首页> 外国专利> METHOD FOR MODELING AIRCRAFT PERFORMANCE THROUGH ADAPTIVE AIRCRAFT PERFORMANCE MODELS

METHOD FOR MODELING AIRCRAFT PERFORMANCE THROUGH ADAPTIVE AIRCRAFT PERFORMANCE MODELS

机译:通过自适应飞机性能模型建模飞机性能的方法

摘要

A method for modeling aircraft performance including (a) introducing aircraftdegradation coefficients in a nominal aircraft performance model of anaircraft andobtaining a degraded aircraft performance model, (b) calculating computedtrajectorydata in a trajectory computation infrastructure using as inputs aircraftintent whichrepresents trajectory data, weather data, and the degraded aircraftperformancemodel; (c) comparing the trajectory data with the computed trajectory data;(d)obtaining an enhanced aircraft performance model by considering the degradedaircraft performance model as the enhanced aircraft performance model, whentheresult of the comparison is less than a previously established threshold; and(e)modifying, when the result of the comparison is higher than the previouslyestablished threshold, the aircraft degradation coefficients and executingsteps (a) to(e) of the method, until the result of the comparison is less than thepreviouslyestablished threshold.
机译:一种对飞机性能进行建模的方法,包括(a)引入飞机飞机名义性能模型中的退化系数飞机和获得降级的飞机性能模型,(b)计算得出弹道轨迹计算基础设施中的数据用作输入飞机意向表示轨迹数据,天气数据和退化的飞机性能模型; (c)将轨迹数据与计算出的轨迹数据进行比较;(d)通过考虑降级来获得增强的飞机性能模型飞机性能模型作为增强型飞机性能模型的比较的结果小于先前确定的阈值;和(e)修改,当比较的结果高于先前的确定的阈值,飞机降级系数并执行步骤(a)至(e)的方法,直到比较结果小于先前确定的阈值。

著录项

  • 公开/公告号CA2869686C

    专利类型

  • 公开/公告日2017-12-05

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号CA20142869686

  • 发明设计人 CASADO MAGANA ENRIQUE JUAN;

    申请日2014-11-04

  • 分类号G08G5;G07C5/08;

  • 国家 CA

  • 入库时间 2022-08-21 12:48:04

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