Multi-CDS-instance-integrated high-performance cockpit display system

A cockpit display system, high-performance technology, applied in the direction of digital output to display equipment, data processing input/output process, instruments, etc., can solve the problem of reducing the performance of screen A, and meet the requirements of improving display performance and real-time performance high effect

Active Publication Date: 2019-08-02
CHINESE AERONAUTICAL RADIO ELECTRONICS RES INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In many UA systems, some UA screens (Screen A) are relatively simple, and the display drawing time is relatively short, such as 1 time unit, while some UA screens (Screen B) are more complicated, and the display drawing time is long

Method used

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  • Multi-CDS-instance-integrated high-performance cockpit display system
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  • Multi-CDS-instance-integrated high-performance cockpit display system

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Embodiment Construction

[0019] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention more clear, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Apparently, the described embodiments are some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0020] The features of various aspects of the embodiments of the present invention will be described in detail below. In the following detailed description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. It will be apparent, however, to one skilled in the art that the present invention may be pra...

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Abstract

The invention belongs to the technical field of integrated avionics system design, relating to a multi-CDS instance integrated high-performance cabin display system based on ARINC661. The system comprises a partition operation system module, a configuration file display module, an IO communication module, a CDS software module, a window management module and a display scheduling module. The partition operation system module is used for providing a plurality of independent physically isolated partitions for an integrated platform of the cabin display system, different CDS instances run in different partitions, and each CDS instance calls different display configuration files and finally displays the display configuration files through the display scheduling module and the window managementmodule. According to the system, a plurality of CDS instances are operated in a plurality of partitions on a partition operation system, different UA layers are drawn in different areas on a physicaldisplay. Different drawing frequencies are completed in different display areas, and the overall display performance of the system is improved.

Description

technical field [0001] The invention belongs to the technical field of comprehensive avionics system design, in particular to a high-performance cockpit display system integrated with multiple CDS instances based on ARINC661. Background technique [0002] With the continuous improvement of the integration of avionics systems and the continuous improvement of the requirements for human-computer interaction, the cockpit display system is also developing towards an open architecture. The ARINC661 specification divides the cockpit display system into UA (UserApplication, UA for short) and CDS ( Cockpit Display System (CDS for short) two functional modules, aiming to completely isolate the display function and logic processing function of the interface, and improve the openness and portability of the display system. A complex cockpit display system integrates multiple UA subsystems. All UA system parameters need to be comprehensively displayed on one display. In the existing disp...

Claims

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Application Information

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IPC IPC(8): G06F3/14
CPCG06F3/1407G06F3/1423
Inventor 许药林钱珏宋青钱学佳胡潇
Owner CHINESE AERONAUTICAL RADIO ELECTRONICS RES INST
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