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1. 发明授权

US07690603B2 Method and device to assist in the piloting of an aircraft in a non-precision approach during a landing phase 有权
标题翻译：在着陆阶段协助以非精密方式驾驶飞机的方法和装置
公开(公告)号：US07690603B2
公开(公告)日：2010-04-06
申请号：US10781910
申请日：2004-02-20
申请人： Eric Peyrucain , Patrice Rouquette , Christophe Jourdan
发明人： Eric Peyrucain , Patrice Rouquette , Christophe Jourdan
IPC分类号： G01C21/00
CPC分类号： G01C21/165 , G01S19/48 , G05D1/0676 , G08G5/0021
摘要： A method to assist the piloting of an aircraft in a non-precision approach during a landing phase may include a series of successive steps that are carried out interactively and automatically. The steps include verifying, in accordance with respective standards of operation, conditions relating to the correct functioning of a plurality of equipment of the aircraft and to the integrity and precision of measurements of parameters used for implementing the non-precision approach, based on information from the plurality of equipment. On the basis of the verified conditions, an appropriate approach category is selected and presented on a display screen.
摘要翻译：在着陆阶段期间协助以非精密方式驾驶飞机的方法可包括以交互方式和自动地执行的一系列连续步骤。这些步骤包括根据相应的操作标准，根据相关的操作标准，根据来自于飞行器的多个设备的正确功能以及用于实施非精密方法的参数的测量的完整性和精度，多个设备。在验证条件的基础上，选择适当的方法类别并将其显示在显示屏幕上。

2. 发明授权

US07038613B1 Method and device for determining at least one cue of vertical position of an aircraft 有权
标题翻译：用于确定飞行器的垂直位置的至少一个提示的方法和装置
公开(公告)号：US07038613B1
公开(公告)日：2006-05-02
申请号：US10803091
申请日：2004-03-18
申请人： Patrice Rouquette , Eric Peyrucain , Jacques Rosay
发明人： Patrice Rouquette , Eric Peyrucain , Jacques Rosay
IPC分类号： G01S13/91
CPC分类号： G05D1/0676 , B64D45/04 , G01S1/045 , G01S1/14
摘要： A method and device for determining a vertical position cue of an aircraft while landing in the presence of a lateral alignment beam, which is emitted from the ground and provides an indication of the aircraft's lateral alignment with respect to a landing strip, may include detecting the lateral alignment beam with aircraft equipment. On the basis of cues relating to the detected lateral alignment beam and of predetermined cues, an axis of approach of the aircraft is determined. Additionally, the actual position and a preset position of the aircraft, which corresponds to the position the aircraft would have if it were on the approach axis, are determined. On the basis of the actual and preset positions of the aircraft, the vertical deviation of the aircraft, representing the vertical position cue, is computed.
摘要翻译：一种用于在存在从地面发射并提供飞机相对于着陆带的横向对准的指示的横向对准梁存在的情况下确定飞行器的垂直位置提示的方法和装置可以包括检测横向对准梁与飞机设备。基于与所检测到的横向对准梁和预定线索相关的线索，确定飞机的接近轴线。此外，飞机的实际位置和预设位置对应于飞机在接近轴上将具有的位置。根据飞机的实际和预置位置，计算代表垂直位置提示的飞行器的垂直偏差。

3. 发明申请

US20060109167A1 METHOD AND DEVICE FOR DETERMINING AT LEAST ONE CUE OF VERTICAL POSITION OF AN AIRCRAFT 有权
标题翻译：用于确定航空器垂直位置的最小一个方法和装置
公开(公告)号：US20060109167A1
公开(公告)日：2006-05-25
申请号：US10803091
申请日：2004-03-18
申请人： Patrice Rouquette , Eric Peyrucain , Jacques Rosay
发明人： Patrice Rouquette , Eric Peyrucain , Jacques Rosay
IPC分类号： G01S13/91
CPC分类号： G05D1/0676 , B64D45/04 , G01S1/045 , G01S1/14
摘要： A method and device for determining a vertical position cue of an aircraft while landing in the presence of a lateral alignment beam, which is emitted from the ground and provides an indication of the aircraft's lateral alignment with respect to a landing strip, may include detecting the lateral alignment beam with aircraft equipment. On the basis of cues relating to the detected lateral alignment beam and of predetermined cues, an axis of approach of the aircraft is determined. Additionally, the actual position and a preset position of the aircraft, which corresponds to the position the aircraft would have if it were on the approach axis, are determined. On the basis of the actual and preset positions of the aircraft, the vertical deviation of the aircraft, representing the vertical position cue, is computed.
摘要翻译：一种用于在存在从地面发射并且提供飞机相对于着陆带的横向对准的指示的横向对准梁的存在下确定飞行器的垂直位置提示的方法和装置可以包括检测横向对准梁与飞机设备。基于与检测到的横向对准梁和预定线索有关的线索，确定飞行器的接近轴线。此外，飞机的实际位置和预设位置对应于飞机在接近轴上将具有的位置。根据飞机的实际和预置位置，计算代表垂直位置提示的飞行器的垂直偏差。

4. 发明申请

US20090043433A1 AIRCRAFT GUIDANCE SYSTEM 有权
标题翻译：飞机指导系统
公开(公告)号：US20090043433A1
公开(公告)日：2009-02-12
申请号：US12280126
申请日：2007-03-26
申请人： Vincent Markiton , Eric Peyrucain , Lionel Bertin , Jean-Louis De Menorval
发明人： Vincent Markiton , Eric Peyrucain , Lionel Bertin , Jean-Louis De Menorval
IPC分类号： G01C23/00 , B64D45/04
CPC分类号： G01C23/005
摘要： The guidance system (1) comprises means (2, 6) for generating an alphanumeric identification characteristic, making it possible to identify a data item which must be used for a selected guidance mode of the aircraft, and display means (10) which automatically shows this alphanumeric identification characteristic on a display screen (12).
摘要翻译：引导系统（1）包括用于产生字母数字识别特征的装置（2,6），使得可以识别必须用于飞行器的选定引导模式的数据项目，以及自动显示的显示装置（10）这种字母数字识别特征在显示屏幕（12）上。

5. 发明授权

US5957412A Method and device for vertical guidance of an aircraft 失效
标题翻译：飞机垂直引导的方法和装置
公开(公告)号：US5957412A
公开(公告)日：1999-09-28
申请号：US936549
申请日：1997-09-24
申请人： Yves Saint Upery , Eric Peyrucain
发明人： Yves Saint Upery , Eric Peyrucain
IPC分类号： G05D1/06 , G05D1/08
CPC分类号： G05D1/0607
摘要： The present invention relates to a method and a device for guiding an aircraft (A) according to a prescribed vertical flight path (T).According to the invention:the vertical distance he between said aircraft (A) and said flight path (T) is determined;the difference ve between the actual vertical velocity (Vz) of the aircraft (A) and the vertical velocity (Vzth) which it would have on the flight path (T) is determined;a vertical acceleration variation Anz is calculated:.DELTA.nz=((k1.(he-hc))+(ve-vc)).k2k1 and k2 being characteristic coefficients, hc and vc being precontrol terms, and k1.(he-hc) being restricted; andsaid restricted variation Anz is applied to the aircraft.
摘要翻译：本发明涉及一种根据规定的垂直飞行路径（T）引导飞行器（A）的方法和装置。根据本发明，确定所述飞机（A）和所述飞行路径（T）之间的垂直距离; 确定飞行器（A）的实际垂直速度（Vz）与飞行路径（T）上将具有的垂直速度（Vzth）之间的差值ve; 计算垂直加速度变化Anz：DELTA nz =（（k1。（he-hc））+（ve-vc）），k2k1和k2是特征系数，hc和vc是预控项，k1（he-hc ）受到限制并且将限制变化Anz应用于飞行器。

6. 发明授权

US08050860B2 Method and device for displaying a flight plan of an aircraft 有权
标题翻译：显示飞机飞行计划的方法和装置
公开(公告)号：US08050860B2
公开(公告)日：2011-11-01
申请号：US11828896
申请日：2007-07-26
申请人： Eric Peyrucain , Philippe Haas , Véronique Roan , Gautier Taravella
发明人： Eric Peyrucain , Philippe Haas , Véronique Roan , Gautier Taravella
IPC分类号： G01C21/00
CPC分类号： G08G5/0034 , G01C23/00 , G08G5/0021 , G09B29/007
摘要： The invention relates to a method and device for displaying a flight plan of an aircraft. The display device includes a display presenting unit making it possible to identify the flight phase of each waypoint of a flight plan which is displayed on a screen, and an activation unit making it possible to directly access a corresponding flight phase page.
摘要翻译：本发明涉及一种显示飞机飞行计划的方法和装置。显示装置包括显示提示单元，使得可以识别显示在屏幕上的飞行计划的每个航点的飞行阶段，以及激活单元，使得可以直接访问相应的飞行相位页面。

7. 发明授权

US07715955B2 Aircraft piloting system, at least for piloting the aircraft during a non precision approach with a view to a landing 有权
标题翻译：飞机驾驶系统，至少在不精确的方法中驾驶飞机，以便着陆
公开(公告)号：US07715955B2
公开(公告)日：2010-05-11
申请号：US10803184
申请日：2004-03-18
申请人： Gilles Tatham , Eric Peyrucain
发明人： Gilles Tatham , Eric Peyrucain
IPC分类号： B64G1/36
CPC分类号： G05D1/0676
摘要： An aircraft piloting system may include information sources that provide a position indication relating to the aircraft and information that characterizes a virtual approach axis. An information processing unit processes information emanating from the information sources and includes an assisted approach mode function and a landing aid multimode receiver that implements a precision approach. A user device uses the information provided by the landing aid multimode receiver to support the guidance of the aircraft up to its landing.
摘要翻译：飞机驾驶系统可以包括提供与飞机有关的位置指示的信息源和表征虚拟进近轴的信息。信息处理单元处理从信息源发出的信息，并且包括辅助进场模式功能和实现精确方法的着陆援助多模接收机。用户设备使用着陆援助多模接收机提供的信息来支持飞机直到其着陆的引导。

8. 发明授权

US5925079A Process and device for guiding a mobile craft 失效
标题翻译：引导手机的过程和装置
公开(公告)号：US5925079A
公开(公告)日：1999-07-20
申请号：US681977
申请日：1996-07-30
申请人： Eric Peyrucain , Yves Saint Upery
发明人： Eric Peyrucain , Yves Saint Upery
IPC分类号： G05D1/02 , G01C21/00 , B64C19/00
CPC分类号： G05D1/0202
摘要： A mobile craft is guided with respect to a trajectory. To guide the craft, the distance xtk is determined between the mobile craft and the point of orthogonal projection of the mobile craft on a segment of the trajectory. The angle tkae is determined between the direction of travel of the mobile craft and the direction at the point of orthogonal projection. A control value is computed for the lateral attitude from the distance and angle, two characteristic coefficients and a nominal control value. This control value is applied to the craft.
摘要翻译：移动工艺相对于轨迹被引导。为了引导工艺，在移动工艺和移动工艺在轨迹的一段上的正交投影点之间确定距离xtk。角度tkae在移动飞行器的行进方向和正交投影点的方向之间确定。从距离和角度计算横向姿态的控制值，两个特征系数和标称控制值。该控制值适用于工艺。

9. 发明授权

US08219307B2 Aircraft navigation aid device 有权
标题翻译：飞机导航辅助装置
公开(公告)号：US08219307B2
公开(公告)日：2012-07-10
申请号：US12595891
申请日：2008-04-07
申请人： Laurent Valex , André Bourdais , Thomas Sauvalle , Eric Peyrucain
发明人： Laurent Valex , André Bourdais , Thomas Sauvalle , Eric Peyrucain
IPC分类号： G06F19/00
CPC分类号： G08G5/065 , G08G5/0021
摘要： An aircraft navigation aid device includes at least one flight management system, an airport navigation aid unit which is incorporated in this flight management system, and a common interface unit.
摘要翻译：飞机导航辅助装置包括至少一个飞行管理系统，并入飞行管理系统的机场导航辅助单元和公共接口单元。

10. 发明授权

US07899586B2 Aircraft guidance system 有权
标题翻译：飞机引导系统
公开(公告)号：US07899586B2
公开(公告)日：2011-03-01
申请号：US12280126
申请日：2007-03-26
申请人： Vincent Markiton , Eric Peyrucain , Lionel Bertin , Jean-Louis De Menorval
发明人： Vincent Markiton , Eric Peyrucain , Lionel Bertin , Jean-Louis De Menorval
IPC分类号： G06G7/70 , G06G7/76 , G01S13/00 , H04N7/00 , G01C23/00
CPC分类号： G01C23/005
摘要： A guidance system includes a device to generate an alphanumeric identification characteristic, enabling identification of a data item which is used for a selected guidance mode of an aircraft. The system also includes a display unit which automatically shows the alphanumeric identification characteristic on a display screen.
摘要翻译：引导系统包括用于产生字母数字识别特征的装置，使得能够识别用于飞行器的选定引导模式的数据项。该系统还包括显示单元，其在显示屏幕上自动显示字母数字识别特性。

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