The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
May. 06, 2025

Filed:

May. 30, 2024
Applicant:

Viasat, Inc., Carlsbad, CA (US);

Inventors:

Lance B. Diamond, Johns Creek, GA (US);

Donald L. Runyon, Duluth, GA (US);

Eric L. Cross, Alpharetta, GA (US);

Assignee:

Viasat, Inc., Carlsbad, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H01Q 1/28 (2005.12); H01Q 1/42 (2005.12); H01Q 3/02 (2005.12); H01Q 3/08 (2005.12); H01Q 3/24 (2005.12); H01Q 21/06 (2005.12); H01Q 21/28 (2005.12); H04B 7/06 (2005.12); H04B 7/08 (2005.12); H04B 7/185 (2005.12); H04B 7/195 (2005.12);
U.S. Cl.
CPC ...
H01Q 1/28 (2012.12); H01Q 1/42 (2012.12); H01Q 3/02 (2012.12); H01Q 3/08 (2012.12); H01Q 3/24 (2012.12); H01Q 21/06 (2012.12); H01Q 21/28 (2012.12); H04B 7/0608 (2012.12); H04B 7/0814 (2012.12); H04B 7/18508 (2012.12); H04B 7/1851 (2012.12); H04B 7/195 (2012.12);
Abstract

In one example, an antenna system is described. The antenna system includes a primary antenna on an aircraft. The primary antenna is mechanically steerable and has an asymmetric antenna beam pattern with a narrow beamwidth axis and a wide beamwidth axis at boresight. The antenna system also includes a secondary antenna on the aircraft, the secondary antenna including an array of antenna elements. The antenna system also includes an antenna selection system to control communication of a signal between the aircraft and a target satellite via the primary antenna and the secondary antenna. The antenna selection system switches communication of the signal from the primary antenna to the secondary antenna when a performance characteristic for communication with the target satellite satisfies a threshold due to a position of the aircraft relative to the target satellite.


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