Airbus Operations (s.a.s.)

Airbus (sas)

Airbus Operations Gmbh

Airbus Corporation

Pascale Louise

Thierry Bourret

Xavier Dal Santo

Nicolas Chauveau

Emmanuel Cortet

Pierre Scacchi

Jean Muller

Pierre Depape

Claire Ollagnon

Sebastien S Giuliano

Thomas Stanislawiak

Francois Bounaix

Patrice Rouquette

Florian Constans

Jacques Rosay

Nicolas Caule

Fabien Perrin

Josep Boada-Bauxell

Erwin Grandperret

Sylvain Devineau

Charles Renault Leberquer

Alain Dupre

Delphine MacDonald

Sébastien Drieux

Fabien Silly

Francois Melin

Anthony Atencia

Marie-Odile Plantecoste

Charles Renault Lerberquer

François Melin

Christian Serieyssol

A taxiing path optimization system is provided for computing a taxi path of an aircraft using available taxi routes of a corresponding airport. An interaction means management unit manages interactions between a user and the taxiing path optimization system using an interactive device for inputting a taxi clearance. An aircraft positioning management unit manages positional information of the corresponding airport and aircraft received from a plurality of sources for augmenting an aircraft position by consolidating the aircraft position with the positional information in a complementary fashion. A taxi path display unit displays the taxi path based on the inputted taxi clearance and the augmented aircraft position, wherein the taxi path is automatically computed based on aircraft characteristics or airport capabilities.

Systems and methods for providing optimized taxiing path operation for an aircraft

A method is described for aiding the piloting of an airplane by ensuring availability of an automatic pilot that is normally controlled as a function of speed information of the airplane when the speed information is lost. The method includes detecting a loss of the speed information of the airplane. In response to the detection of the loss of the speed information, the method includes determining flight data of the airplane being independent from the speed information of the airplane, determining control parameters from the flight data, and controlling the automatic pilot based on the control parameters and without the speed information of the airplane. The automatic pilot includes an automatic piloting system or a flight director.

Automatic method and device for aiding the piloting of an airplane

Methods, systems, and computer readable media are disclosed for direct arming aircraft runway approach guidance modes, for example and without limitation, for aircraft operational. In some aspects, a method for directly arming a runway approach guidance mode of an aircraft includes displaying on a display unit an airport, selecting the airport and selecting an active runway for final approach, displaying an path toward the selected final approach runway, selecting the final approach runway, displaying on the display unit at least one symbol associated with at least one runway approach guidance mode, and arming at least one of the at least one runway approach guidance mode.

Methods, systems and computer readable media for arming aircraft runway approach guidance modes

The display device comprises display means which highlight on a screen, preferably of PFD type, the information useful to the pilot relating to at least one flight parameter, especially while reducing the corresponding scale on said screen.

Method and device for displaying flight parameters on an aircraft

An aircraft ground or sea approach anomaly detection method. The method includes the steps of characterizing a flight phase of the aircraft, determining a prohibited flight envelope, defining a set of prohibited vertical speeds of the aircraft for given altitudes in relation to the ground or the sea, as a function of the flight phase of the aircraft characterized, and detecting a ground approach anomaly of the aircraft as a function of a current vertical speed and altitude in relation to the ground or the sea of the aircraft, in relation to the prohibited flight envelope determined.

Detection of aircraft descent anomaly

Aircraft cockpit display screen with graphical user interface

The device comprises servocontrol means which automatically control, in a combined manner, an automatic thrust system of the aircraft and airbrakes of the aircraft, as a supplement to usual means for steering the vertical trajectory, so that the aircraft attains a speed setpoint and/or altitude setpoint, at the location defined by a geographical constraint.

Method and device for aiding the management of the flight of an aircraft

A device includes means for generating and applying to an aircraft protecting orders avoiding a flight with an excessive descent rate. More specifically, the device includes components configured to perform a series of operations including measuring the current vertical speed and the current height of the aircraft and comparing these flight parameters with a safety envelope defining couples of vertical speed and height that are indicative of an excessive descent rate. If the current vertical speed and height are located in the safety envelope, a protection is triggered by generating protecting orders to remove the aircraft from the safety envelope and applying those protecting orders to control surfaces of the aircraft.

Method and device for automatically protecting an aircraft against an excessive descent rate

The guiding mode transition aiding device includes a target heading determining device and a mode transition triggering system. The target heading determining device is configured to determine a target heading which represents the heading value reached by the aircraft at the end of a procedure of folding the wings of the aircraft flat from a current operating state. The mode transition triggering system receives the target heading and compares the target heading to a desired heading to be reached by the airplane to assist with triggering a transition between a rolling angle holding mode, in which the aircraft flies with a constant rolling angle, to a heading holding mode, in which the aircraft flies with a constant heading. This device and associated methods may be used during in flight refueling operations.

Method and device for aiding the control of guiding modes transitions of an aircraft

A method of aiding the piloting of an airplane ensures the availability of an automatic pilot and a thrust regulation system on board the airplane. To this end, the method includes determining first information by measuring the actual airspeed of the airplane, and this first information is used to control the automatic pilot and the thrust regulation system in a primary mode during normal operations of the airplane. When the first information is lost by becoming unavailable or unreliable, the automatic pilot and the thrust regulation system are each controlled in a secondary mode by control parameters determined using additional flight data independent from the actual airspeed of the airplane and the first information. Consequently, an alternative or redundant control is supplied for ensuring the continued operation of an automatic pilot without necessary intervention from crew members on board the airplane.

A device for aiding the flight management of an aircraft includes a calculation device for determining in real time an updated lateral trajectory that the aircraft will follow and a display device for displaying this updated lateral trajectory on a cockpit screen of the aircraft. Consequently, the crew of the aircraft is able to readily visualize and understand the updated lateral trajectory that will put the aircraft back on the original course as a result of the display on the display device.

Method and device for aiding the flight management of an aircraft

Button for an aircraft control device

Growing community of inventors

Toulouse, France

Pascale Louise