Thales

Issoire Aviation

Eric Guillouet

Sylvain Lissajoux

Marc Riedinger

Christophe Garnavault

Joël Bosson

Thibaut Debard

Joel Bosson

Romain Klur

Pierre Gutierrez

Antoine Bonnet

Patrick Gouhier

The present invention relates to an aid system () for piloting an aircraft, the aircraft including at least two piloting units each having at least one piloting member that can be actuated by a pilot to command at least one control surface of the aircraft. The piloting aid system () includes a module () for detecting actions performed on at least one piloting unit and a feedback module () indicating, via a man-machine interface (A,B) separate from the piloting members, the movement of said piloting member and/or the force exerted on said piloting member.

Pilot assistance system of an aircraft

This method makes it possible to generate a resulting setpoint trajectory of an aircraft, a guiding system controlling the trajectory of the aircraft relative to the resulting setpoint trajectory. The generating method is implemented by an electronic device and comprises selecting at least one mode from among several operating modes, acquiring a setpoint trajectory prepared by a flight management system, obtaining an alternative setpoint trajectory from an element from among a module for computing a trajectory and an external generating system, and generating the resulting setpoint trajectory, which includes one or several segments of the alternative setpoint trajectory for the period of time corresponding to the selection of another mode.

Method and device for generating a resulting setpoint trajectory of an aircraft, related computer program product and aircraft

A method and device for generating at least one set point from a flight control set point, a motor control set point and an aircraft guidance set point, a related computer program product and an aircraft are disclosed. In one aspect, the method includes acquiring a mechanical property relative to at least one corresponding primary control member and computing at least one set point from among one or more primary set points and one or more secondary set points. The method also includes generating at least one of the computed set point(s) and switching, based on the mechanical property acquired for the corresponding primary control member, between a first mode in which one or more primary set points are generated and a second mode in which one or more secondary set points are generated.

Method and device for generating at least one set point from a flight control set point, a motor control set point and an aircraft guidance set point, related computer program product and aircraft

Growing community of inventors

Toulouse, France

Eric Guillouet