Flight simulator network communication method based on dynamic interface

A flight simulator and dynamic interface technology, applied in the field of network data communication and network communication, can solve the problems of many communication channels, inconsistent data interfaces, and low work efficiency.

Active Publication Date: 2019-03-01
JIANGXI HONGDU AVIATION IND GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In view of the above-mentioned actual situation, the technical problem solved by the present invention is to provide a flight simulator network communication method based on a dynamic interface, to solve the flight simulator maintenance work caused by many communication channels and inconsistent data interfaces in the original communication method The problem of large volume and low work efficiency

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  • Flight simulator network communication method based on dynamic interface
  • Flight simulator network communication method based on dynamic interface
  • Flight simulator network communication method based on dynamic interface

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Embodiment Construction

[0017] Combine below Figure 1~Figure 3 , clearly and completely describe the technical solution of the embodiment of the present invention, obviously, the described embodiment is only a specific embodiment of the present invention, not all embodiments.

[0018] Such as figure 1 As shown, in the communication system of the flight simulator, it is composed of a visual control computer 102, a display control / task computer 105, a flight simulation computer 103, a cockpit acquisition controller 100, a sound computer 101, a main control computer 104, etc., and is networked. Communication, data exchange communication between each computer through Ethernet.

[0019] Such as figure 2 The shown computer configures the dynamic interface text file of the required communication through the configuration data interface, and the computers of each system are configured according to the dynamic data interface text file, such as: the data acquisition controller 100 passes the corresponding ...

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Abstract

The invention provides a flight simulator network communication method based on a dynamic interface. The condition of the flight simulator network communication method based on the dynamic interface is that each system of the flight simulator performs data communication through an Ethernet. Each interface that requires communication is standardized in the same way through adopting a prescribed dynamic interface configuration and data communication network configuration; a sending end sends all data to the Ethernet using a format in a multicast mode; a receiving end receives all the data; eachsystem selects and processes required data items according to a dynamic interface configuration file; and the data of the configuration file is stored as a text file with a uniform format. The flightsimulator network communication method based on the dynamic interface is beneficial to increasing and modification of the interface, the maintenance of the system and the protection of the simulator.

Description

technical field [0001] The invention relates to the field of network communication, in particular to a dynamic interface-based flight simulator network communication method, which belongs to the technical field of network data communication. Background technique [0002] There are many devices in the flight simulator, and data communication between the various systems is required. How to communicate efficiently and uniformly is very important. Generally, the flight simulator uses Ethernet to build a network system, and the subsystems exchange data through the network, using UDP point-to-point and multicast methods, and periodic sending and blocking receiving modes. When two computers communicate through multicast, they need to add a unified multicast segment, multicast port number, and the communication interface needs to be unified; when two computers communicate through point-to-point, they need to bind the receiving end and sending end, and unify the communication interfa...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04L12/24
CPCH04L41/0803
Inventor 杨宛璐黄祖丹叶猛王云杨衍舒孙双双张志强韩立王建普吴慧钦邓铸洲
Owner JIANGXI HONGDU AVIATION IND GRP
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