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IMA (Integrated Modular Avionics) system performance degradation modeling and simulation method

A comprehensive modular, avionics system technology, applied in electrical digital data processing, special data processing applications, instruments, etc., can solve problems such as difficulties, increased maintenance objectives of avionics system depending on the situation, and many parts involved in the system, and achieve cost low cost effect

Active Publication Date: 2018-01-16
NORTHWESTERN POLYTECHNICAL UNIV
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the application of health management to airborne avionics systems is still in its infancy, especially with the characteristics of high complexity, many components involved in the system, multi-attributes, nonlinearity, etc., such as IMA, each module, function or sub-system of the system The coupling relationship between systems is tight, the transmission and impact of faults are complex, and the symptom parameters of electronic system faults are not obvious enough or are sudden changes. These factors increase the difficulty of achieving the purpose of condition-based maintenance of integrated modular avionics systems

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  • IMA (Integrated Modular Avionics) system performance degradation modeling and simulation method
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  • IMA (Integrated Modular Avionics) system performance degradation modeling and simulation method

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Embodiment Construction

[0029] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.

[0030] Step 1: The hardware composition of IMA includes Remote Data Concentrator (RDC), Common Data Network (CDN) and Common Computing Resource (CCR), avionics full-duplex communication Ethernet switch (Avionics Full-Duplex SwitchedEthernet, AFDX) as the exchange bus between electronic systems, general computing modules (general computing modules, GPM) is the core to realize each resident function, external data is collected by RDC and stored in the memory through the bus, when the function is executed GPM calls memory resources, and realizes various functions by calculating according to corresponding programs;

[0031]Step 2: As an electronic device with high coupling and high complexity, IMA is accompanied by a variety of faults in its life cycle. Among them, intermittent faults and transient faults will disappear with system operation, reset, restart...

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Abstract

The invention provides an IMA (Integrated Modular Avionics) system performance degradation modeling and simulation method, and relates to the field of aircraft avionics. The IMA system performance degradation modeling and simulation method comprises the step of regarding performance of a soft fault in a whole IMA life cycle as representation of IMA system performance degradation to accordingly build an IMA system performance degradation model. The IMA system performance degradation modeling and simulation method avoids the dilemma that data driving based modeling cannot be carried out by utilizing original data due to insufficient IMA system performance degradation, provides a new idea for the IMA performance degradation modeling and describes an IMA system performance change course by combining a resource reliability function with the fact whether soft faults such as an intermittent fault and a transient fault occurs in the whole IMA period; as the IMA system performance degradation course is expressed by a probability model, the cost is low and a foundation for condition-based maintenance is laid.

Description

technical field [0001] The invention relates to the field of aircraft avionics, in particular to a simulation method for performance degradation of an avionics system. Background technique [0002] Failure of the Integrated Modular Avionics (IMA) system infrastructure will affect all systems using this shared resource. The failure of a resource may result in the total failure, partial failure, or loss of redundancy of all applications that directly use the resource. The primary impact of a failed resource can be determined through analysis and / or testing. However, in many cases cascading failures caused by failed resources are difficult to determine. [0003] Although there is enough information to assist IMA developers in making a comprehensive safety assessment, including failure analysis of a very complex IMA system, however, several complex avionics systems (including non-ARINC653 architecture systems) are currently in service abroad. , under failure conditions, there...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
Inventor 高泽海马存宝李媛媛陈杰宋东和麟张天伟
Owner NORTHWESTERN POLYTECHNICAL UNIV
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