首页> 外国专利> FLIGHT MANAGEMENT SYSTEM WITH INTEGRATED TACTICAL COMMANDS FOR USE WITH AN AIRCRAFT AND METHOD OF OPERATING SAME

FLIGHT MANAGEMENT SYSTEM WITH INTEGRATED TACTICAL COMMANDS FOR USE WITH AN AIRCRAFT AND METHOD OF OPERATING SAME

机译:与飞机一起使用的具有综合战术命令的飞行管理系统和相同的操作方法

摘要

A flight management system (24) for use in automatically generating a flight path trajectory (26) for an aircraft (10) is provided. The flight path trajectory including a plurality of waypoints (28) and a plurality of vectors (30) extending between each waypoint of the plurality of waypoints, the flight management system including a processor (302) is configured to calculate a first flight path trajectory (36) including an origin waypoint (40) and a destination waypoint (42), receive a tactical command indicating a change in flight trajectory, and calculate a second flight path trajectory (38) based at least in part on the tactical command, the calculated second flight path trajectory including a departure waypoint along the first flight path trajectory, an intercept waypoint (48) along the first flight path trajectory, and a departure vector from the departure waypoint (46) to the intercept waypoint.
机译:提供了一种用于自动生成飞机(10)的飞行轨迹(26)的飞行管理系统(24)。包括多个航路点(28)和在多个航路点的每个航路点之间延伸的多个矢量(30)的飞行航迹轨迹,包括处理器(302)的飞行管理系统配置为计算第一飞行航迹轨迹(包括起点航路点(40)和目的地航路点(42)的36),接收指示飞行轨迹变化的战术命令,并至少部分地基于该战术命令来计算第二飞行路线轨迹(38),第二飞行路径轨迹包括沿着第一飞行路径轨迹的出发航点,沿着第一飞行路径轨迹的拦截航点(48)以及从出发航点(46)到拦截航点的离开向量。

著录项

  • 公开/公告号CA2763334C

    专利类型

  • 公开/公告日2019-09-17

    原文格式PDF

  • 申请/专利权人 GE AVIATION SYSTEMS LLC;

    申请/专利号CA20122763334

  • 发明设计人 WALTER RANDY LYNN;

    申请日2012-01-05

  • 分类号G05D1/10;B64D43;B64D47;G08G5;

  • 国家 CA

  • 入库时间 2022-08-21 11:59:13

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