Abstract:
Disclosed herein are a method and apparatus for performing a configuration of an aeronautical system. The apparatus includes a display unit, an intermediate model generation unit, an Extensible Markup Language (XML) conversion unit, and a translator. The display unit display displays a user interface for receiving aeronautical system setting information in compliance with an ARINC 653 standard. The intermediate model generation unit generates an intermediate model of source code based on the setting information received via the user interface. The XML conversion unit creates an XML document by performing XML conversion on the generated intermediate model. The translator generates a source code file in compliance with the ARINC 653 standard by converting the generated XML document.
Abstract:
Disclosed herein is an apparatus for providing a user interface used to input the configuration values of an aeronautical system. The apparatus includes a software architecture unit for receiving or checking the attributes of software applied to the aeronautical system, a hardware architecture unit for providing a hardware design model that is a base for the operation of the software, a scheduling unit for receiving information about the scheduling of partition information that belongs to the configuration values and transforming the scheduling information in a specific form, a memory unit for storing the attributes of the software, a health monitoring unit for configuring health monitoring based on the software architecture unit, and a connection unit for receiving connection information regarding that partitions are connected to which channel.