Honeywell International Inc.

Honeywell Spol, S.r.o.

Radek Zaruba

Martin Mlaskac

Petr Kanovsky

Alfonso Malaga

Jan Bilek

Vit Stencel

Andrew James Fraser

Karel Adamek

David Whittleton

Jan Kubalcik

Petr Burian

In one embodiment, a secure communications processor is provided. The secure communications data processor comprises a satellite datalink gateway; wherein the satellite datalink gateway is configured to translate data, to be transmitted to or received from a satellite communications system, from a first internet protocol to at least one of a second internet protocol or another protocol, and to be received by or transmitted from a router; a satellite communications link processor coupled to the satellite datalink gateway; and wherein the secure communications data processor is configured to be coupled between at least one router and a satellite communications radio system, and to be installed in a vehicle separately from the at least one router and the satellite communications radio system.

System and method for satellite communications link

A radio system comprises a plurality of software defined radio units, and a plurality of digital data switches each in operative communication with at least one of the radio units, with the digital data switches operatively connected to each other. A plurality of antenna units are each in operative communication with at least one of the radio units through at least one of the digital data switches. A plurality of radio resources managers are each operatively coupled to one or more of the digital data switches, with each of the radio resources managers configured to control one or more of the digital data switches to route digital data between the radio units and the antenna units.

Interconnection fabric with protocol agnostic switch for flexible radio avionics

The radio system comprises a radio unit and an antenna unit coupled to the radio unit. The antenna unit is physically separate and located remote from the radio unit. The antenna unit further comprises a digital pre-distortion engine configured to pre-distort a modulated digital data signal; a digital to analog converter configured to convert the pre-distorted digital data signal to a pre-distorted analog data signal; and a power amplifier configured to amplify the pre-distorted analog data signal which distorts the pre-distorted analog data signal. The distortion introduced by the power amplifier is opposite to the pre-distortion introduced by the digital pre-distortion engine such that the pre-distortion introduced by the digital pre-distortion engine approximately cancels the distortion introduced by the power amplifier. The radio unit further comprises a coefficient computation engine configured to calculate coefficients used by the digital pre-distortion engine to pre-distort the modulated digital data signal.

System and method for digital predistortion

In one embodiment, a main radio unit for an avionic communication system is provided. The main radio unit includes a software defined radio (SDR) configured to simultaneously provide at least one safety certified channel for a cockpit of an aircraft and at least one other channel for cabin services of the aircraft, wherein the SDR is configurable such that the SDR can generate signals corresponding to different communication protocols. The main radio unit also includes an interface for the at least one safety certified channel, wherein the interface is configured to convert signals between a protocol for hardware in the cockpit and a satellite communication protocol used by the SDR for the at least one safety certified channel; and wherein the SDR is configured to communicate with an RF unit for transmission and reception of signals over an antenna.

Reconfigurable satcom avionics radio

Systems and methods for acquiring global navigation satellite system (GNSS) signals. An incoming signal is multiplied with a time shifted spreading code replica and converted to zero (or very low) nominal frequency. The converted signal is filtered and downsampled by a large scale. A signal power metric and frequency offset are then determined. This is performed over multiple slices. Fast acquisition is achieved by parallel concatenation of numerous slices.

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Decin, Czechia

Radek Zaruba