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    AUTOPILOT SYSTEM FOR AN AIRCRAFT AND RELATED PROCESS
    1.
    发明申请
    AUTOPILOT SYSTEM FOR AN AIRCRAFT AND RELATED PROCESS 审中-公开
    用于飞机和相关过程的自动驾驶系统

    公开(公告)号：US20170008613A1

    公开(公告)日：2017-01-12

    申请号：US15203605

    申请日：2016-07-06

    Applicant: DASSAULT AVIATION

    Inventor： Arnaud TURPIN ,  Nicolas LE CORRE

    IPC: B64C13/18 ,  G05D1/04 ,  G05D1/08 ,  G05D1/00

    CPC classification number: B64C13/18 ,  G05D1/0061 ,  G05D1/042 ,  G05D1/0808 ,  G05D1/0833

    Abstract: An autopilot system for an aircraft and related process are provided. The system includes a first load factor command definition and application module; a second roll command definition and application module; a control module of the first definition and application module and the second definition and application module, able to define parameters of a recovery maneuver seeking to return the aircraft to setpoint attitudes at the end of a maneuver from initial attitudes. The control module includes a submodule for computing at least one pair of authorities respectively applied by the first module and by the second module during the recovery maneuver. The authorities are computed as a function of at least a current movement parameter of the aircraft and a safety parameter.

    Abstract translation: 提供了一种用于飞机和相关过程的自动驾驶仪系统。 该系统包括第一负载因子命令定义和应用模块; 第二卷命令定义和应用模块; 第一定义和应用模块和第二定义和应用模块的控制模块，其能够定义在初始态度的操纵结束时寻求将飞机返回到设定点态度的恢复机动的参数。 控制模块包括用于在恢复操作期间分别由第一模块和第二模块分别施加的至少一对权限的子模块。 当局被计算为飞机的至少当前运动参数和安全参数的函数。

    VISION SYSTEM FOR AN AIRCRAFT APPROACHING A LANDING RUNWAY AND ASSOCIATED VISION METHOD
    3.
    发明申请
    VISION SYSTEM FOR AN AIRCRAFT APPROACHING A LANDING RUNWAY AND ASSOCIATED VISION METHOD 有权
    用于航空飞行轨迹和相关视觉方法的视觉系统

    公开(公告)号：US20140097973A1

    公开(公告)日：2014-04-10

    申请号：US14044305

    申请日：2013-10-02

    Applicant: DASSAULT AVIATION

    Inventor： Olivier BAUDSON ,  Arnaud TURPIN

    IPC: G08G5/00

    CPC classification number: G08G5/0047 ,  G01C23/00 ,  G06T19/006

    Abstract: The system according to the invention comprises an assembly for managing the graphic interface of a display, capable of controlling the display, on at least a first region of the display, of a peripheral area formed by a synthetic image comprising at least one synthetic surface representation of the terrain, and capable of maintaining at least one area representative of the position of a landing runway, centered on the landing runway, and at least one front area, adjacent to the center area, substantially free of any synthetic surface representation of the terrain. The management assembly includes means for dynamically defining the length (L) of the front area on the display as a function of a vertical decision position (DP) associated with a selected approach for said landing runway.

    Abstract translation: 根据本发明的系统包括用于管理显示器的图形界面的组件，其能够在显示器的至少第一区域上控制由包括至少一个合成表面表示的合成图像形成的外围区域的显示器 并且能够保持代表在着陆跑道上的着陆跑道的位置的至少一个区域，以及与中心区域相邻的至少一个前区域，基本上没有地形的任何合成表面表示 。 管理组件包括用于根据与所述着陆跑道的所选方法相关联的垂直决定位置（DP）来动态地定义显示器上的前区域的长度（L）的装置。

    AIRCRAFT VISION SYSTEM WITH RELIEF LINES AND ASSOCIATED METHOD
    5.
    发明申请
    AIRCRAFT VISION SYSTEM WITH RELIEF LINES AND ASSOCIATED METHOD 有权
    具有救援线和相关方法的飞机视觉系统

    公开(公告)号：US20140100721A1

    公开(公告)日：2014-04-10

    申请号：US14044245

    申请日：2013-10-02

    Applicant: DASSAULT AVIATION

    Inventor： Olivier BAUDSON ,  Arnaud TURPIN

    IPC: B64D45/00

    CPC classification number: B64D45/00 ,  G01C23/00 ,  G06T19/006

    Abstract: The vision system for an aircraft according to the invention comprises a display management system, on a display, capable of dynamically displaying synthetic information coming from a synthetic environment generating assembly on the display. The management assembly can control the display, on a first region of the display, of relief lines representative of the terrain situated facing the aircraft, without displaying synthetic surface representations of the terrain in the intermediate areas situated between the relief lines of the first region of the display. The generating assembly includes means for determining the position of the crest lines of the terrain from topographical data present in at least one database, and means for computing the position of the relief lines from the position of the crest lines of the terrain.

    Abstract translation: 根据本发明的用于飞机的视觉系统包括在显示器上能够动态地显示来自合成环境生成组件的合成信息的显示管理系统。 管理组件可以在显示器的第一区域上控制表示面向飞行器的地形的浮雕线的显示，而不在位于第一区域的浮雕线之间的中间区域中的地形的合成表面表示 显示器。 生成组件包括用于根据存在于至少一个数据库中的地形数据确定地形的顶部线的位置的装置，以及用于从地形的顶部线的位置计算浮雕线的位置的装置。

    DISPLAY SYSTEM OF AN AIRCRAFT, COMPRISING A FLARE GUIDING CUE AND RELATED METHOD
    6.
    发明申请
    DISPLAY SYSTEM OF AN AIRCRAFT, COMPRISING A FLARE GUIDING CUE AND RELATED METHOD 审中-公开
    飞行器显示系统，包含一个引导引擎和相关方法

    公开(公告)号：US20160379502A1

    公开(公告)日：2016-12-29

    申请号：US15189907

    申请日：2016-06-22

    Applicant: DASSAULT AVIATION

    Inventor： Sébastien LEPAGE ,  Olivier BAUDSON ,  Arnaud TURPIN

    IPC: G08G5/02 ,  G08G5/00 ,  B64D45/08

    CPC classification number: G08G5/025 ,  B64D43/00 ,  B64D45/08 ,  G01C23/005 ,  G08G5/0021 ,  G08G5/0086

    Abstract: A display system of an aircraft, including a flare guiding cue and related method are provided. The display system includes a display unit; and an assembly for generating a display on the display unit, configured to dynamically display, on the display unit, at least one horizon line, a slope scale of the aircraft relative to the horizon line, and a speed vector symbol, representative of the slope of the aircraft relative to the horizon line. The display generator is configured to display, upon approaching a landing strip, a flare guidance symbol, the position of the flare guidance symbol on the display unit depending on the topographical slope of the approached landing strip.

    Abstract translation: 提供飞机的显示系统，包括火炬指导提示和相关方法。 显示系统包括显示单元; 以及用于在所述显示单元上生成显示器的组件，被配置为在所述显示单元上动态地显示所述飞机相对于所述水平线的至少一个水平线，斜率以及代表所述斜率的速度矢量符号 的飞机相对于地平线。 显示发生器被配置为在接近着陆条时，根据接近的着陆带的地形坡度，在展示单元上显示火炬引导符号的位置。

    AIRCRAFT VISION SYSTEM, AND ASSOCIATED VISION METHOD
    8.
    发明申请
    AIRCRAFT VISION SYSTEM, AND ASSOCIATED VISION METHOD 有权
    飞机视觉系统及相关视觉方法

    公开(公告)号：US20140214245A1

    公开(公告)日：2014-07-31

    申请号：US14043739

    申请日：2013-10-01

    Applicant: Dassault Aviation

    Inventor： Olivier BAUDSON ,  Arnaud TURPIN

    IPC: B64D45/00

    CPC classification number: B65D45/00 ,  B64D45/00 ,  G06T19/006

    Abstract: The system according to the invention comprises a display and a synthetic image dynamic generating assembly. It includes a management assembly for the graphic interface of the display, capable of controlling the dynamic display, on a first region of the display, of a synthetic image and able to maintain, in certain movement configurations of the aircraft, a second region of the display delimited by the edge substantially with no synthetic surface representation of the terrain. The management assembly includes means for dynamically delimiting the edge of the first region. The delimiting means are configured to dynamically compute the position of the edge as a function of a determined visibility distance (DV), taken relative to the aircraft.

    Abstract translation: 根据本发明的系统包括显示器和合成图像动态产生组件。 它包括用于显示器的图形界面的管理组件，其能够在显示器的第一区域上控制合成图像的动态显示，并且能够在飞行器的某些移动配置中维持第二区域 由边缘基本上没有地形的合成表面表示来界定的显示。 管理组件包括用于动态地限定第一区域的边缘的装置。 定界装置被配置为根据相对于飞机获得的确定的可见距离（DV）来动态地计算边缘的位置。

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