首页> 外国专利> Real-time method for determining the behavior of an aircraft is based on use of a linear model of the aircraft that is continuously updated by calculation of an equilibrium state vector and from it dynamic model components

Real-time method for determining the behavior of an aircraft is based on use of a linear model of the aircraft that is continuously updated by calculation of an equilibrium state vector and from it dynamic model components

机译:用于确定飞机行为的实时方法是基于飞机线性模型的使用,该线性模型通过计算平衡状态矢量及其动态模型组件不断进行更新

摘要

The method involves repeating the following steps ; (a) determination of a vector lambda illustrating the current state of equilibrium from a current linear model of the aircraft (b) determination of equilibrium values for model parameters from lambda (c) calculation of the dynamic component of model behavior from at least a number of the values (d) introduction of the dynamic component into the linear model to obtain a new current linear model An Independent claim is made for a device for real-time determination of the behavior of an aircraft.
机译:该方法涉及重复以下步骤; (a)从飞机的当前线性模型确定说明当前平衡状态的向量lambda(b)从lambda确定模型参数的平衡值(c)从至少一个数字计算模型行为的动态分量值(d)将动态分量引入线性模型以获得新的当前线性模型的说明。对用于实时确定飞机行为的设备提出了独立权利要求。

著录项

  • 公开/公告号FR2831301A1

    专利类型

  • 公开/公告日2003-04-25

    原文格式PDF

  • 申请/专利权人 EUROCOPTER;

    申请/专利号FR20010013435

  • 发明设计人 EGLIN PAUL;

    申请日2001-10-18

  • 分类号G06G7/78;G06N7/00;G09B9/08;

  • 国家 FR

  • 入库时间 2022-08-21 23:37:50

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