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SYSTEM FOR ESTIMATING AIRSPEED OF AIRCRAFT BASED ON WEATHER BUFFER MODEL

机译:基于天气缓冲模型的飞机起降估算系统

摘要

To provide a system including a weather buffer model for estimating airspeed in an extreme flight condition of an aircraft.SOLUTION: A system and a method for estimating a plurality of airspeed parameters of an aircraft are disclosed. The system comprises one or more processors and a memory coupled to the processor. The memory storing data comprises a database and a program code that, when executed by the one or more processors, causes the system to receive a plurality of operating parameters that each represents one operating condition of the aircraft. The system is further caused to determine a model based dynamic pressure based on the operating parameters. The model based dynamic pressure is estimated based on steady flight conditions of the aircraft. The system is further caused to determine a bridge based dynamic pressure based on at least a temperature deviation and an inertial speed vector. The bridge based dynamic pressure is estimated for extreme flight conditions of the aircraft.SELECTED DRAWING: Figure 3
机译:提供一种包括天气缓冲器模型的系统,用于估计飞机的极端飞行条件下的空速。解决方案:公开了一种用于估计飞机的多个空速参数的系统和方法。该系统包括一个或多个处理器以及耦合到该处理器的存储器。存储数据的存储器包括数据库和程序代码,当由一个或多个处理器执行该程序代码时,程序代码使系统接收多个运行参数,每个运行参数代表飞机的一种运行状态。进一步促使系统基于操作参数确定基于模型的动压。基于模型的动态压力是根据飞机的稳定飞行条件估算的。进一步使系统至少基于温度偏差和惯性速度矢量来确定基于桥的动压。根据飞机的极端飞行条件估算出基于桥梁的动压力选图:图3

著录项

  • 公开/公告号JP2019038519A

    专利类型

  • 公开/公告日2019-03-14

    原文格式PDF

  • 申请/专利权人 BOEING CO;

    申请/专利号JP20180107379

  • 发明设计人 LUO JIA;

    申请日2018-06-05

  • 分类号B64D43/02;G01P5;

  • 国家 JP

  • 入库时间 2022-08-21 12:24:51

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