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An Automatic Test System for Avionics System

An automatic test system and avionics system technology, applied in general control systems, control/regulation systems, instruments, etc., can solve problems such as incomplete judgment, wrong automatic data judgment results, and impact on testing.

Active Publication Date: 2016-04-06
SHENYANG HANGSHENG TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although this kind of judgment improves the test efficiency to a certain extent, because it is only a judgment on a certain time point, if the data flow changes dynamically during an operation, it can only judge the correctness of the last shot of data, resulting in judgment Incomplete
Moreover, the operation of each simulator and exciter needs to be carried out manually at present. If the timing of the operation does not meet the requirements, or there is a little operation error, it will often cause the data to be automatically judged as wrong, which will affect the test.

Method used

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  • An Automatic Test System for Avionics System
  • An Automatic Test System for Avionics System
  • An Automatic Test System for Avionics System

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0050] The automatic test system of the avionics system described in the present embodiment is connected to the tested avionics system 1, and is characterized in that: the automatic test system of the avionics system is composed as follows: aircraft flight simulator 2, external object simulation 3, conduction actuator 4, non-aviation system simulator 5, test console 6, each target simulator 7, comprehensive test system 8, judgment and recording system 9, prompt system 10; where:

[0051] The airborne flight simulator 2 that provides simulated flight parameters for the avionics system is connected with the inertial navigation equipment (11) and the air data computer 12 of the avionics system, and receives commands such as power supply, heating, and external store launch of the avionics system , and the external storage simulator 3 that simulates the status of the external storage at each storage point is connected with the avionics system 1 to provide a simulated radio environme...

Embodiment 2

[0087] See attached figure 2 , the avionics system 1 under test includes a control system, a remote terminal 1 , and a remote terminal 2 . The radar target simulator is connected with the remote terminal 2 through a radio frequency cable; the remote terminal 2 is provided with simulated target data; the carrier flight simulator is connected with the remote terminal 1 through an ARINC429 bus connection, and the remote terminal 1 is provided with simulated carrier flight parameters; The remote terminal 1, the remote terminal 2 and the control and comprehensive test system are connected through the bus, so that the comprehensive test system collects the data of the avionics system under test; meanwhile, the radar target simulator, the aircraft flight simulator 2, the judgment and recording system 9, The comprehensive test system 8, the test console 6, and the prompt system 10 are connected to the real-time network switch 13 through the fiber optic channel, so that the entire aut...

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Abstract

The invention discloses an automatic testing system of an avionics system. The automatic testing system of the avionics system is connected to the tested avionics system (1). The automatic testing system of the avionics system is composed of an aerial carrier flight emulator (2), an external store simulator (3), a conducting exciter (4), a non-avionics system emulator (5), a testing general control platform (6), an each-target simulator (7), an integrated test system (8), a judging and recording system (9) and a prompting system (10). Real-time network connection is conducted on testing auxiliary devices such as the external store simulator, the each-target simulator, the conducting exciter and the aerial carrier flight emulator through the automatic testing system of the avionics system. Each testing auxiliary device is automatically controlled to generate a signal with a strict time series in each inspection step and judgment about data correctness is achieved through a method capable of being called searching type automatic judgment under the control of the testing general control platform so that automatic testing can be achieved. According to the automatic testing system of the avionics system, the efficiency of avionics system testing is effectively improved and the comprehensiveness of automatic testing is improved to a great extent.

Description

technical field [0001] The invention relates to the technical field of structural design and application of a test system for an avionics system, and in particular provides an automatic test system for an avionics system. Background technique [0002] At present, in the integration test of the avionics system, the judgment of the data flow is made by manual judgment or static automatic judgment. Manual judgment is time-consuming and labor-intensive, which not only delays the progress of product delivery, but also may lead to missed judgments and misjudgments. The so-called static automatic judgment is to control the test system to collect the data flow on the current bus after the operation of a certain inspection step, and automatically judge the correctness of all data at this collection time point. The judgment method described in "Test System", patent number: ZL201220652188.4. Although this kind of judgment improves the test efficiency to a certain extent, because it i...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B17/02
Inventor 邹德儒刘文旭张宇孟凡石
Owner SHENYANG HANGSHENG TECH CO LTD
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