US 2011/0032143 A1 · Fixed User Terminal for Inclined Orbit Satellite Operation

Abstract

An advanced multiple-beam fixed ground terminal is achieved that is capable of simultaneously tracking multiple inclined orbit satellites, increasing and suppressing gain in multiple directions. The fixed user terminal equipped with digital beam-forming and null-forming technique can track and identify signals from multiple inclined orbit satellites at the same time. This technique enables a geostationary satellite drift to an inclined orbit without losing communication with ground terminals which not only increase the life span of an inclined orbit satellite, but also relieve the scarcity of geo-stationary orbit. In extreme cases, satellite can be placed in the same slot which further enhanced the usage of geosynchronous orbits. Another present invention is to from double nulls whose null width is much wider than a single null. A wider null increases the system robustness to frequency drift and change of signal direction, thus in turn reduce the system's complexity by lowering update beam wave vectors. To use the same beam wave vector on wider frequency spans, an FIR filter need to be designed according to system requirements.

Claims10

Dependent claims

A mechanically fixed ground user terminal transceiver which is capable of performing a one-dimensional electronic scan and tracking with a range from −15 to +15 degrees, with the present fixed user terminal comprising:

an antenna array composed of a plurality of antenna elements;
at least one low noise amplifier and one frequency down converter connected to the plurality of antenna elements and adapted to down-convert the signals from the plurality of antenna elements to at least one of an intermediate frequency and baseband frequency;
a memory element adapted to store calibration data comprising beam weighting vectors associated with plurality of said antenna elements;
a digital beam forming (DBF) processor adapted to process the frequency down-converted signals from the plurality of antenna elements, wherein the DBF processor is further adapted to:
apply the beam weighting vectors to the frequency down-converted signals,
selectively combine one or some of the weighted down-converted signals,
create at least one coherent beam from the combination of the weighted down converted signals;
an array processor adapted to control the DBF which processes the down-converted signals from the plurality of antenna elements, wherein the array processor is further adapted to:
dynamically assign one or some of multiple array elements to form at least on beam
dynamically alter the beam weighting vectors (BWVs) to change a pointing direction of the at least one coherent beam for tracking at least one of the plurality of GPS satellites.

7 more elements

Dependencies are inferred from the claim text.

Fixed User Terminal for Inclined Orbit Satellite Operation

Life of this patent

Fixed User Terminal for Inclined Orbit Satellite Operation

Life of this patent

Abstract

Claims10