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Piloting aid for control of aircraft - employs data acquisition system to present control information in graphic form

机译:飞机控制驾驶辅助工具-使用数据采集系统以图形形式显示控制信息

摘要

A control system for a vehicle, such as an aircraft or marine craft, acts as an aid to the pilot by presenting the control information in graphic form on a screen. This suggests to the pilot that control action is necessary to maintain quality of performance. An aircraft has a number of sensors which are connected to a data acquisition system followed by a filter circuit for the data. A comparator checks these values with instruction values and the difference output is applied to a circuit which tests the range of action. This information is then transmitted to a control calculator which is programmed from a mathematical model of the piloting and which was obtained from experimental conditions. The calculator output is applied via an ordering system to the screen of a synthesiser.
机译:用于车辆的控制系统,例如飞机或海上航行器,通过在屏幕上以图形形式显示控制信息来辅助飞行员。这向飞行员暗示了控制措施对于保持性能质量是必要的。一架飞机有许多传感器,这些传感器连接到数据采集系统,然后连接到数据的滤波电路。比较器用指令值检查这些值,并将差值输出施加到测试作用范围的电路。然后,此信息将传输到控制计算器,该控制计算器是根据飞行员的数学模型进行编程的,并且是从实验条件中获得的。计算器的输出通过订购系统应用于合成器的屏幕。

著录项

  • 公开/公告号FR2439423A1

    专利类型

  • 公开/公告日1980-05-16

    原文格式PDF

  • 申请/专利权人 ADERSA;

    申请/专利号FR19780029781

  • 申请日1978-10-19

  • 分类号G05D1/00;

  • 国家 FR

  • 入库时间 2022-08-22 17:20:28

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