Airbus Operations (s.a.s.)

Thomas Koebel

Nicolas Albert

Boris Kozlow

Maxime Wachenheim

Thomas Pastre

Remy Laugero

A display method comprises a step during which an aircraft flight management computer sends display instructions to a display management system, to control the display of an aircraft flight plan window. The display method also comprises steps comprising acquiring a reference point and a vertical flight profile of the aircraft comprising the reference point, and computing, using the vertical flight profile, an altitude of the reference point. It also comprises steps comprising acquiring an information item relating to a flight phase associated with the reference point, acquiring an information item relating to a selected display range, determining a vertical centering coefficient of a display window relating to the vertical flight profile, as a function of the flight phase and transmitting, to the display management system, instructions for displaying the display window as a function of the altitude of the reference point and of the centering coefficient of the display window.

Method, device and system for displaying a vertical flight profile of an aircraft

A method and assembly for guidance of an aircraft during a low-altitude flight. The guidance assembly comprises a memory forming part of a flight management system, which is configured to store an active flight trajectory and any new flight trajectory, generated by the flight management system, and a memory forming part of a guidance system, which is configured to also store the flight trajectory and any new flight trajectory, which are received from the flight management system, the guidance assembly being configured to periodically transmit from the guidance system to the flight management system identification codes for the flight trajectories recorded in the memory of the guidance system.

Method and assembly for guidance of an aircraft during a low-altitude flight

A device for revising a low-altitude flight phase of a flight path of an aircraft includes an input unit configured to allow an operator to input parameters to define an intermediate flight section (Si) which has to be inserted into a low-altitude flight phase, and a processing unit configured to calculate a profile relating to the intermediate flight section (Si) using input parameters, and to automatically insert this profile into the flight phase between a first upstream part (P) and a second downstream part (P) so as to establish a revised flight phase (PR).

Method and device for revising a low-altitude flight phase of a flight path of an aircraft

A method and device for displaying the performance of an aircraft when climbing and/or descending. The device includes devices for data capture, calculation and generating images for a display screen. The calculation device is configured to calculate a maximum slope that the aircraft can adopt depending on current data received from a data capture device. A display device presents images of the maximum slope superimposed with altitudes of a projected flight plan.

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Toulouse, France

Thomas Koebel