DUAL-ANGLE ADJUSTMENT OF A SATELLITE-TRACKING ANTENNA WITH A SINGLE MOTOR

• US 20100259458A1
• Filed: 04/14/2009
• Published: 10/14/2010
• Est. Priority Date: 04/14/2009
• Status: Abandoned Application

• Current Assignee: Qualcomm, Inc.
• Original Assignee: Qualcomm, Inc.
• Inventors: Benacka, Thomas J., Mattis, Eric S., Tian, Bin
• Application Number:
  US12/423,620
• Publication Number:
  US 20100259458A1
• Time in Patent Office: Days
• US Class Current: 343/766
• CPC Class Codes: H01Q 1/3275 mounted on a horizontal surface of the vehicle, e.g. on roof, hood, trunk
• CPC Class Codes: H01Q 3/08 for varying two co-ordinates of the orientation

Abstract

An apparatus includes an azimuth adjuster coupled between a motor and a directional antenna. Motor rotation causes the azimuth adjuster to rotate the antenna about an azimuthal axis. The motor rotation also causes an elevation adjuster to rotate, which causes a screw mechanism to modify an elevation angle by pivoting the antenna about an elevational axis. To aim the directional antenna, a body-direction vector of a movable body with the antenna attached thereto is determined. Based on an elevational relationship between the body-direction vector and a satellite-direction vector, the elevation adjuster modifies the elevation angle of the antenna by rotating the motor to achieve full-turn amounts to pivot the antenna. The azimuth adjuster modifies an azimuth angle of the antenna based on an azimuthal relationship between the body-direction vector and the satellite-direction vector by rotating the motor to achieve partial-turn amounts of the antenna.

Claims

1. An antenna aiming apparatus, comprising:

a motor including a motor spindle;

a directional antenna;

an azimuth adjuster operably coupling the motor spindle and the directional antenna, the azimuth adjuster for rotating the directional antenna about an azimuthal axis responsive to a motor rotation;

an elevation adjuster operably coupled with the motor and for rotating responsive to the motor rotation; and

a screw mechanism operably coupled to the elevation adjuster and for modifying an elevation angle of the directional antenna responsive to a rotation of the elevation adjuster.

2. The antenna aiming apparatus of claim 1, wherein the elevation adjuster comprises:

a first gear fixedly coupled to a fixed portion of the antenna aiming apparatus; and

an elevation gear rotationally coupled with the screw mechanism and engaged with the first gear.

3. The antenna aiming apparatus of claim 1, wherein the elevation adjuster comprises an elevation spindle rotationally coupled with the screw mechanism and further comprising a conveyor operably coupled between a fixed portion of the antenna aiming apparatus and the elevation spindle for coupling a rotational motion between the directional antenna and the elevation spindle.

4. The antenna aiming apparatus of claim 3, wherein the conveyor is selected from the group consisting of a belt, a chain, and engaged gears.

5. The antenna aiming apparatus of claim 3, wherein the conveyor comprises:

a first gear fixedly coupled to a fixed portion of the antenna aiming apparatus; and

an elevation gear fixedly coupled to the elevation spindle and engaged with the first gear.

6. The antenna aiming apparatus of claim 3, wherein the conveyor comprises:

a first gear fixedly coupled to a fixed portion of the antenna aiming apparatus;

an intermediate gear including an intermediate spindle and engaged with the first gear; and

a bevel gear fixedly coupled to the elevation spindle and engaged with a bevel gear fixedly coupled to the intermediate gear.

7. The antenna aiming apparatus of claim 1, further comprising a linkage operably coupled between the screw mechanism and the directional antenna for pivotally adjusting the directional antenna about an elevational axis.

8. An antenna aiming apparatus, comprising:

a motor including a motor spindle;

a directional antenna fixedly attached to the motor spindle;

a first gear fixedly attached to the motor;

an elevation gear engaged with the first gear, the elevation gear including an elevation spindle; and

a screw mechanism coupled between the elevation spindle and the directional antenna.

9. The antenna aiming apparatus of claim 8, further comprising a linkage operably coupled between the screw mechanism and the directional antenna.

10. An antenna aiming apparatus, comprising:

a motor including a motor spindle;

a directional antenna;

an azimuth adjuster operably coupling the motor and the directional antenna and comprising;

a clutch plate fixedly attached to the directional antenna; and

a clutch arm fixedly attached to the motor spindle and for engaging with the clutch plate to rotate the directional antenna about an azimuthal axis as the motor spindle rotates;

an elevation adjuster operably coupling the motor and the directional antenna and comprising;

a solenoid for engaging with the clutch plate to inhibit rotation of the clutch plate; and

a conveyor operably coupled to the motor spindle to move the conveyor to and fro as the motor spindle rotates; and

a linkage fixedly coupled to the conveyor to pivot the directional antenna about an elevational axis as the conveyor moves to and fro.

11. The antenna aiming apparatus of claim 10, further comprising a detent mechanism for biasing the clutch arm against the clutch plate to inhibit slippage of the clutch arm relative to the clutch plate when the solenoid is not engaged with the clutch plate and to allow slippage of the clutch arm relative to the clutch plate when the solenoid is engaged with the clutch plate.

12. An antenna aiming apparatus, comprising:

a motor;

a directional antenna;

an azimuth adjuster operably coupling the motor and the directional antenna, the azimuth adjuster adapted to rotate the directional antenna about an azimuthal axis responsive to a motor rotation;

an elevation adjuster operably coupled with the motor and for rotating responsive to the motor rotation; and

a screw mechanism operably coupling the elevation adjuster and the directional antenna and for modifying an elevation angle of the directional antenna responsive to a rotation of the motor; and

a controller operably coupled to the motor for determining a motor rotation amount.

13. The antenna aiming apparatus of claim 12, wherein the controller further comprises a GPS receiver for determining GPS coordinates and the controller is further for:

determining an elevation and a body-direction vector responsive to the GPS coordinates; and

determining the motor rotation amount responsive to the body-direction vector.

14. The antenna aiming apparatus of claim 12, wherein the controller further comprises an inertial sensor for determining inertial information about a movable body to which the antenna aiming apparatus is attached and the controller is further for:

determining an body-direction vector responsive to the inertial information; and

determining the motor rotation amount responsive to the body-direction vector.

15. The antenna aiming apparatus of claim 12, wherein the controller further comprises a signal monitor for detecting a signal on the antenna and the controller is further for:

determining a strength of the signal; and

determining the motor rotation amount responsive to the strength of the signal.

16. A method, comprising:

determining a body-direction vector of a movable body with a satellite-tracking antenna attached thereto;

adjusting an elevation angle of the satellite-tracking antenna responsive to an elevational relationship between the body-direction vector and a satellite-direction vector by rotating a motor to achieve full-turn amounts of the satellite-tracking antenna; and

adjusting an azimuth angle of the satellite-tracking antenna responsive to an azimuthal relationship between the body-direction vector and the satellite-direction vector by rotating the motor to achieve partial-turn amounts of the satellite-tracking antenna.

17. The method of claim 16, wherein determining the body-direction vector comprises:

periodically determining GPS locations of the movable body; and

establishing the body-direction vector from at least two of the GPS locations.

18. The method of claim 16, wherein determining the body-direction vector comprises acquiring inertial information from inertial sensors attached to the movable body.

19. The method of claim 16, further comprising adjusting the elevation angle of the satellite-tracking antenna responsive to a determination that the movable body has performed substantially a full rotation by rotating the motor to achieve one full-turn amount of the satellite-tracking antenna.

20. A method, comprising:

performing a signal strength analysis for a satellite-tracking antenna attached to a movable body;

adjusting an elevation angle of the satellite-tracking antenna responsive to the signal strength analysis by rotating a motor to achieve full-turn amounts of the satellite-tracking antenna;

adjusting an azimuth angle of the satellite-tracking antenna responsive to the signal strength analysis by rotating the motor to achieve partial-turn amounts of the satellite-tracking antenna; and

periodically repeating the performing the signal strength analysis, the adjusting the elevation angle and the adjusting the azimuth angle to enhance a signal strength for the satellite-tracking antenna.

21. The method of claim 20, further comprising:

determining a body-direction vector of the movable body;

adjusting the elevation angle of the satellite-tracking antenna responsive to an elevational relationship between the body-direction vector and a satellite-direction vector by rotating the motor to achieve the full-turn amounts of the satellite-tracking antenna; and

adjusting the azimuth angle of the satellite-tracking antenna responsive to an azimuthal relationship between the body-direction vector and the satellite-direction vector to achieve the partial-turn amounts of the satellite-tracking antenna.

22. The method of claim 21, wherein determining the body-direction vector comprises:

periodically determining GPS locations of the movable body; and

establishing the body-direction vector from at least two of the GPS locations.

23. The method of claim 21, wherein determining the body-direction vector comprises acquiring inertial information from inertial sensors attached to the movable body.

24. A method, comprising:

periodically determining GPS locations of a movable body with a satellite-tracking antenna attached thereto;

determining an elevation of the movable body from at least one of the GPS locations;

determining a body-direction vector of the movable body from at least two of the GPS locations;

adjusting an elevation angle of the satellite-tracking antenna responsive to the elevation by rotating a motor to achieve full-turn amounts of the satellite-tracking antenna; and

adjusting an azimuth angle of the satellite-tracking antenna responsive to an azimuthal relationship between the body-direction vector and the satellite-direction vector to by rotating the motor to achieve partial-turn amounts of the satellite-tracking antenna.

25. A system, comprising:

means for determining a body-direction vector of a movable body with a satellite-tracking antenna attached thereto; and

means for coupling adjustments to an elevation angle and adjustments to an azimuth angle of a satellite-tracking antenna with a same motor rotation responsive to a relationship between the body-direction vector and a satellite-direction vector, wherein the satellite-tracking antenna rotates responsive to the motor, and wherein;

full-turn amounts of the satellite-tracking antenna adjust the elevation angle; and

partial-turn amounts of the satellite-tracking antenna adjust the azimuth angle.

26. The system of claim 25, wherein the means for determining the body-direction vector comprises means for acquiring inertial information of the movable body.

27. The system of claim 25, wherein the means for determining the body-direction vector comprises:

means for periodically determining GPS locations of the movable body; and

means for establishing the body-direction vector from at least two of the GPS locations.

28. The system of claim 25, further comprising means for adjusting the elevation angle of the satellite-tracking antenna responsive to a means for determining that the movable body has performed substantially a full rotation by rotating the motor to achieve one full-turn amount of the satellite-tracking antenna.

29. The system of claim 25, further comprising:

means for performing a signal strength analysis of the satellite-tracking antenna;

means for rotating the motor at least one additional full-turn amount to adjust the elevation angle of the satellite-tracking antenna responsive to the signal strength analysis; and

means for rotating the motor an additional partial-turn amount to adjust the azimuth angle of the satellite-tracking antenna responsive to the signal strength analysis.