System and apparatus for driving antenna

Patent metadata

Field	Value
Publication number	US-10985449-B2
Application number	US-202016736957-A
Country	US
Kind code	B2
Filing date	Jan 8, 2020
Priority date	Jun 27, 2014
Publication date	Apr 20, 2021
Grant date	Apr 20, 2021

Abstract

A multiple-antenna positioning system with a single drive element, providing reduced weight and complexity over systems that have a drive element for each antenna. In certain examples, each antenna can be coupled with a rotating spindle, with each antenna spindle being coupled with a pair of link arms. By driving a single drive spindle, each of the antenna spindles in the system can be rotated by the associated pair of link arms. The link arms can have an adjustable length, such as through a turnbuckle mechanism, to reduce backlash in the system, and in some examples can apply a preload to the system. By reducing backlash, the multiple antenna positioning system can have improved responsiveness to a rotation of the single drive element, as well as improved stability of the positioning of each antenna when the drive element is held in a fixed position.

First claim

What is claimed is:

1. An antenna assembly, comprising:
a first antenna having a first boresight;
a second antenna having a second boresight that is not parallel with the first boresight;
a first drive element configured to simultaneously change an elevation angle of the first boresight and change an elevation angle of the second boresight; and
a second drive element configured to simultaneously change an azimuth angle of the first boresight and change an azimuth angle of the second boresight.

2. The antenna assembly of claim 1 , wherein the first drive element is configured to change the elevation angle of the first boresight about a first axis and change the elevation angle of the second boresight about a second axis that is non-coincident with the first axis.

3. The antenna assembly of claim 1 , wherein the first drive element is configured to change the elevation angle of the first boresight about a first axis and change the elevation angle of the second boresight about a second axis that is non-parallel with the first axis.

4. The antenna assembly of claim 1 , wherein the second drive element is configured to change the azimuth angle of the first boresight and the azimuth angle of the second boresight about a same axis.

5. The antenna assembly of claim 1 , wherein the azimuth angle of the first boresight and the azimuth angle of the second boresight are separated by a fixed angle.

6. The antenna assembly of claim 1 , wherein the azimuth angle of the first boresight and the azimuth angle of the second boresight are separated by 180 degrees.

7. The antenna assembly of claim 1 , wherein the first antenna is configured to operate over a first frequency band, and the second antenna is configured to operate over a second frequency band that is different from the first frequency band.

8. The antenna assembly of claim 1 , further comprising:
an antenna control unit operable to cause the antenna assembly to:
track a first satellite for communications via the first antenna; and
track a second satellite for communications via the second antenna.

9. The antenna assembly of claim 8 , wherein the antenna control unit is operable to determine to switch between communications via the first antenna and communications via the second antenna.

10. The antenna assembly of claim 8 , wherein the antenna control unit is operable to determine to switch between communications via the first antenna and communications via the second antenna based at least in part on a change of position of the antenna assembly.

11. The antenna assembly of claim 8 , wherein the antenna control unit is operable to determine to switch between communications via the first antenna and communications via the second antenna based at least in part on a network availability, a communication capacity, or a communication cost, or a combination thereof.

12. The antenna assembly of claim 8 , wherein the antenna control unit is operable to determine to switch between communications via the first antenna and communications via the second antenna based at least in part on an error condition or a fault condition.

13. The antenna assembly of claim 8 , wherein the antenna control unit is operable to determine to switch between communications via the first antenna and communications via the second antenna based at least in part on a degradation of communications via the first antenna.

14. A method of communication, comprising:
tracking a first target device for communications via a first antenna having a first boresight, wherein tracking the first target device comprises positioning the first boresight in an elevation direction using a first drive element and positioning the first boresight in an azimuth direction using a second drive element;
determining to switch from communications via the first antenna to communications via a second antenna having a second boresight that is not parallel with the first boresight;
tracking a second target device for communication via the second antenna, wherein tracking the second target device comprises positioning the second boresight in the elevation direction using the first drive element and positioning the second boresight in the azimuth direction using the second drive element.

15. The method of claim 14 , wherein the first target device is a first satellite, and the second target device is a second satellite that is different than the first satellite.

16. The method of claim 14 , wherein determining to switch from communications via the first antenna to communications via the second antenna comprises:
determining to switch from communication with the first target device to communication with the second target device.

17. The method of claim 14 , wherein determining to switch from communications via the first antenna to communications via the second antenna is based at least in part on a change of position of an antenna assembly that includes the first antenna and the second antenna.

18. The method of claim 14 , wherein determining to switch from communications via the first antenna to communications via the second antenna is based at least in part on a network availability, a communication capacity, a communication cost, or a combination thereof.

19. The method of claim 14 , wherein determining to switch from communications via the first antenna to communications via the second antenna is based at least in part on an error condition or a fault condition.

20. The method of claim 14 , wherein determining to switch from communications via the first antenna to communications via the second antenna is based at least in part on a degradation of communications via the first antenna.

Assignees

• Viasat Inc

Inventors

• Newkirk Jack C
• Holt B Wayne
• Smith Bradley H
• Skinner Kevin M
• Blalock E Mitchell

Classifications

• H01Q3/06

  over a restricted angle · CPC title

• H01Q21/28

  Combinations of substantially independent non-interacting antenna units or systems {(multiple beam H01Q25/00)} · CPC title

• H04B7/18519

  Operations control, administration or maintenance · CPC title

• G01N1/14

  Suction devices, e.g. pumps; Ejector devices · CPC title

• B01L3/021

  Pipettes, i.e. with only one conduit for withdrawing and redistributing liquids · CPC title