Functional Safety Oriented Integrated Design for Avionics System Resources: Multilayer Weighted Networks Model

Chu, Jiayun; Jiao, Jian; Zhao, Tingdi

doi:10.1109/rams.2019.8768989

Cited by 2 publications

(1 citation statement)

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“…In recent years, with the development of aerospace technology, the data processed by spacecraft are trending towards diversity, complexity, and standard internationalization [1,2]. In order to adapt to the development trend of space data communication technology, selecting a suitable forward design method for the aerospace electronic communication system has become a top priority [3,4].…”

Section: Introductionmentioning

confidence: 99%

Forward Design Method of Avionics System Based on Communication

Peng

2021

Mobile Information Systems

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With the rapid development of computer technology, electronic technology, and control technology, communication-based avionics systems can provide greater potential for the improvement of aircraft combat capabilities. Moreover, during the flight, passengers have an increasing demand for space communications. How to provide passengers with a communication-based aerospace electronic system that is indistinguishable from the ground during the flight is a problem that needs to be solved urgently. The research on the forward design method of this system has been highly valued by experts at home and abroad. This article is a communication-based forward design method for avionics systems. Based on the development of aerospace data communication technology, this article discusses the advantages of the application of the CCSDS (Consultative Committee for Space Data Systems) protocol in the design of aerospace electronic communication systems. This research designs the technical scheme of the entire aerospace communication electronic system and refers to the relevant CCSDS protocol to complete the design of the distributor’s fast transmission telemetry package and the distributor’s slow transmission telemetry package. This article introduces the two existing architectures of the integrated avionics system, compares and analyzes them, and then elaborates the integrated avionics system architecture based on trusted computing and the trust chain transfer mechanism. The experimental results show that the method designed in this paper uses the NBSP basic protocol in an aeronautical communication environment with a nesting depth of 2 s. When the data transmission delay is 2 s, the NBSP scheme is 0.9 and the NERON scheme is 0.4. This shows that the design method of this study is able to meet the requirements of the system and technical indicators.

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Section: Introductionmentioning

confidence: 99%