TRAJECTORY MONITORING
    1.
    发明申请
    TRAJECTORY MONITORING 有权
    轨道监测

    公开(公告)号:US20160358482A1

    公开(公告)日:2016-12-08

    申请号:US15171887

    申请日:2016-06-02

    Applicant: THALES

    CPC classification number: G08G5/0047 G05D1/0077 G06F11/16

    Abstract: A method for monitoring the flight trajectory of an aircraft comprises the steps reiterated in time consisting in receiving and comparing two trajectory objects, the trajectory objects being associated with two initially identical flight trajectories determined independently of each other over time; and, in case of difference between the two trajectory objects, determining a failed trajectory from the two flight trajectories by comparison with the last known state without fault, the last known state without fault corresponding to two identical trajectory objects. Developments describe the use of flight plan segments, of signatures, fault isolation simultaneously to a change of current leg, the use of levels of operational safety according to an RNP-AR procedure and the notification of the pilot of the trajectory determined as having failed. Software and system aspects are also described.

    Abstract translation: 用于监视飞行器的飞行轨迹的方法包括在时间上重复的步骤,包括接收和比较两个轨迹对象,轨迹对象与随时间彼此独立地确定的两个最初相同的飞行轨迹相关联; 并且在两个轨迹对象之间的差异的情况下,通过与没有故障的最后一个已知状态进行比较来确定来自两个飞行轨迹的故障轨迹,对于两个相同的轨迹对象,最后一个没有故障的已知状态。 发展描述了使用飞行计划段,签名,故障隔离同时改变当前路段,使用根据RNP-AR程序的操作安全级别以及确定为失败的轨迹的导频的通知。 还描述了软件和系统方面。

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