Safety assessment methods for avionics software system

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dc.contributor.advisor Jia, Huamin
dc.contributor.advisor Madani, Irfan
dc.contributor.author Mao, Jiawen
dc.date.accessioned 2019-07-12T11:19:54Z
dc.date.available 2019-07-12T11:19:54Z
dc.date.issued 2017-11
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/14339
dc.description.abstract Nowadays, the avionics software has been becoming more and more critical for both civil and military aircraft. However, the software may become crazy sometimes and may cause the catastrophic result if any failure in software. Therefore, the software safety assessment is not only crucial to the specific software, but also for the system and aircraft. Although there are some industry standards as guidelines for development of software system, applications of these standards to practical software systems are still challenged and hard to operate in practice. This thesis tries to solve this problem. After analyses and summaries of the system safety assessment process and existing software safety assessment process in different fields, research wants to propose the systematic and comprehensive software safety assessment process and method for avionics software. The thesis presents the research process, and proposes one suitable avionics software safety assessment process. Meanwhile, thesis uses a real functional block in flight management system as a case study, and then conducts the software safety requirement assessment based on the proposed software safety assessment method. After analysis the result of case study, this proposed software safety assessment process and methods can quickly and correctly identify the software design errors. So, this analysis can use to prove the feasibility and validity of this proposed software safety assessment process and methods, which will help engineers modify every software design errors at the early stage in order to guarantee the software safety. en_UK
dc.language.iso en en_UK
dc.rights © Cranfield University, 2015. All rights reserved. No part of this publication may be reproduced without the written permission of the copyright holder.
dc.subject Software safety en_UK
dc.subject software development process en_UK
dc.subject software safety assessment process en_UK
dc.subject DO-178C en_UK
dc.subject ARP4754A en_UK
dc.subject functional hazard assessment en_UK
dc.subject fault tree analysis en_UK
dc.subject failure mode and effects analysis en_UK
dc.subject formal method en_UK
dc.subject NuSMV en_UK
dc.title Safety assessment methods for avionics software system en_UK
dc.type Thesis en_UK


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