Patent application number | Description | Published |
20130026299 | Method And Device For An Optimal Management Of The Slats, The Flaps And The Landing Gear Of An Aircraft - Method and device for an optimal management of the slats, the flaps and the landing gear of an aircraft. | 01-31-2013 |
20130030611 | METHOD AND DEVICE FOR AN OPTIMAL MANAGEMENT OF THE VERTICAL TRAJECTORY OF AN AIRCRAFT - The device ( | 01-31-2013 |
20130030612 | METHOD AND DEVICE FOR AN OPTIMAL MANAGEMENT OF THE ENERGY OF AN AIRCRAFT - Method and device for an optimal management of the energy of an aircraft. | 01-31-2013 |
20130184900 | VEHICLE ENERGY CONTROL SYSTEM WITH A SINGLE INTERFACE - A system for controlling energy of a vehicle, for example an aircraft, characterized in that it comprises:
| 07-18-2013 |
20130190949 | VEHICLE ENERGY CONTROL SYSTEM - A system for controlling energy of a vehicle, for example an aircraft, comprising a control interface able to be in at least one first and one second state, the first state being an instruction state in which the interface generates at least a first instruction for speed of variation of a current energy of the vehicle and the second state being a resting state in which it gives no instruction, the interface furthermore being configured to return into the second state after having been brought into the first state. | 07-25-2013 |
20140039731 | METHOD AND DEVICE FOR AIDING THE MANAGEMENT OF THE FLIGHT OF AN AIRCRAFT - 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. | 02-06-2014 |
20140346280 | System And Method For Controlling An Aircraft - A system for controlling an aircraft control parameter including a control interface including a mobile element configured to move on a travel, of which at least two portions are separated by a neutral position; a return element bringing the mobile element back to the neutral position when it is not actuated; and an interaction element, and a control unit configured to memorize an item of information corresponding to a first position of the mobile element at an instant of activation of the interaction element; and generate a setpoint of the aircraft control parameter, as a function of a control associated with the first position of the mobile element for which said information has been memorized; or a current position of the mobile element, when this current position is situated on the same portion of travel as the first position and is more remote than the latter from the neutral position. | 11-27-2014 |
20150276428 | METHOD AND SYSTEM FOR ASSISTING THE PILOTING OF AN AIRCRAFT - A method for assisting the piloting of an aircraft landing on a runway comprising determining current flight conditions of the aircraft, determining, with the help of the current flight conditions, the following distances between projections, in a horizontal plane, of the current position of the aircraft and a position of contact with the ground: a minimum approach distance; a standard approach distance; and a distance to destination according to a predetermined flight path. The method includes placing the three distances in order according to their respective values, and displaying, along a scale of a screen in the aircraft cockpit, a first, a second and a third symbol respectively associated with the minimum approach distance, with the standard approach distance and with the distance to destination, these three symbols being placed in order on the scale according to the order of the distances with which they are associated. | 10-01-2015 |