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System and method for converting an aircraft from a flight condition lying outside a permissible flight condition range to a flight condition lying within the permissible flight condition range

机译:用于将飞机从处于允许的飞行条件范围之外的飞行条件转换为处于允许的飞行条件范围内的飞行条件的系统和方法

摘要

A system and method for converting an aircraft from a flight condition lying outside a permissible flight condition range to a flight condition lying within the permissible flight condition range, that can be assigned to a sensor system and a control device of the aircraft. The system includes a control override module for taking over or returning the control authority over the aircraft based on a control take-over signal and for feeding control set points if the control takeover signal is set; a maneuver selection module; a threshold value generator for calculating the flight range limit on the basis of measured variables of the sensor system; a decision module; a command generator that is functionally connected on the one hand to the decision module and the maneuver selection module and on the other hand to the control override module and, when the control takeover signal is set, calculates the control set points based on the maneuver information and transmits them to the control override module.
机译:一种用于将飞机从处于允许的飞行条件范围之外的飞行状态转换到处于许可的飞行条件范围内的飞行条件的系统和方法,其可以被分配给飞机的传感器系统和控制装置。该系统包括控制超控模块,该控制超控模块用于基于控制接管信号来接管或返回飞行器的控制权限,并且如果设置了控制接管信号,则用于馈送控制设定点;以及机动选择模块;阈值发生器,用于基于传感器系统的测量变量来计算飞行距离极限;决策模块;命令发生器,其功能上一方面与决策模块和操纵选择模块相连,另一方面与控制超控模块相连,并且在设置了控制接管信号时,会根据操纵信息计算控制设定点并将它们传输到控制优先模块。

著录项

  • 公开/公告号US7676303B2

    专利类型

  • 公开/公告日2010-03-09

    原文格式PDF

  • 申请/专利权人 MARTIN HANEL;

    申请/专利号US20060485313

  • 发明设计人 MARTIN HANEL;

    申请日2006-07-13

  • 分类号G01C23;

  • 国家 US

  • 入库时间 2022-08-21 18:47:43

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