Airbus France

Gilles Tatham

Eric Peyrucain

Michel Falcati

Diane Rambach

Dominique Pomies

Pierre Durel

The device () for behavior simulation of a radio navigation system, without the latter being installed on an aircraft, comprising a means () for determining a position of the aircraft, characterized in that it further comprises:

Method and device for simulating radio navigation instruments

An aircraft piloting system may include information sources that provide a position indication relating to the aircraft and information that characterizes a virtual approach axis. An information processing unit processes information emanating from the information sources and includes an assisted approach mode function and a landing aid multimode receiver that implements a precision approach. A user device uses the information provided by the landing aid multimode receiver to support the guidance of the aircraft up to its landing.

Aircraft piloting system, at least for piloting the aircraft during a non precision approach with a view to a landing

Maintenance process and device for a radionavigation installation of an aircraft. The maintenance device () comprises a first means of recording () for recording on a first recording medium () first events relating to data external to the aircraft, received by said radionavigation installation (), a second means of recording () for recording on a second recording medium () second events relating to malfunctions occurring on board the aircraft, and means () for making it possible to analyze said first and second events recorded on said first and second recording media (), so as to determine whether said radionavigation installation () should or should not be disassembled.

Maintenance process and device for a radionavigation installation of an aircraft

A system for aiding the landing of an aircraft on a runway uses an angular vertical position of the aircraft and includes at least one landing aid radio. In a stand-alone manner, the position of the aircraft in latitude and longitude is determined, and the position of the threshold of the runway in latitude and longitude is determined. A computing unit corrects, on the basis of positions of the aircraft and of the threshold of the runway, the angular vertical position of the aircraft. The corrected angular vertical position is used to aid the landing of the aircraft.

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La Salvetat Saint Gilles, France

Gilles Tatham