Method for realizing airborne software and hardware matching loading system

A software system and matching technology, applied in the field of aviation information, can solve the problems of low loading efficiency of airborne software and hardware

Inactive Publication Date: 2019-11-22
上海航空工业(集团) 有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In order to solve the problem of low loading efficiency of existing airborne software and hardware, the present invention provides a method for realizing an airborne software and hardware matching loading system. The method for implementing an airborne software and hardware matching loading system includes the following step:

Method used

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  • Method for realizing airborne software and hardware matching loading system
  • Method for realizing airborne software and hardware matching loading system

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Embodiment Construction

[0037] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals designate the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.

[0038] see figure 1 According to an embodiment of the present invention, a method for realizing matching loading of onboard software and hardware includes the following steps S101 to S105:

[0039] Step S101: Create an airborne equipment system view configuration item, an airborne equipment system design module, and an airborne equipment associated object that characterizes the order effectiveness of the airborne equipment system design module according to the aircraft configuration plan, the airborne equipment The associated object is ...

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Abstract

The invention discloses a method for realizing airborne software and hardware matching loading. The method comprises the following steps: creating an airborne equipment system view configuration item,an airborne equipment system design module and an airborne equipment associated object; creating an airborne software system view configuration item, an airborne software system design module and anairborne software association object, and associating the airborne equipment system view configuration item with the airborne software system view configuration item; and hanging the airborne equipment system view configuration item and the airborne software system view configuration item to a preset system view top layer structure node. The method comprises the following steps: creating an airborne equipment system view configuration item, an airborne equipment system design module, an airborne equipment associated object, an airborne software system view configuration item, an airborne software system design module and an airborne software associated object; and the airborne software system design module capable of being used for loading is screened out in a mode of associating the airborne equipment system view configuration item with the airborne software system view configuration item, so that the loading efficiency is improved.

Description

technical field [0001] The invention relates to the field of aeronautical information, in particular, the invention relates to a method for implementing an airborne software and hardware matching loading system. Background technique [0002] The current design and development of domestic civil aircraft adopts the internationally popular "main engine factory-supplier" working mode. For the airborne software development process, OEMs define aircraft requirements, system requirements, and interface control specifications, and confirm and verify the proposed requirements; suppliers develop equipment requirements and high-level software requirements based on system requirements, and based on software High-level requirements, according to RTCA / DO-178B as a compliance method to develop software products to achieve predetermined functions. [0003] Civil aircraft airborne software has the characteristics of long development cycle, frequent version updates, and intensive related eng...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F9/445G06F17/50
CPCG06F9/44521
Inventor 韩志芳石新景俞晓波姜佳璐雷华欢
Owner 上海航空工业(集团) 有限公司
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