首页> 外国专利> METHOD FOR CALCULATING A VERTICAL TRACK OF AN AIRCRAFT FROM ITS CURRENT POSITION, COMPUTER PROGRAM PRODUCT AND CALCULATION SYSTEM THEREFOR

METHOD FOR CALCULATING A VERTICAL TRACK OF AN AIRCRAFT FROM ITS CURRENT POSITION, COMPUTER PROGRAM PRODUCT AND CALCULATION SYSTEM THEREFOR

机译:从飞机当前位置计算垂直轨迹的方法,计算机程序产品及其计算系统

摘要

This method comprises a step of determining (115) a vertical trajectory of the aircraft comprising sub-steps of calculating (120, 130) an initial trajectory section and N following trajectory sections, to compose (135) the vertical trajectory of the aircraft from the calculated trajectory sections and freeze this vertical trajectory. The method further comprises steps for determining (140) a status of each of the altitude constraints along the entire vertical trajectory of the aircraft, each status being chosen between an attainable status when the corresponding altitude constraint is satisfied. and a status missed in the opposite case, and display (150) to the operator of the vertical trajectory of the aircraft and the altitude constraints determined status.
机译:该方法包括确定(115)飞机的垂直轨迹的步骤,该子步骤包括计算(120、130)初始轨迹截面和N个跟随轨迹截面的子步骤,以从(120)中构成(135)飞机的竖直轨迹。计算轨迹截面并冻结此垂直轨迹。该方法进一步包括确定(140)沿飞行器的整个垂直轨迹的每个高度限制的状态的步骤,当满足相应的高度限制时,在可获得的状态之间选择每个状态。在相反情况下错过状态,并向操作者显示(150)飞机的垂直轨迹和高度限制确定状态。

著录项

  • 公开/公告号FR3068490A1

    专利类型

  • 公开/公告日2019-01-04

    原文格式PDF

  • 申请/专利权人 THALES;

    申请/专利号FR20170000697

  • 发明设计人 MANUEL BAUER;GEOFFREY DURAND;

    申请日2017-06-30

  • 分类号G05D1/06;G01C21/20;

  • 国家 FR

  • 入库时间 2022-08-21 11:43:53

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号