AIRCRAFT PILOTING ASSISTANCE METHOD

    公开(公告)号:US20250078838A1

    公开(公告)日:2025-03-06

    申请号:US18824807

    申请日:2024-09-04

    Applicant: THALES

    Abstract: An aircraft piloting assistance method, including the following steps implemented by an electronic piloting assistance device: detecting an event, with said event being an event for identifying a note class from among a set of predefined events for identifying N note classes, with N being an integer≥2; following the detecting step, triggering the acquisition of a voice signal currently being transmitted or received by the pilot and associated with the note class, and processing the acquired voice signal, with the processing being a function of the note class and comprising at least the conversion of the voice signal into text and the generation of a note as a function of the text.

    METHOD AND DEVICE FOR DETERMINING THE OPTIMAL TURN DIRECTION OF AN AIRCRAFT
    2.
    发明申请
    METHOD AND DEVICE FOR DETERMINING THE OPTIMAL TURN DIRECTION OF AN AIRCRAFT 有权
    用于确定飞机的最佳方向的方法和装置

    公开(公告)号:US20150356874A1

    公开(公告)日:2015-12-10

    申请号:US14730088

    申请日:2015-06-03

    Applicant: THALES

    CPC classification number: G08G5/0034 G05D1/0202 G08G5/0039 G08G5/0047

    Abstract: A method determines the optimal turn direction of an aircraft among two directions, right and left, following a lateral trajectory to join an arrival straight charted by an angle of arrival, based on a departure point and angle of departure defining a departure straight oriented along movement of the aircraft, the direction defined by a respectively positive or negative optimal turn sign, comprising: determining a conventional departure sign of the departure point; determining a centred value of an angle of change of course equal to the difference between the angle of arrival and angle of departure referred back between −180° and +180°, the centred value exhibiting a logical sign corresponding to the centred value sign of the angle of change of course; determining the sign of the optimal turn based on comparison between the departure sign and the logical sign, the sign of the optimal turn defining optimal turn direction.

    Abstract translation: 一种方法基于出发点和离开角度定义沿着运动定向的出发直线,确定飞机在左右两个方向之间的最佳转向方向,沿着横向轨迹连接到达到达的直线的方向 所述飞行器的方向由相应的正或负最佳转向标志限定,包括:确定出发点的常规出发标志; 确定变化角度的中心值当然等于-180°至+ 180°之间所指的到达角和出发角之间的差异,该中心值表现出对应于中心值符号的逻辑符号 变化的角度; 根据出发符号和逻辑符号之间的比较确定最佳转弯的符号,最佳转向的符号确定最佳转向方向。

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