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公开(公告)号：US09550562B2
公开(公告)日：2017-01-24
申请号：US14283290
申请日：2014-05-21
Applicant: Airbus Operations S.A.S.
Inventor： Florian Constans , Josep Boada-Bauxell , Pierre Scacchi
Abstract: 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.
Abstract translation: 一种用于控制飞行器控制参数的系统，其包括控制接口，所述控制接口包括被配置为在行程上移动的移动元件，其中至少两个部分被中立位置分隔; 返回元件，当移动元件未被启动时返回到中立位置; 以及控制单元，被配置为在所述交互元件的激活时刻存储对应于所述移动元件的第一位置的信息项; 并且根据与已经存储了所述信息的移动元件的第一位置相关联的控制来生成飞行器控制参数的设定点; 或当该当前位置位于与第一位置相同的行进部分上并且比中立位置更远离移动元件的当前位置时，移动元件的当前位置。
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Patent Agency Ranking
公开(公告)号：US20140346280A1
公开(公告)日：2014-11-27
申请号：US14283290
申请日：2014-05-21
Applicant: AIRBUS OPERATIONS S.A.S.
Inventor： Florian Constans , Josep Boada-Bauxell , Pierre Scacchi
Abstract: 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.
Abstract translation: 一种用于控制飞行器控制参数的系统，其包括控制接口，所述控制接口包括被配置为在行程上移动的移动元件，其中至少两个部分被中立位置分隔; 返回元件，当移动元件未被启动时返回到中立位置; 以及控制单元，被配置为在所述交互元件的激活时刻存储对应于所述移动元件的第一位置的信息项; 并且根据与已经存储了所述信息的移动元件的第一位置相关联的控制来生成飞行器控制参数的设定点; 或当该当前位置位于与第一位置相同的行进部分上并且比中立位置更远离移动元件的当前位置时，移动元件的当前位置。
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公开(公告)号：US20180090019A1
公开(公告)日：2018-03-29
申请号：US15562709
申请日：2016-04-04
Applicant: Airbus Operations S.A.S.
Inventor： Pierre Scacchi , Thibault Lefez
CPC classification number: G08G5/065 , G01C23/00 , G08G5/0008 , G08G5/0021 , G08G5/0078
Abstract: In an aircraft including a cockpit, a unit for monitoring the situation of the aircraft and a radio communication unit, the device for aiding the ground rolling is configured to: acquire, from the monitoring unit, information the situation of the aircraft and determine predicted positions of the aircraft for a set of future instants, and for each vehicle of a set of other vehicles situated on the surface of the airport: acquire, from the radio communication unit, information regarding the situation of the vehicle, which information is transmitted by this vehicle, determine predicted positions of the vehicle and calculate a distance between the predicted position of the aircraft and the predicted position of the vehicle for each instant of the set of future instants and compare this distance with a predetermined distance threshold and, emit an alert in the cockpit if this distance is less than this distance threshold.
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公开(公告)号：US09994303B2
公开(公告)日：2018-06-12
申请号：US14808453
申请日：2015-07-24
Applicant: Airbus Operations (S.A.S.)
Inventor： Pierre Scacchi , Thierry Bourret , Franck Laine , Matthieu Mayolle , Sabrina Betton , Cécile Puissacq , Olivier Sapin
CPC classification number: B64C13/22 , B64C13/04 , B64C13/042 , B64C13/18 , B64D43/00 , G01C23/005 , G05D1/0061
Abstract: A control system and method for an aircraft configured to operate according to a first mode of operation corresponding to an automatic piloting of the aircraft and a second mode of operation corresponding to a manual piloting of the aircraft, the system including a selection member. The system is configured to operate according to the first mode of operation when the selection member is not actuated continuously and to operate according to the second mode of operation when the selection member is actuated continuously.
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公开(公告)号：US10516472B2
公开(公告)日：2019-12-24
申请号：US15650350
申请日：2017-07-14
Applicant: AIRBUS OPERATIONS (S.A.S.) , AIRBUS (S.A.S.)
Inventor： Pierre Scacchi , Thomas Stanislawiak , Marc Audibert , Raphaël Renier , Pierre Depape , Martial Pohin
Abstract: A device and system for transferring information from an avionics system of an aircraft to an independent computer. The device can be embedded onboard an aircraft for transferring information arising from an avionics system from the aircraft to a computer independent of the avionics system. The device includes at least one radiofrequency receiver configured to receive information which arises from the avionics system and is emitted destined for the ground or another aircraft, at least one transmitter, and a processing unit to command the transmission by the transmitter, to the computer, of at least some of the information received by the radiofrequency receiver.
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公开(公告)号：US10035608B2
公开(公告)日：2018-07-31
申请号：US14973574
申请日：2015-12-17
Applicant: AIRBUS OPERATIONS (S.A.S.)
Inventor： Pierre Scacchi , Matthieu Mayolle
CPC classification number: B64D43/02 , G01C23/005 , G05D1/042 , G05D1/0607 , G05D1/0653 , G05D1/101 , G08G5/0021 , G08G5/003 , G08G5/0047 , G08G5/0065 , G08G5/025
Abstract: A method and device for aiding piloting of an aircraft, during at least one flight phase including piloting steps. The device includes a unit for real-time acquisition of flight parameters of the aircraft, a calculation unit for calculating in real time with the parameters, for each of the piloting steps, a distance between current position of the aircraft and a position along a flight trajectory followed by the aircraft, at which the aircraft will reach the corresponding piloting step. At least one display unit is provided for displaying, in real time, characteristic signs each illustrating one of the piloting steps, the characteristic signs being integrated into the environment viewed with the aid of the screen and being positioned so as to make it possible to locate a place of the environment along the flight trajectory followed by the aircraft, at which the aircraft will reach the piloting step.
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