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Communication data link fusion method and device and computer readable storage medium

A technology of communication data and fusion method, applied in the field of aviation communication, can solve the problems of single communication channel system communication failure, loss, and high reliability dependence of single communication channel, so as to reduce stability dependence, avoid communication failure, and improve system reliability sexual effect

Pending Publication Date: 2022-01-11
西安怀智电子科技有限公司
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0005] The present application provides a communication data link fusion method, device, and computer-readable storage medium to solve the problem of excessive dependence on the reliability of a single communication channel when application data is transmitted through different data buses in aviation communication in the prior art. High, when a single communication channel failure occurs, it is easy to spread and cause system communication failure, causing irreparable losses

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  • Communication data link fusion method and device and computer readable storage medium
  • Communication data link fusion method and device and computer readable storage medium
  • Communication data link fusion method and device and computer readable storage medium

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Embodiment Construction

[0049] It should be understood that the specific embodiments described here are only used to explain the present application, and are not intended to limit the present application.

[0050] In the subsequent description, suffixes such as 'module', 'part' or 'unit' applied to denote elements are only for facilitating the description of the present application and have no specific meaning by themselves. Therefore, 'module', 'part' or 'unit' may be mixedly used.

[0051] see figure 1 , which is an aeronautical communication system architecture for implementing various embodiments of the present application. The architecture of the communication network system may include: electromechanical system, electromechanical electronic system, control / mission system, and avionics system.

[0052] The electromechanical system is the necessary and basic condition to ensure the performance of various functions of the aircraft. It includes a number of different electromechanical electronic s...

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PUM

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Abstract

The invention discloses a communication data link fusion method and device and a computer readable storage medium, and belongs to the technical field of aviation communication. The method comprises the following steps: monitoring communication data of a communication terminal; when to-be-sent communication data is monitored, obtaining channel states of all communication links, wherein one communication link is selected as a sending channel according to the channel states of all the communication links, and the channel states comprise the link connection state, the link utilization rate and the link delay; and sending the communication data to be sent by using the selected communication link. By adopting the method and the device, the dependence on the stability of a single channel is reduced, the realization of standardization of a system communication software interface is facilitated, the consistency is improved, and meanwhile, the portability of application software is also improved.

Description

technical field [0001] The present application relates to the technical field of aeronautical communication, in particular to an aeronautical communication data link fusion method, device and computer-readable storage medium. Background technique [0002] The control system, electromechanical system and avionics system are integrated in all kinds of aviation aircraft at present, and the application data between the control system and the electromechanical system and avionics system are transmitted through different data buses, such as 1553B bus, 1394B bus, etc. [0003] In the existing technology, when the application data is transmitted through different data buses, the reliability of the single communication channel is too high. When a single communication channel fails, it is easy to spread and cause system communication failure, resulting in irreparable losses. [0004] Therefore, it is necessary to provide a highly reliable data link fusion method, device and computer-r...

Claims

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Application Information

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IPC IPC(8): H04L12/40
CPCH04L12/40189H04L12/40006H04L2012/4028
Inventor 不公告发明人
Owner 西安怀智电子科技有限公司