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    METHOD FOR MONITORING THE INTEGRITY OF AN AIRCRAFT POSITION COMPUTED ON BOARD
    1.
    发明申请
    METHOD FOR MONITORING THE INTEGRITY OF AN AIRCRAFT POSITION COMPUTED ON BOARD 有权
    监控船上计算机飞行员位置的完整性的方法

    公开(公告)号：US20080046141A1

    公开(公告)日：2008-02-21

    申请号：US11841061

    申请日：2007-08-20

    申请人： Stephane Dattler ,  Vincent Markiton

    发明人： Stephane Dattler ,  Vincent Markiton

    IPC分类号： G01M17/00 ,  G01C21/00

    CPC分类号： G01C21/20 ,  G01C21/165

    摘要： A method for monitoring the integrity of an aircraft position computed on board including on-board means for monitoring the aircraft position that are able to detect common-mode failures. Dissimilar computing channels of the aircraft position are utilized, the dissimilar channels being on-board in the aircraft. Each aircraft position primary computing channel is supplemented by a dissimilar computing channel, which allows the coherence of the primary aircraft position, the position computed by the primary computing channels, to be verified. Mechanisms for verifying the reliability of the results from dissimilar computing channels are implemented to limit a loss of performance from the utilization of dissimilar computing channels, which are less performing than primary computing channels.

    摘要翻译： 一种用于监测在船上计算的飞行器位置的完整性的方法，包括用于监视能够检测共模故障的飞行器位置的机载装置。 使用飞机位置的不相似的计算通道，飞机中不同的通道在板上。 每个飞机位置主计算通道由不同的计算通道补充，允许主飞机位置的相干性，由主计算通道计算的位置被验证。 用于验证来自不同计算通道的结果的可靠性的机制被实现以限制来自使用不同于主计算通道的不同计算通道的不同计算通道的性能损失。

    METHOD AND DEVICE FOR DETERMINING A DECISION HEIGHT DURING AN AUTONOMOUS APPROACH OF AN AIRCRAFT
    2.
    发明申请
    METHOD AND DEVICE FOR DETERMINING A DECISION HEIGHT DURING AN AUTONOMOUS APPROACH OF AN AIRCRAFT 有权
    用于确定飞机自动方法中的决定高度的方法和装置

    公开(公告)号：US20080150785A1

    公开(公告)日：2008-06-26

    申请号：US11831671

    申请日：2007-07-31

    申请人： Vincent Markiton ,  Stephane Dattler

    发明人： Vincent Markiton ,  Stephane Dattler

    IPC分类号： G01S13/00

    CPC分类号： G05D1/0676

    摘要： The subject of the invention is a method of aiding the piloting of an aircraft (3), which is intended to aid the piloting of the aircraft during an autonomous approach to a landing runway (P) for the purpose of landing, said aircraft comprising at least one locating means (10, 12), wherein: a) an estimated instant of arrival of the aircraft on the runway is determined; b) a prediction of the performance of said locating means of the aircraft at least at this instant of arrival is determined; and c) on the basis of said performance of the locating means and of characteristics of said approach, at least one minimum decision height (Hmin) corresponding to this instant of arrival is determined, above which the aircraft is protected from the risks of collision with the environment when it is guided automatically onto an approach axis (A) corresponding to said approach. The invention also relates to a device for implementing this method.

    摘要翻译： 本发明的主题是帮助飞行员（3）的驾驶的方法，其旨在在为了着陆的目的在对着陆跑道（P）的自主进场期间有助于飞行员的驾驶，所述飞行器包括在 至少一个定位装置（10,12），其中：a）确定所述飞机在跑道上的估计时刻; b）至少在该到达时刻确定飞机的所述定位装置的性能的预测; 和c）基于所述定位装置的所述性能和所述方法的特征，确定对应于该到达时刻的至少一个最小决定高度（Hmin），在此之上，保护飞机免受与 当它被自动引导到对应于所述方法的接近轴线（A）时的环境。 本发明还涉及一种用于实现该方法的装置。

    Aircraft standby display device
    3.
    发明授权
    Aircraft standby display device 有权
    飞机待机显示装置

    公开(公告)号：US07764198B2

    公开(公告)日：2010-07-27

    申请号：US11573437

    申请日：2005-07-27

    申请人： Didier Brehin ,  Stephane Dattler

    发明人： Didier Brehin ,  Stephane Dattler

    IPC分类号： G01C23/00 ,  G01C21/00 ,  G08B21/00

    CPC分类号： G01C23/00

    摘要： An aircraft standby display device includes a set of data sources, a data processing unit, and a display. The display presents altitude control indicators representing speed, altitude, attitude, and a heading scale that includes a characteristic symbol indicating a next route point of an aircraft flight plan. The heading scale is independent of the altitude control indicators. The display also presents a quantitative value that: (1) indicates the remaining distance of flight of the aircraft to reach the next route point and (2) is associated with the characteristic symbol.

    摘要翻译： 飞机待机显示装置包括一组数据源，数据处理单元和显示器。 显示器显示代表速度，高度，姿态和标题的高度控制指示器，其包括指示飞行器飞行计划的下一个路线点的特征符号。 航向规模与高度控制指标无关。 显示还提供了一个定量值：（1）表示飞机到达下一个路线点的剩余飞行距离，（2）与特征符号相关联。

    AIRCRAFT STANDBY DISPLAY DEVICE
    5.
    发明申请
    AIRCRAFT STANDBY DISPLAY DEVICE 有权
    飞机待机显示设备

    公开(公告)号：US20090224945A1

    公开(公告)日：2009-09-10

    申请号：US11573437

    申请日：2005-07-27

    申请人： Didier Brehin ,  Stephane Dattler

    发明人： Didier Brehin ,  Stephane Dattler

    IPC分类号： G01C23/00 ,  G01C21/00

    CPC分类号： G01C23/00

    摘要： The invention concerns a device comprising a set of data sources, a data processing unit, and a display which presents on a display unit (8) altitude control indicators (9, 10, 11) representing at least speed, altitude and altitude data of the aircraft and a heading scale (12) including a characteristic symbol (13) indicating at least one next route point of the aircraft flight plan, said heading scale (12) being independent of said altitude control indicators (9, 10, 11), as well as a quantitative value (14) which indicates the remaining distance of flight of the aircraft to reach said next route point and which is associated with said characteristic symbol (13).

    摘要翻译： 本发明涉及一种包括一组数据源，数据处理单元和在显示单元（8）上呈现高度控制指示器（9,10,11）的设备的装置，所述高度控制指示器（9,10,11）至少代表了所述高度控制指示器 飞行器和标题（12），其包括表示飞行器飞行计划的至少一个下一个路线点的特征符号（13），所述航向比例（12）独立于所述高度控制指示器（9,10,11），如 以及指示飞机到达所述下一路线点的剩余飞行距离并与所述特征符号（13）相关联的定量值（14）。

    METHOD AND DEVICE FOR AIDING THE NAVIGATION OF AN AIRCRAFT FLYING AT A LOW ALTITUDE
    7.
    发明申请
    METHOD AND DEVICE FOR AIDING THE NAVIGATION OF AN AIRCRAFT FLYING AT A LOW ALTITUDE 有权
    用于援助低空飞行员飞行航行的方法和装置

    公开(公告)号：US20110066370A1

    公开(公告)日：2011-03-17

    申请号：US12882848

    申请日：2010-09-15

    申请人： Stephane Dattler

    发明人： Stephane Dattler

    IPC分类号： G01C21/00

    CPC分类号： G01S19/15 ,  G01S19/20

    摘要： A method and device for aiding the navigation of an aircraft flying at low altitude as described. The device (1) includes positioning means (2) generating the current position of the aircraft, and calculation means (4) for detecting when the budgets allocated to a position error of the aircraft are exceeded by protection ranges.

    摘要翻译： 一种用于帮助飞行器在低空飞行的导航的方法和装置，如所述。 装置（1）包括产生飞行器当前位置的定位装置（2）和用于检测分配给飞机位置误差的预算何时超过保护范围的计算装置（4）。

    Method and device for updating the position of an aircraft
    9.
    发明授权
    Method and device for updating the position of an aircraft 有权
    用于更新飞机位置的方法和装置

    公开(公告)号：US08755995B2

    公开(公告)日：2014-06-17

    申请号：US12254457

    申请日：2008-10-20

    申请人： Philippe Haas ,  Stephane Dattler ,  Julien Nico

    发明人： Philippe Haas ,  Stephane Dattler ,  Julien Nico

    IPC分类号： G01C21/00

    CPC分类号： G01C21/165 ,  G01C25/005 ,  G01S13/86 ,  G01S19/48

    摘要： The device (1) comprises a first system (3) which comprises means (14) for calculating the vector difference between a position generated by this first system (3) and a realignment position received from a second system (4), for one and the same date-stamping, and means (16) for adding this difference to any new position of the aircraft, generated by said first system (3), so as to obtain each time a realigned position.

    摘要翻译： 设备（1）包括第一系统（3），其包括用于计算由第一系统（3）产生的位置与从第二系统（4）接收的重新排列位置之间的向量差的装置（14） 相同的日期戳，以及用于将所述差异加到由所述第一系统（3）生成的飞行器的任何新位置的装置（16），以便每次获得重新排列的位置。

    Method and device for monitoring the ability to navigate of an aircraft during a phase of flight close to the ground
    10.
    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。