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    System for aiding the piloting of an aircraft during the approach to a runway with a view to a landing
    6.
    发明授权
    System for aiding the piloting of an aircraft during the approach to a runway with a view to a landing 有权
    在进入跑道的过程中协助驾驶飞机的系统，以便着陆

    公开(公告)号：US07647140B2

    公开(公告)日：2010-01-12

    申请号：US11145951

    申请日：2005-06-07

    申请人： Jean-Pierre Demortier ,  Isabelle Lacaze ,  Jean-Louis De Menorval

    发明人： Jean-Pierre Demortier ,  Isabelle Lacaze ,  Jean-Louis De Menorval

    IPC分类号： G06F19/00

    CPC分类号： G05D1/0676

    摘要： A system for aiding the piloting of an aircraft during a runway approach includes an information source that provides information relating to the aircraft and its environment. A computation unit determines, with the aid of information provided by the information source, an energy reference profile having a trajectory reference profile and a speed reference profile that allows the aircraft to regain a stabilized approach trajectory, if it follows the reference profile. A monitor verifies that the aircraft is following the reference profile. An indicator supplies the pilot with piloting indications for piloting the aircraft so as to follow the reference profile.

    摘要翻译： 在跑道方法中辅助飞机驾驶的系统包括提供与飞行器及其环境有关的信息的信息源。 计算单元借助于由信息源提供的信息确定具有轨迹参考轮廓和速度参考轮廓的能量参考轮廓，其允许飞机重新获得稳定的进场轨迹，如果它遵循参考轮廓。 监视器验证飞机是否遵循参考资料。 一个指示器为飞行员提供驾驶飞行员的驾驶指示，以便遵循参考资料。

    System for aiding the piloting of an aircraft during the approach to a runway with a view to a landing
    7.
    发明申请
    System for aiding the piloting of an aircraft during the approach to a runway with a view to a landing 有权
    在进入跑道的过程中协助驾驶飞机的系统，以便着陆

    公开(公告)号：US20060025901A1

    公开(公告)日：2006-02-02

    申请号：US11145951

    申请日：2005-06-07

    申请人： Jean-Pierre Demortier ,  Isabelle Lacaze ,  Jean-Louis De Menorval

    发明人： Jean-Pierre Demortier ,  Isabelle Lacaze ,  Jean-Louis De Menorval

    IPC分类号： G01C23/00

    CPC分类号： G05D1/0676

    摘要： System for aiding the piloting of an aircraft during the approach to a runway with a view to a landing. The system (1) comprises information sources (3) able to provide information relating to the aircraft and to its environment, a computation unit (4) which determines, with the aid of information provided by the information sources (3), an energy reference profile which preferably comprises a trajectory reference profile and a speed reference profile and which is intended to allow the aircraft to regain a stabilized approach trajectory, if it follows this reference profile, means of monitoring (7) for verifying that the aircraft is indeed following said reference profile, and means of indication (6) which supply the pilot with piloting indications at least to make it possible to pilot the aircraft in such a way that it always follows said reference profile.

    摘要翻译： 在进入跑道的过程中协助驾驶飞机的系统，以便着陆。 系统（1）包括能够提供与飞机及其环境相关的信息的信息源（3），计算单元（4），其借助于由信息源（3）提供的信息确定能量参考 其优选地包括轨迹参考轮廓和速度参考轮廓，并且其旨在允许飞机重新获得稳定的进场轨迹（如果遵循该参考轮廓），则监视装置（7）用于验证飞机是否确实遵循所述 参考简档和指示装置（6），其向飞行员提供驾驶指示，至少使得可以以使其始终遵循所述参考轮廓的方式驾驶飞行器。

    Method for checking takeoff or landing parameters, and associated device
    9.
    发明申请
    Method for checking takeoff or landing parameters, and associated device 有权
    检查起飞或着陆参数的方法及相关设备

    公开(公告)号：US20070124034A1

    公开(公告)日：2007-05-31

    申请号：US11563743

    申请日：2006-11-28

    申请人： Fabien Pitard ,  Jean-Pierre Demortier ,  Serge Laporte ,  Serge Boyer ,  Bernard Deret ,  Laurent Fonteneau

    发明人： Fabien Pitard ,  Jean-Pierre Demortier ,  Serge Laporte ,  Serge Boyer ,  Bernard Deret ,  Laurent Fonteneau

    IPC分类号： G06F19/00

    CPC分类号： G05D1/0083

    摘要： A method for checking takeoff or landing parameters of an aircraft comprises a step (E101) of determining takeoff or landing parameters on the basis of a series of input conditions. It additionally comprises the following steps: calculation (E103) of regulatory data on the basis of determined takeoff or landing parameters; and comparison (E104) of the calculated regulatory data with predefined threshold values, with a view to establishing whether the determined takeoff or landing parameters are valid or invalid. Use to ensure reliability of the determination of optimized takeoff or landing parameters.

    摘要翻译： 用于检查飞行器起飞或着陆参数的方法包括基于一系列输入条件来确定起飞或着陆参数的步骤（E 101）。 它还包括以下步骤：根据确定的起飞或着陆参数来计算（E 103）监管数据; 以及计算的调节数据与预定阈值的比较（E 104），以便确定所确定的起飞或着陆参数是有效还是无效。 用于确定优化起飞或着陆参数的可靠性。