim 1, wherein said memory unit further includes:

a satellite coordinate memory area for storing said at least one satellite coordinates; and

a vehicle coordinate memory area for storing a vehicle coordinate and a vehicle position of said vehicle.

14. The satellite signal control box according to claim 1, wherein said driving unit is a step motor.

15. An antenna system, mounted on a vehicle for automatically locking on at least one of a plurality of satellites in the space according to a lock-on signal, comprising:

an operational interface generating a scan drive signal representative of a scan pattern and scan coordinates;

an antenna device;

a driving system coupled with the antenna unit;

a driving control circuit coupled with the driving unit and receiving said scan driving signal generated by said operational interface to drive the antenna unit for space scanning in accordance with said scan pattern and scan coordinates,

wherein said antenna unit captures, during said space scanning, satellite signals from a plurality of satellites in the scanned space upon meeting said scan coordinates, said satellite signals include scan data, wherein said scan data includes peak values of the satellite signals strength;

a processing unit coupled with the driving control circuit for analyzing the scan data to obtain individual satellite coordinates of the satellites based on said peak values of said satellite signals strength in correspondence to said scan coordinates; and

a memory unit coupled with the processing unit for storing the satellite coordinates of the satellites;

wherein, upon receiving a lock-on signal for a target satellite from said operational interface, the processing unit captures the respective satellite coordinate of said target satellite from said memory unit according to the lock-on signal;

wherein, according to the captured satellite coordinate of the target satellite, the processing unit transmits an antenna control signal to the driving control circuit, the driving control circuit, responsive to said antenna control signal, sends a driving signal to the driving unit to point the antenna unit at the target satellite.

16. The antenna system according to claim 15, wherein said antenna unit is a digital video broadcasting-satellite (DVB-S) antenna.

17. The antenna system according to claim 16, wherein said antenna unit is a dish antenna.

18. The antenna system according to claim 16, wherein said antenna unit is a flat antenna.

19. The antenna system according to claim 15, wherein said antenna unit further has at least one DVB-S antenna and at least one digital video broadcasting-terrestrial (DVB-T) antenna, in which said driving system is coupled with the DVB-S antenna.

20. The antenna system according to claim 15, further including a mobile digital signal receiving/transmitting unit coupled with said antenna unit.

21. The antenna system according to claim 20, further including a control signal processing circuit, the control signal processing circuit further having a control signal amplifier coupled with said processing unit for amplifying a control signal generated from said processing unit.

22. The antenna system according to claim 21, wherein said control signal processing circuit further has a control signal driving circuit coupled with said mobile digital signal receiving/transmitting unit, the control signal amplifier and the antenna unit for controlling said mobile digital signal receiving/transmitting unit according to said control signal.

23. The antenna system according to claim 15, further including a satellite signal processing circuit, the satellite signal processing circuit further including a tuner coupled with said antenna unit for tuning a satellite signal received by said antenna unit.

24. The antenna system according to claim 23, wherein said satellite signal processing circuit further includes a decoder coupled with said tuner.

25. The antenna system according to claim 15, further including:

a global positioning system (GPS) coupled with said processing unit; and

a GPS antenna coupled with the GPS for obtaining a satellite position coordinate of said vehicle and further transmitting said antenna control signal according to said satellite position coordinate and said satellite coordinate of said target satellite.

26. The antenna system according to claim 15, further including a vehicle position-sensing unit coupled with said processing unit for obtaining a vehicle position of said vehicle, said antenna control signal being sent according to the vehicle position and said satellite coordinate of said target satellite.

27. The antenna system according to claim 26, wherein said vehicle position further includes an azimuth angle of said vehicle and an elevation angle of said vehicle and said vehicle position-sensing unit further includes:

a gyroscope for determining the azimuth angle; and

a gravity-sensing element for determining the elevation angle.

28. The antenna system according to claim 15, wherein said memory unit further includes:

a satellite coordinate memory area for storing said satellite coordinates of said satellites; and

a vehicle coordinate memory area for storing a vehicle coordinate and a vehicle position of said vehicle.

29. The antenna system according to claim 15, wherein said driving system is a step motor.

30. A method for driving at least one antenna device to lock on at least one of a plurality of satellites in the space, comprising the steps of:

(a) generating at an operational interface a scan driving signal representative of a scan pattern and scan coordinates,

(b) receiving at an antenna unit said scan driving signal from said operational interface to start a space scanning in accordance with said scan pattern and scan coordinates;

(c) capturing, at said antenna unit, satellite signals from the plurality of satellites in the scanned space upon meeting said scan coordinates, said satellite signals include a scan data, wherein said scan data includes peak values of said satellite signal strength;

(d) analyzing, at a processing unit operationally coupled to said antenna unit, the obtained scan data to obtain individual satellite coordinates of the satellites based on said peak values of said satellite signals strength in correspondence to said scan coordinates, and recording the respective satellite coordinates of the satellites in a memory unit;

(e) receiving at said processing unit a lock-on signal generated at said operational interface that defines one of the satellites to be locked as a target satellite, and retrieving from said memory unit the satellite coordinate of the target satellite in accordance with lock-on signal;

(f) sending from said processing unit to a driving control unit an antenna control signal corresponding to the satellite coordinate of the target satellite; and

(g) generating at a driving control unit a driving signal according to the antenna control signal to drive the antenna unit to point at the target satellite.

31. The method according to claim 30, wherein said step (d) is accomplished by the steps of:

(d1) said antenna unit performing said space scan according to plural scan coordinates in order to have said scan data containing individual signal strengths with respect to the scan coordinates;

(d2) checking in a predetermined order whether a current one of the signal strengths of said scan data is a local peak value;

(d3) if in said step (d2) said signal strength is a local peak value, checking further whether the peak value is induced by an interface signal (Qd3), otherwise, performing the step (d2); and

(d4) if the peak value is not induced by an interference signal, capturing said scan coordinate corresponding to the peak value to be one of said satellite coordinates and going back to perform the step (d2);

if the peak value is induced by an interference signal, performing the step (d2).

32. The method according to claim 31, wherein said antenna unit is mounted on a vehicle, said method further includes, between said step (d) and said step (e), the steps of:

receiving a dynamic position signal to obtain a vehicle coordinate of said antenna unit, and computing said satellite coordinates.

33. The method according to claim 32, wherein said dynamic position signal is a GPS dynamic position signal and said vehicle coordinate includes a satellite position coordinate of said vehicle.

34. The method according to claim 32, wherein said dynamic position signal is a vehicle dynamic position signal and said vehicle coordinate includes a vehicle position of said vehicle.

35. The method according to claim 32, wherein said antenna control signal is sent in accordance with said satellite coordinate and said vehicle coordinate.

36. The method according to claim 30, wherein said antenna unit is a digital video broadcasting-satellite (DVB-S) antenna.

37. The method according to claim 36, wherein said antenna unit is a dish antenna.

38. The method according to claim 36, wherein said antenna unit is a flat antenna.