Viasat, Inc.

Bradley H Smith

E Mitchell Blalock

Kevin Mark Skinner

Jack C Newkirk

B Wayne Holt

Eric L Cross

James E Petranovich

Douglas J Merrell

Samuel C Finney

Ian F Winfield

Alex Yeshanov

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.

System and apparatus for driving antenna

Systems and methods are described herein for performing mispointing correction operations that can provide accurate pointing of an antenna towards a satellite, while also satisfying interference requirements with other satellites. As a result, the mispointing correction operations described herein can improve resource efficiency of communication systems using such antennas and help ensure compliance with interference requirements of other satellites.

Methods and systems for performing antenna pointing while mitigating interference with a nearby satellite

Disclosed is a method and apparatus for validating a two-way satellite communication system in an aircraft. The two-way satellite communication system may include a network access unit, a modem, and a satellite antenna assembly. A satellite link emulator may be disposed proximate the aircraft. A validation controller may initiate a validation test of the two-way satellite communication system using the satellite link emulator, including receiving, at the satellite link emulator, a transmitted uplink signal from the satellite antenna assembly, and transmitting, using the satellite link emulator, a downlink signal to the satellite antenna assembly in response to the received uplink signal. A pass/fail indication may be determined based on operation of the network access unit, the modem, and the satellite antenna assembly during the validation test.

Validation of a two-way satellite communication system without utilizing a satellite

Growing community of inventors

Cumming, GA, United States of America

Bradley H Smith