首页> 外国专利> METHOD OF PREDICTION OF AN AIRCRAFT SHORT TERM FLIGHT PATH, COMPUTER PROGRAM PRODUCT, ASSOCIATED PREDICTION DEVICE, GUIDANCE METHOD, GUIDANCE SYSTEM AND AIRCRAFT

METHOD OF PREDICTION OF AN AIRCRAFT SHORT TERM FLIGHT PATH, COMPUTER PROGRAM PRODUCT, ASSOCIATED PREDICTION DEVICE, GUIDANCE METHOD, GUIDANCE SYSTEM AND AIRCRAFT

机译:飞机短途飞行路线的预测方法,计算机程序产品,相关的预测装置,制导方法,制导系统和飞机

摘要

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.
机译:公开了一种用于预测飞机的短期飞行路线的方法,计算机程序产品,相关的预测装置,制导方法和制导系统。一方面,飞机的飞行路径在每个时刻与矢量相关联,该矢量包括飞机的位置,飞机的姿态以及该位置和姿态的阶次和二次时间导数中的至少一个分量。短期飞行路径是指从飞行路径的计算时间起最多30秒的时间段内飞机的飞行路径。该方法包括获取表示飞机的主要控制构件的位移的控制信号,并在随后的预测时间预测飞机的短期飞行路径的至少一个分量。

著录项

  • 公开/公告号EP2957871B1

    专利类型

  • 公开/公告日2017-05-03

    原文格式PDF

  • 申请/专利权人 THALES;

    申请/专利号EP20150170522

  • 申请日2015-06-03

  • 分类号G05D1/10;G01C23;G08G5;

  • 国家 EP

  • 入库时间 2022-08-21 14:06:28

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