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

    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。

    System for aiding the piloting of an aircraft during the approach to a runway with a view to a landing
    8.
    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

    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。

    Terrain avoidance method and system for an aircraft
    10.
    发明授权
    Terrain avoidance method and system for an aircraft 有权
    飞机的地形回避方法和系统

    公开(公告)号:US07899620B2

    公开(公告)日:2011-03-01

    申请号:US11908786

    申请日:2006-03-01

    IPC分类号: G08G1/16

    摘要: A terrain avoidance method and system for an aircraft includes a collision alarm device and an auto-pilot device including a first determination unit for determining a climbing order with optimal slope for the aircraft, a checking unit for checking whether a first altitude gain at the relief, by applying the optimal slope climbing order, is sufficient for clearing said relief, a finding unit for finding if at least one heading variation value exists, for which the corresponding altitude gain is sufficient to clear the relief, and a switching and calculating unit for applying to the aircraft, if the first altitude gain is sufficient, an optimal slope climbing order with an order to maintain the current heading and, if the first altitude gain is insufficient, a particular climbing order sufficient to clear the relief, with a heading order which corresponds to the selected heading variation value.

    摘要翻译: 一种用于飞行器的地形回避方法和系统包括一个碰撞报警装置和一个自动导航装置,包括用于确定飞机具有最佳坡度的爬坡顺序的第一确定单元,用于检查浮雕处的第一高度增益的检查单元 通过应用最佳坡度爬坡顺序,足以清除所述浮雕,找出单元,用于确定是否存在至少一个航向变化值,相应的高度增益足以使其消除浮力;以及切换和计算单元,用于 如果第一高度增益足够,则适用于飞机,具有维持当前航向的最佳斜坡爬升顺序,如果第一高度增益不足,则具有足以清除浮雕的特定爬坡顺序 其对应于所选择的航向变化值。