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公开(公告)号：US09939818B2
公开(公告)日：2018-04-10
申请号：US14808646
申请日：2015-07-24
Applicant: Airbus Operations (S.A.S.)
Inventor： Josep Boada-Bauxell , Victor Gibert , Laurent Burlion , Abdelhamid Chriette , Franck Plestan
CPC classification number: G05D1/0676 , G06K9/52 , G06T7/60 , G06T7/73 , H04N7/18
Abstract: A system for automatic landing of an aircraft on a runway, including an onboard image capture system, image analyzer for detecting in an image a landing runway and determining characteristics of a segment connecting a planned point of impact on the runway and a vanishing point of the image, a measurement module for measuring observables in an inertial frame tied to the runway, on the basis of characteristics of the segment, the observables including a first observable, a second observable, and a third observable, an estimator for estimating longitudinal, lateral and vertical position deviations of aircraft position relative to point of impact from measurements of the first, second and third observables, and guidance for determining aircraft guidance orders from the longitudinal, lateral and vertical deviations and of the relative heading angle.
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2.发明申请公开(公告)号：US20140039731A1
公开(公告)日：2014-02-06
申请号：US13956872
申请日：2013-08-01
Applicant: AIRBUS OPERATIONS (S.A.S.)
Inventor： Charles Renault Leberquer , Florian Constans , Josep Boada-Bauxell , Pascale Louise
IPC: B64C19/00
CPC classification number: B64C19/00 , G01C23/00 , G05D1/042 , G05D1/0607
Abstract: 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.
Abstract translation: 该装置包括伺服控制装置，其以组合的方式自动控制飞行器的自动推力系统和飞行器的空气制动器，作为用于转向垂直轨迹的通常装置的补充，使得飞行器达到速度设定点和/或 高度设定点，在由地理约束定义的位置。
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Patent Agency Ranking
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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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：US10597168B2
公开(公告)日：2020-03-24
申请号：US15786741
申请日：2017-10-18
Applicant: Airbus Operations S.A.S.
Inventor： Josep Boada-Bauxell , Fabrice Bousquet
Abstract: The device for assisting the landing of an aircraft in a phase of descent for the purpose of a landing on a runway with the help of an instrument landing assistance module includes an image capturing module for capturing a sequence of successive images of the ground, an image processing module, a monitoring module for detecting on the processed images at least one visual characteristic corresponding to a runway, a computation module for computing a current position of the aircraft and a comparison module for comparing the computed current position with a signal representative of a current position of the instrument landing assistance module, a go-around warning being transmitted to a display unit, if the current positions are not substantially identical.
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公开(公告)号：US20180118372A1
公开(公告)日：2018-05-03
申请号：US15786741
申请日：2017-10-18
Applicant: Airbus Operations S.A.S.
Inventor： Josep Boada-Bauxell , Fabrice Bousquet
Abstract: The device for assisting the landing of an aircraft in a phase of descent for the purpose of a landing on a runway with the help of an instrument landing assistance module includes an image capturing module for capturing a sequence of successive images of the ground, an image processing module, a monitoring module for detecting on the processed images at least one visual characteristic corresponding to a runway, a computation module for computing a current position of the aircraft and a comparison module for comparing the computed current position with a signal representative of a current position of the instrument landing assistance module, a go-around warning being transmitted to a display unit, if the current positions are not substantially identical.
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公开(公告)号：US08880245B2
公开(公告)日：2014-11-04
申请号：US13956872
申请日：2013-08-01
Applicant: Airbus Operations (S.A.S.)
Inventor： Charles Renault Leberquer , Florian Constans , Josep Boada-Bauxell , Pascale Louise
CPC classification number: B64C19/00 , G01C23/00 , G05D1/042 , G05D1/0607
Abstract: 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.
Abstract translation: 该装置包括伺服控制装置，其以组合的方式自动控制飞行器的自动推力系统和飞行器的空气制动器，作为用于转向垂直轨迹的通常装置的补充，使得飞行器达到速度设定点和/或 高度设定点，在由地理约束定义的位置。
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