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Aircraft

A technology of aircraft and microcontroller, applied in the field of aircraft to achieve the effect of ensuring integrity

Active Publication Date: 2018-11-23
LIEBHERR AEROSPACE LINDENBERG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] A disadvantage here is that the electrical interface is only compatible with certain types of sensors or analog interfaces or can only be used to actuate certain drive elements or other components
[0004] Therefore, using the same electronic device for different applications is only very limited or impossible according to the prior art

Method used

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Embodiment Construction

[0035] exist figure 1 The electronic device is denoted by reference numeral 100 . Reference numeral 10 denotes critical and non-critical interfaces or sensors, wherein critical and non-critical interfaces or sensors are arranged in region 10 a and non-critical interfaces or sensors are arranged or provide their signals in region 10 b.

[0036] As can further be seen from the figures, the non-critical signals according to 10b are transmitted to the discrete input / output modules (In / Out) of the power switch 111 or to the analog input / output modules (Input / Output) 112 . The same applies to critical and non-critical interfaces or sensors 10a, which are likewise transmitted to units 111 and 112, a configurable signal correlation device 60 being arranged between these two components. The electronic device therefore preferably has, in addition to the microcontroller 30 and one or more FPGA cores 20 , means for a configurable signal correlation device 60 .

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Abstract

The invention relates to an aircraft comprising at least one component and at least one electronic device for controlling the component, wherein the electronic device has at least one interface, by means of which signals can be provided for controlling the component, wherein the electronic device has a combination of at least one micro-controller and at least one FPGA core, which are connected toone another via a communications connection, wherein the FPGA core can be configured such that signals can be processed that are each different from one another according to the configuration of the FPGA core.

Description

technical field [0001] The invention relates to an aircraft having at least one component and having at least one electronic device for actuating the component, wherein the electronic device has at least one interface by means of which a signal for actuating the component is provided. Background technique [0002] The use of so-called remote electronic units (REUs) is known from the prior art, which are adapted for specific applications in order to be used only for the associated electrical interface. [0003] A disadvantage here is that the electrical interface is only compatible with certain types of sensors or analog interfaces or can only be used to actuate certain drive elements or other components. [0004] Therefore, using the same electronic device for different applications is only very limited or impossible according to the prior art. Contents of the invention [0005] It is therefore the object on which the invention is based to improve an aircraft of the type ...

Claims

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Application Information

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IPC IPC(8): G05D1/00B64C13/50G05B19/05G05B23/02G06F15/78
CPCG05B19/0421B64D43/00G06F13/4027G05D1/0077H04L12/40032H04L2012/4028
Inventor 赖内·米尔扎雷克弗兰克·克伦布格
Owner LIEBHERR AEROSPACE LINDENBERG
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