METHOD FOR PREDICTING A SHORT TERM FLIGHT PATH OF AN AIRCRAFT, COMPUTER PROGRAM PRODUCT, ASSOCIATED PREDICTION DEVICE, GUIDANCE METHOD, GUIDANCE SYSTEM AND AIRCRAFT
    2.
    发明申请
    METHOD FOR PREDICTING A SHORT TERM FLIGHT PATH OF AN AIRCRAFT, COMPUTER PROGRAM PRODUCT, ASSOCIATED PREDICTION DEVICE, GUIDANCE METHOD, GUIDANCE SYSTEM AND AIRCRAFT 有权
    用于预测飞机短程飞行路径的方法,计算机程序产品,相关预测装置,指导方法,指导系统和飞机

    公开(公告)号:US20150364046A1

    公开(公告)日:2015-12-17

    申请号:US14739303

    申请日:2015-06-15

    Applicant: THALES

    CPC classification number: G08G5/0047 G01C23/00 G05D1/101

    Abstract: A method for predicting a short-term flight path of an aircraft, a computer program product, an associated prediction device, a guidance method, and a guidance system of an aircraft are disclosed. In one aspect, the flight path of the aircraft is associated at each time moment with a vector including at least one component from among a position of the aircraft, attitudes of the aircraft and order 1 and 2 time derivatives of the position and attitudes. The short-term flight path is the flight path of the aircraft for a time period of up to 30 seconds from a computation time of the flight path. The method includes acquiring a control signal representative of a displacement of a primary control member of the aircraft and predicting, at a subsequent prediction time, at least one component of the short-term flight path of the aircraft. The prediction step can be carried out at the computation time.

    Abstract translation: 公开了一种用于预测飞行器的短期飞行路径的方法,计算机程序产品,相关联的预测装置,引导方法和飞行器的引导系统。 在一个方面,飞行器的飞行路径在每个时刻与包括从飞机的位置,飞行器的姿态以及位置和态度的顺序1和2时间导数之间的至少一个分量的矢量相关联。 短程飞行路径是从飞行路线的计算时间起飞机飞行时间长达30秒的飞行路线。 该方法包括获取表示飞行器的主控制构件的位移的控制信号,并且在随后的预测时间预测飞行器的短期飞行路径的至少一个分量。 预测步骤可以在计算时进行。

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