首页> 外国专利> INTEGRATED TEST SYSTEM FOR SUPPORTING MULTIPLE FORMS OF AIRCRAFT AND MEHTOD FOR CONTROLLING THAT SYSTEM

INTEGRATED TEST SYSTEM FOR SUPPORTING MULTIPLE FORMS OF AIRCRAFT AND MEHTOD FOR CONTROLLING THAT SYSTEM

机译:支持多种形式飞机的综合测试系统及其控制方法

摘要

aspect of the present invention is to achieve out of this experimental system that supports a single configuration of the aircraft derivative aircraft aircraft to provide a method for controlling a multi-shape for supporting integrated test system and a system supporting. According to one aspect of the present invention, in the aircraft for supporting integrated laboratory, a power supply for supplying power to equipment mounted on the aircraft integrated laboratory; Power control unit for controlling the power supplied to the equipment for the aircraft from the power supply; A signal control unit for controlling the number of data signal transmitted and received between the equipment for aircraft cross; And a first control unit for controlling the shape of the power control unit and the signal control unit; Shape for supporting a multi-service aircraft test system includes the integration is, (a) step of receiving the aircraft geometry to be implemented in integrated laboratory; (B) the (a) to read the control data received from the base of the aircraft-like step is a step; And (c) input in step (a) to control the power control unit and signal control unit according to any one of claims 1 to 4, wherein in the first configuration the control unit according to any one of claims 1 to 4, wherein The steps to configure the receiving aircraft configuration; How to control the aircraft for supporting multiple integrated test system that includes a shape is provided. Thus, by experiment system can be expanded to support the aircraft in the aircraft of the multi-like support system for a single experiment shape, avoid prolonged conventional single-like aircraft support the development and production cost increase arising from the period of experiment systems, aircraft The experimental system of support equipment can easily add and delete using the shape control software, it can be used by the operator to easily set the environment that you want to use, excellent in scalability, when adding and deleting of aircraft support equipment test system does not affect the shape of the other equipment aircraft configuration is easy. ;
机译:本发明的一个方面是从该实验系统中实现,该实验系统支持飞机衍生飞机的单一配置,以提供一种用于控制用于支持综合测试系统的多形状的方法和系统支持。根据本发明的一个方面,在用于支持综合实验室的飞机中,电源用于向安装在飞机综合实验室上的设备供电。功率控制单元,用于控制从电源向飞机设备提供的功率;信号控制单元,用于控制飞机交叉设备之间收发的数据信号的数量;第一控制单元,用于控制功率控制单元和信号控制单元的形状;用于支持多用途飞机测试系统的形状包括集成:(a)接收要在集成实验室中实施的飞机几何形状的步骤; (b)。(a)。读取从飞机基接​​收的控制数据的步骤是步骤; (c)在步骤(a)中输入以控制根据权利要求1至4中任一项所述的功率控制单元和信号控制单元,其中在第一配置中,根据权利要求1至4中任一项所述的控制单元,其中配置接收飞机配置的步骤;提供了如何控制飞机以支持包括形状的多个集成测试系统。这样,通过扩展实验系统就可以将飞机支持在多架飞机的单一样机支撑系统中进行单个实验形状,避免了传统的单架飞机长时间的支撑架的开发和生产成本的增加,实验系统的周期,飞机辅助设备的实验系统可以使用形状控制软件轻松地添加和删除,操作员可以在添加和删除飞机辅助设备测试系统时轻松地设置想要使用的环境,扩展性极佳。不影响其他设备外形的飞机配置很容易。 ;

著录项

  • 公开/公告号KR101298779B1

    专利类型

  • 公开/公告日2013-08-22

    原文格式PDF

  • 申请/专利权人

    申请/专利号KR20110056054

  • 发明设计人 김경태;

    申请日2011-06-10

  • 分类号B64F5/00;G01M99/00;

  • 国家 KR

  • 入库时间 2022-08-21 16:24:37

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