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公开(公告)号：US20190197906A1
公开(公告)日：2019-06-27
申请号：US16209201
申请日：2018-12-04
Applicant: Airbus Operations S.A.S.
Inventor： Thierry Bourret , Matthieu Barba , Maxime Semat , Florent Lanterna , Didier Sauve
CPC classification number: G08G5/0047 , G01C23/005 , G05D1/0077 , G05D1/101 , G08G5/0013 , G08G5/0073 , G08G5/025
Abstract: A piloting aid system for ensuring the availability an automatic pilot corresponding to an automatic piloting system and/or a flight director and/or a thrust regulation device to be controlled as a function of a speed information item determined from a source of information, and configured to operate according to a first current guidance mode and an approach capability that are part of a first set of guidance modes and approach capabilities. The system includes a surveillance module to be able to detect the loss of sources of information, a module for determining a second set of guidance modes and of approach capabilities as a function of the source or sources of information whose loss was detected by the surveillance module, a module for use, by the automatic pilot and/or the thrust regulation device, of a second current guidance mode and an approach capability that are part of the second set.
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2.发明授权Method and device for vertically guiding an aircraft during an approach of a runway along a lateral approach trajectory 有权在沿着横向进近轨迹的跑道接近期间垂直引导飞行器的方法和装置公开(公告)号：US09561868B2
公开(公告)日：2017-02-07
申请号：US14586433
申请日：2014-12-30
Applicant: Airbus Operations (S.A.S.)
Inventor： Thierry Bourret , Kenji Ahualle Horimoto
CPC classification number: B64D45/04 , B64C13/18 , G01C23/005 , G05D1/042 , G05D1/0676
Abstract: A method and device including a unit to extract a linear terrain profile stored in memory, a terrain height for a current distance of the aircraft, a unit for determining a current height of the aircraft with respect to the terrain, using at least one measurement taken by a radar altimeter, a unit for computing a first current altitude of the aircraft, using the terrain height and the current height, a unit for computing a second current altitude of the aircraft, corresponding to an altitude on an approach profile of the current position of the aircraft and a unit for computing the difference between the first and second current altitudes, the difference being transmitted to a guidance unit to vertically guide the aircraft.
Abstract translation: 一种包括提取存储在存储器中的线性地形剖面的单元的方法和装置，飞行器当前距离的地形高度，用于使用至少一次测量来确定飞机相对于地形的当前高度的单元 通过雷达高度计，用于使用地形高度和当前高度来计算飞行器的第一当前高度的单元，用于计算飞行器的第二当前高度的单元，其对应于当前位置的接近轮廓上的高度 并且用于计算第一和第二当前高度之间的差异的单元，差异被传送到引导单元以垂直地引导飞行器。
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3.发明申请METHOD AND DEVICE FOR VERTICALLY GUIDING AN AIRCRAFT DURING AN APPROACH OF A RUNWAY ALONG A LATERAL APPROACH TRAJECTORY 有权方法和装置，用于在横向方向轨迹中的方法中垂直地指导飞机公开(公告)号：US20150203214A1
公开(公告)日：2015-07-23
申请号：US14586433
申请日：2014-12-30
Applicant: Airbus Operations (S.A.S.)
Inventor： Thierry Bourret , Kenji AHUALLE HORIMOTO
CPC classification number: B64D45/04 , B64C13/18 , G01C23/005 , G05D1/042 , G05D1/0676
Abstract: A method and device including a unit to extract a linear terrain profile stored in memory, a terrain height for a current distance of the aircraft, a unit for determining a current height of the aircraft with respect to the terrain, using at least one measurement taken by a radar altimeter, a unit for computing a first current altitude of the aircraft, using the terrain height and the current height, a unit for computing a second current altitude of the aircraft, corresponding to an altitude on an approach profile of the current position of the aircraft and a unit for computing the difference between the first and second current altitudes, the difference being transmitted to a guidance unit to vertically guide the aircraft.
Abstract translation: 一种包括提取存储在存储器中的线性地形剖面的单元的方法和装置，飞行器当前距离的地形高度，用于使用至少一次测量来确定飞机相对于地形的当前高度的单元 通过雷达高度计，用于使用地形高度和当前高度来计算飞行器的第一当前高度的单元，用于计算飞行器的第二当前高度的单元，其对应于当前位置的接近轮廓上的高度 并且用于计算第一和第二当前高度之间的差异的单元，差异被传送到引导单元以垂直地引导飞行器。
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Patent Agency Ranking
4.发明授权Method and device for determining a linear terrain profile along a lateral approach trajectory of an airport 有权用于沿着机场的侧向进近轨迹确定线性地形剖面的方法和装置公开(公告)号：US09342988B2
公开(公告)日：2016-05-17
申请号：US14586461
申请日：2014-12-30
Applicant: Airbus Operations (S.A.S.)
Inventor： Thierry Bourret , Kenji Ahualle Horimoto
IPC: G05D1/00 , G05D1/08 , G05D3/00 , G06F7/00 , G06F17/00 , G08G5/00 , G01S13/88 , G01C5/00 , G01C5/06 , G01C23/00
CPC classification number: G08G5/0086 , G01C5/005 , G01C5/06 , G01C23/00 , G01S13/882
Abstract: A device comprising a computation unit for computing, for each of a plurality of different distances relative to a threshold of a landing runway along a lateral approach trajectory, a geometric altitude, using a measured and stored barometric altitude, a computation unit for computing a terrain height, by subtracting, from the computed geometric altitude, a measured and stored height, and a computation unit for determining a terrain profile from the set of terrain heights computed for the set of different distances.
Abstract translation: 一种装置，包括计算单元，用于针对沿着侧向进近轨迹的着陆跑道的阈值的多个不同距离中的每一个计算单元，使用测量和存储的气压高度计算几何高度，用于计算地形的计算单元 高度，通过从所计算的几何高度中减去测量和存储的高度，以及计算单元，用于根据针对该组不同距离计算的地形高度集合来确定地形剖面。
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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：US09904291B2
公开(公告)日：2018-02-27
申请号：US15157176
申请日：2016-05-17
Applicant: AIRBUS OPERATIONS (S.A.S.)
Inventor： Florent Lanterna , Thierry Bourret , Jean Muller
CPC classification number: G05D1/042 , B64C13/18 , B64C19/00 , G05D1/0055 , G05D1/0088 , G05D1/0607 , G08G5/04 , G08G5/045
Abstract: A method and a system for controlling an emergency descent of an aircraft. The system (1) includes a unit (2) for detecting an emergency situation, a unit (11) for calculating a usual emergency descent command, a unit (12) for calculating a limited emergency descent command, a selection unit (14) configured for selecting the usual emergency descent command or, if application conditions are met and if the limited descent command is less than said usual emergency descent command and greater than a regulation emergency descent command, selecting the limited emergency descent command, and a unit (4) for application, to the aircraft, of the selected emergency descent command.
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公开(公告)号：US20160185448A1
公开(公告)日：2016-06-30
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.
Abstract translation: 一种用于飞行器的控制系统和方法，其被配置为根据对应于飞行器的自动驾驶的第一操作模式进行操作，以及对应于飞行器的手动驾驶的第二操作模式，所述系统包括选择构件。 当选择构件被连续致动时，该系统构造成在选择构件不连续致动时根据第一操作模式操作并根据第二操作模式进行操作。
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8.发明申请METHOD AND DEVICE FOR DETERMINING A LINEAR TERRAIN PROFILE ALONG A LATERAL APPROACH TRAJECTORY OF AN AIRPORT 有权用于确定机场的侧向方向线性线性轮廓的方法和装置公开(公告)号：US20150317905A1
公开(公告)日：2015-11-05
申请号：US14586461
申请日：2014-12-30
Applicant: Airbus Operations (S.A.S.)
Inventor： Thierry Bourret , Kenji AHUALLE HORIMOTO
CPC classification number: G08G5/0086 , G01C5/005 , G01C5/06 , G01C23/00 , G01S13/882
Abstract: A device comprising a computation unit for computing, for each of a plurality of different distances relative to a threshold of a landing runway along a lateral approach trajectory, a geometric altitude, using a measured and stored barometric altitude, a computation unit for computing a terrain height, by subtracting, from the computed geometric altitude, a measured and stored height, and a computation unit for determining a terrain profile from the set of terrain heights computed for the set of different distances.
Abstract translation: 一种装置，包括计算单元，用于针对沿着侧向进近轨迹的着陆跑道的阈值的多个不同距离中的每一个计算单元，使用测量和存储的气压高度计算几何高度，用于计算地形的计算单元 高度，通过从所计算的几何高度中减去测量和存储的高度，以及计算单元，用于根据针对该组不同距离计算的地形高度集合来确定地形剖面。
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