首页> 外国专利> Method and device for generating at least one set point from a flight control set point, a motor control set point and an aircraft guidance set point, related computer program product and aircraft

Method and device for generating at least one set point from a flight control set point, a motor control set point and an aircraft guidance set point, related computer program product and aircraft

机译:从飞行控制设定点,电动机控制设定点和飞行器制导设定点产生至少一个设定点的方法和装置,相关的计算机程序产品和飞机

摘要

A method and device for generating at least one set point from a flight control set point, a motor control set point and an aircraft guidance set point, a related computer program product and an aircraft are disclosed. In one aspect, the method includes acquiring a mechanical property relative to at least one corresponding primary control member and computing at least one set point from among one or more primary set points and one or more secondary set points. The method also includes generating at least one of the computed set point(s) and switching, based on the mechanical property acquired for the corresponding primary control member, between a first mode in which one or more primary set points are generated and a second mode in which one or more secondary set points are generated.
机译:公开了一种用于从飞行控制设定点,电动机控制设定点和飞机制导设定点产生至少一个设定点的方法和设备,相关的计算机程序产品和飞机。一方面,该方法包括获取相对于至少一个相应的主要控制构件的机械性能,以及从一个或多个主要设定点和一个或多个次要设定点中计算至少一个设定点。该方法还包括生成所计算的设定点中的至少一个,并且基于为相应的主控制构件获取的机械特性,在生成一个或多个主要设定点的第一模式与第二模式之间进行切换。其中产生一个或多个次级设定点。

著录项

  • 公开/公告号US9604718B2

    专利类型

  • 公开/公告日2017-03-28

    原文格式PDF

  • 申请/专利权人 THALES;

    申请/专利号US201514740023

  • 申请日2015-06-15

  • 分类号G05D1;G05B19/18;B64C13/22;B64C13/04;B64C13/18;B64D31/04;B64D31/06;B64D31;

  • 国家 US

  • 入库时间 2022-08-21 13:42:53

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