首页> 外国专利> Flight management system for aircraft, has filters smoothing surges of curvilinear distance values generated by curvilinear distance calculation unit, and decomposing value surges into elementary levels based on current aircraft speed

Flight management system for aircraft, has filters smoothing surges of curvilinear distance values generated by curvilinear distance calculation unit, and decomposing value surges into elementary levels based on current aircraft speed

机译:飞机的飞行管理系统,具有过滤器,用于平滑由曲线距离计算单元生成的曲线距离值的波动,并根据当前飞机速度将值波动分解为基本水平

摘要

The system has filters smoothing surges of curvilinear distance values that are generated by a curvilinear distance calculation unit. The filters decomposes the value surges into elementary levels as a function of aircraft`s current speed, where the surges are added one to one during periodical updates. The elementary levels are taken equal to a distance covered at the current aircraft speed over a duration of updation period. A unit calculates direct distance between the current position and a geographical position to be attained.
机译:该系统具有滤波器,可平滑由曲线距离计算单元生成的曲线距离值的波动。过滤器将值激增分解为与飞机当前速度有关的基本水平,其中在定期更新期间将激增一对一地相加。基本水平等于更新期间持续时间内当前飞机速度所覆盖的距离。单位计算当前位置和要达到的地理位置之间的直接距离。

著录项

  • 公开/公告号FR2906622B1

    专利类型

  • 公开/公告日2008-11-28

    原文格式PDF

  • 申请/专利权人 THALES;

    申请/专利号FR20060008652

  • 申请日2006-10-03

  • 分类号G05D1/10;B64D43;

  • 国家 FR

  • 入库时间 2022-08-21 19:07:32

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