首页> 外国专利> Method of adapting a segment of an aircraft trajectory with constant ground gradient segment according to at least one performance criterion

Method of adapting a segment of an aircraft trajectory with constant ground gradient segment according to at least one performance criterion

机译:根据至少一个性能标准使具有恒定地面坡度段的飞机轨迹段适应的方法

摘要

A method for adapting an aircraft constant-gradient descent segment comprises: an acquisition step in which state variables characterizing the aircraft, environment variables characterizing the environment thereof and path variables characterizing the predicted path thereof at one of the initial and final points of the segment are acquired; a calculation step whereby a limit ground gradient for at least one performance criterion is calculated from the state variables, environment variables and path variables; a validity verification step checking the validity of the path initially predicted against the most restrictive limit ground gradient; and when the path initially predicted is not valid: a feasibility verification step checking the feasibility of a command to modify at least one state variable; if feasibility is verified, a prediction of executing the command; otherwise, a prediction of modifying one of the initial and final points of the segment with respect to constraints of the flight plan.
机译:一种用于调整飞机恒定梯度下降段的方法,包括:采集步骤,其中表征飞机的状态变量,表征飞机的环境的环境变量以及表征飞机的初始和最终点之一的预测路径的路径变量是获得计算步骤,从状态变量,环境变量和路径变量中计算出至少一个性能标准的极限地面坡度;有效性验证步骤,对照最严格的极限地面坡度检查最初预测的路径的有效性;当最初预测的路径无效时,可行性验证步骤检查修改至少一个状态变量的命令的可行性;如果可行性得到验证,则预测执行命令;否则,将根据飞行计划的约束来修改航段的起点和终点之一。

著录项

  • 公开/公告号US10126756B2

    专利类型

  • 公开/公告日2018-11-13

    原文格式PDF

  • 申请/专利权人 THALES;

    申请/专利号US201514861610

  • 发明设计人 JOHAN BOYER;RÉMY AULETTO;NORBERT BALOCHE;

    申请日2015-09-22

  • 分类号G05D1/04;G01C21;G05D1/06;G01C23;G08G5/02;G08G5;

  • 国家 US

  • 入库时间 2022-08-21 12:11:58

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