Civil aircraft airborne information system network security test system and method

An airborne information system and testing system technology, applied in the field of civil aircraft airborne information system network security testing system, can solve the problem of no network security testing system and the like

Pending Publication Date: 2021-09-07
XIAN AVIATION COMPUTING TECH RES INST OF AVIATION IND CORP OF CHINA
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AI Technical Summary

Problems solved by technology

[0008] In order to solve the problem that the civil aircraft airborne information system does not have a network security testing system, the present invention provides a civil aircraft airborne information system network security testing system and method

Method used

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  • Civil aircraft airborne information system network security test system and method
  • Civil aircraft airborne information system network security test system and method

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Embodiment Construction

[0061] The present invention will be further described below with reference to the accompanying drawings.

[0062] from figure 1 It can be seen that the network security test system of the aircraft airborne information system of the present invention includes the following modules:

[0063] Airborne Information System Platform Software and Basic Service Vulnerability Scanning Module 101:

[0064] The airborne information system platform software and basic service vulnerability scanning module 101 has the function of upgrading the vulnerability database; it has the platform system vulnerability scanning function of the airborne information system, including the embedded Linux operating system and the VxWorks operating system; it has the network port scanning function of the airborne information system feature that is able to identify vulnerabilities in already started services.

[0065] Airborne information system network communication protocol vulnerability fuzz testing modu...

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Abstract

The invention relates to a civil aircraft airborne information system network security test system and method, and solves the problem that a civil aircraft airborne information system does not have a network security test system. The test system comprises an airborne information system platform software and basic service vulnerability scanning module, an airborne information system network communication protocol vulnerability fuzzy test module, an airborne information system network communication protocol vulnerability penetration test module, an airborne information system network attack simulation test module, an airborne information system wireless network vulnerability test module, and a management and operation module. Through the test platform and the test method, network security robustness and vulnerability tests of the airborne information system are realized, and DO-326A network security verification specification requirements are met.

Description

technical field [0001] The invention relates to a network security testing system and method for an airborne information system of a civil aircraft. Background technique [0002] With the promotion and application of the digital aviation concept, the airborne information system is gradually developing in the direction of realizing control center, flight operation center, cabin, airport, and aircraft information sharing. [0003] The existing airborne information system can collect aircraft parameter information, audio and video information in real time and send them to the ground to realize real-time monitoring of the aircraft on the ground; it can collect and analyze aircraft equipment status information to support aircraft operation and maintenance; it can transmit electronically and loading function to realize rapid update of the aircraft system; provide electronic flight manuals and tools to reduce the workload of the flight crew; provide video data such as the cabin to ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04L29/06H04L12/26H04L29/08
CPCH04L63/1433H04L63/1441H04L63/1458H04L43/08H04L43/18H04L43/06H04L67/12
Inventor 万欣宇张双孔德歧刘绚丁玮王元勋
Owner XIAN AVIATION COMPUTING TECH RES INST OF AVIATION IND CORP OF CHINA
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