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    Method and device for monitoring the ability to navigate of an aircraft during a phase of flight close to the ground
    5.
    发明授权
    Method and device for monitoring the ability to navigate of an aircraft during a phase of flight close to the ground 有权
    用于监视在靠近地面的飞行阶段飞机导航能力的方法和装置

    公开(公告)号：US08275495B2

    公开(公告)日：2012-09-25

    申请号：US12575304

    申请日：2009-10-07

    申请人： Fabien Joyeux ,  Adrien Ott ,  Melanie Morel ,  Romain Merat ,  Stephane Dattler ,  Francois Barre ,  Armelle Seillier

    发明人： Fabien Joyeux ,  Adrien Ott ,  Melanie Morel ,  Romain Merat ,  Stephane Dattler ,  Francois Barre ,  Armelle Seillier

    IPC分类号： G01C5/00

    CPC分类号： G05D1/0646 ,  G05D1/0676 ,  G08G5/0021 ,  G08G5/0086

    摘要： Disclosed is a method and device, which provide an enhanced ability to monitor the navigation of an aircraft during a phase of flight in which the aircraft is close to the ground in which the aircraft uses positional information supplied by a satellite positioning system for the navigation. A display screen is used to display a first characteristic sign representing a selected setpoint value for a height parameter of the aircraft. The display screen also displays a second characteristic sign representing a current auxiliary value expressed in the form of an achievable height parameter. An alert is emitted when the second characteristic sign is determined to be within a predetermined height value of the first characteristic sign, and the alert is shown in visual format on the display screen. An alarm is also emitted following a predetermined time after the alert is emitted, if the setpoint value is not replaced by a new setpoint value.

    摘要翻译： 公开了一种方法和装置，其提供了在飞行器靠近地面的飞行阶段期间监视飞行器的导航的增强的能力，其中飞行器使用由卫星定位系统提供的用于导航的位置信息。 显示屏用于显示表示飞机高度参数的选定设定值的第一特征符号。 显示屏幕还显示表示以可实现的高度参数的形式表示的当前辅助值的第二特征符号。 当第二特征符号被确定在第一特征符号的预定高度值内时，发出警报，并且在显示屏幕上以视觉格式示出警报。 在发出警报之后的预定时间后，如果设定点值未被新的设定值更换，则也发出报警。

    Device For Assisting a Vertical Guidance Approach For Aircraft
    6.
    发明申请
    Device For Assisting a Vertical Guidance Approach For Aircraft 审中-公开
    协助飞机垂直引导方法的装置

    公开(公告)号：US20080172149A1

    公开(公告)日：2008-07-17

    申请号：US11994979

    申请日：2006-07-11

    申请人： Patrice Rouquette ,  Adrien Ott ,  Laure Maes ,  Caroline Aucher ,  Melanie Bats ,  Gregory Ortet

    发明人： Patrice Rouquette ,  Adrien Ott ,  Laure Maes ,  Caroline Aucher ,  Melanie Bats ,  Gregory Ortet

    IPC分类号： G05D1/00

    CPC分类号： G05D1/0676 ,  G01C21/00 ,  G01C23/00

    摘要： The invention concerns an approach assisting device (1) comprising a flight management system (2) which determines an approach paths, an inertial reference system (3) which prepares inertial position data, which receives position data of the aircraft, and which determines a hybrid position of said aircraft, a landing assisting multimode receiver (4) which receives data concerning said approach path and said hybrid position, and which deduces therefrom lateral and vertical angular differences, at least when said approach axis is captured, and a guiding system (7) which receives said lateral and vertical angular differences and uses same for guiding the aircraft, at least when said approach path is captured.

    摘要翻译： 本发明涉及一种方法辅助装置（1），其包括确定进场路径的飞行管理系统（2），准备惯性位置数据的惯性参考系统（3），其接收飞机的位置数据，并确定混合 所述飞行器的位置，至少在所述进场轴被捕获时，接收关于所述进场路径和所述混合位置的数据并从其推断横向和垂直角差的着陆辅助多模接收器（4）和引导系统 ），其接收所述横向和垂直角度差异并且用于引导飞行器，至少当所述进场路径被捕获时。

    Piloting assistance system and an aircraft
    7.
    发明授权
    Piloting assistance system and an aircraft 有权
    试点援助系统和飞机

    公开(公告)号：US09244649B2

    公开(公告)日：2016-01-26

    申请号：US13487716

    申请日：2012-06-04

    申请人： Adrien Ott ,  Serge Germanetti ,  Pierre Boudier

    发明人： Adrien Ott ,  Serge Germanetti ,  Pierre Boudier

    IPC分类号： G06F3/147 ,  G01C23/00 ,  G02B27/01 ,  G09G3/00 ,  B64D10/00 ,  H04N13/04

    CPC分类号： G06F3/147 ,  B64D10/00 ,  G01C23/00 ,  G02B27/01 ,  G02B27/017 ,  G02B2027/0138 ,  G02B2027/014 ,  G09G3/003 ,  G09G2380/12 ,  H04N13/344

    摘要： The present invention relates to a piloting assistance system for an aircraft that is provided with a controller for determining piloting information. The system comprises at least one display system wearable on the head of a pilot, the display system being provided with a left display suitable for being viewed by a left eye of the pilot and a right display suitable for being viewed by a right eye of the pilot, the controller including a first processor for processing the information and a second processor for processing the information, the processors including stored instructions for causing the information to be displayed simultaneously and respectively on the left display and on the right display.

    摘要翻译： 本发明涉及一种用于飞行器的驾驶辅助系统，其具有用于确定驾驶信息的控制器。 所述系统包括至少一个可佩戴在飞行员的头部上的显示系统，所述显示系统设置有左显示器，所述左显示器适合于由所述飞行员的左眼观察，右显示器适于被所述右眼显示 所述控制器包括用于处理所述信息的第一处理器和用于处理所述信息的第二处理器，所述处理器包括用于使所述信息同时显示并存储在左显示器和右显示器上的存储指令。

    PILOTING ASSISTANCE SYSTEM AND AN AIRCRAFT
    9.
    发明申请
    PILOTING ASSISTANCE SYSTEM AND AN AIRCRAFT 有权
    飞机辅助系统和飞机

    公开(公告)号：US20120314034A1

    公开(公告)日：2012-12-13

    申请号：US13487716

    申请日：2012-06-04

    申请人： Adrien Ott ,  Serge Germanetti ,  Pierre Boudier

    发明人： Adrien Ott ,  Serge Germanetti ,  Pierre Boudier

    IPC分类号： G01C21/00 ,  H04N13/04

    CPC分类号： G06F3/147 ,  B64D10/00 ,  G01C23/00 ,  G02B27/01 ,  G02B27/017 ,  G02B2027/0138 ,  G02B2027/014 ,  G09G3/003 ,  G09G2380/12 ,  H04N13/344

    摘要： The present invention relates to a piloting assistance system (10) for an aircraft (1) that is provided with determination means (20) for determining piloting information. The system comprises at least one display system (40) wearable on the head of a pilot, the display system (40) being provided with left display means (41) suitable for being viewed by a left eye of said pilot and right display means (42) suitable for being viewed by a right eye of said pilot, said determination means (20) including first processor means (21) for processing said information and second processor means (22) for processing said information, the processor means including stored instructions for causing said information to be displayed simultaneously and respectively on the left display means (41) and on the right display means (42).

    摘要翻译： 本发明涉及一种用于飞行器（1）的驾驶辅助系统（10），其具有用于确定驾驶信息的确定装置（20）。 所述系统包括至少一个可佩戴在飞行员的头部上的显示系统（40），所述显示系统（40）设有左显示装置（41），所述左显示装置适于由所述飞行员和右显示装置的左眼观察 42），所述确定装置（20）包括用于处理所述信息的第一处理器装置（21）和用于处理所述信息的第二处理器装置（22），所述处理器装置包括存储的指令 使所述信息同时显示在左显示装置（41）和右显示装置（42）上。