Avionics test system

A test system and avionics technology, applied in the direction of testing electrical devices, measuring electricity, measuring devices, etc. in transportation

Pending Publication Date: 2019-08-23
BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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However, in the actual use process, there are i

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Examples

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Embodiment 1

[0035] figure 1 It is a structural block diagram of the avionics test system provided in the first embodiment of the present application. The embodiment of the present application is applicable to the case of testing the avionics system, and the system can be implemented by software and / or hardware.

[0036] Such as figure 1 As shown, the avionics test system includes: a device under test 110, a test platform 120, and a signal transmission channel control device 130. The signal transmission channel control device 130 is connected to the device under test 110 through the device under test interface 131 and passes the test. The platform interface 132 is connected to the test platform 120, where

[0037] The signal transmission channel control device 130 includes:

[0038] At least two wiring matrix boards 133, wherein each wiring matrix board 133 is provided with a loopback connector, and the loopback connector is used to connect the at least two wiring matrix boards;

[0039] Each wiri...

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Abstract

The embodiment of the present application discloses an avionics test system. The device comprises a tested device, a test platform, and a signal transmission channel control device. The signal transmission channel control device is connected with the tested device through a tested device interface and is connected with the test platform through a test platform interface, the signal transmission channel control device comprises at least two wiring matrix boards, a resource connector, and a signal transmission channel control unit, wherein the wiring matrix board is provided with a loopback connector for connecting the at least two wiring matrix boards, the resource connector is connected with the test platform interface; the wiring matrix board is connected with the tested device interfacethrough a ribbon cable, the signal transmission channel control unit is used for controlling a signal transmission channel; and the test platform is used for providing test resources to implement functional test of the tested device. By adopting the above technical scheme, the signal transmission channel can be flexibly controlled, meanwhile, as the control operation is simple, low-level errors such as operation errors and the like can be prevented from influencing the accuracy of the test result.

Description

Technical field [0001] The embodiments of the application relate to the technical field of avionics testing, and in particular to an avionics testing system. Background technique [0002] Airborne avionics equipment mainly includes communication, navigation, display, cockpit entertainment and other equipment. It completes aircraft and ground communication, navigation, information processing and control. It is the core and most important equipment of the aircraft and directly affects the advanced level and comprehensive capabilities of the aircraft. . The airborne avionics equipment is composed of multiple functional units, and there are many problems to be tested, the test process is complicated, and the test is difficult. There are hundreds of test channels and hundreds or even thousands of test ports. The test channels are complex, with multiple channels and multiple interfaces, making flexible control difficult. [0003] In the traditional test scheme, there are mainly two sol...

Claims

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Application Information

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IPC IPC(8): G01R31/00
CPCG01R31/008
Inventor 唐剑谭文韬朱少凡王世元汪澔
Owner BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC
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