Design of Embedded Architecture for Integrated Diagnostics in Avionics Domain

The resent paper introduces a multi-level decision-making approach for design of optimal embedded integrated diagnostic architecture that combines maintenance decisions at the k-levels of system architecture and integration with health and usage monitoring systems (HUMS) mechanisms for achieving efficient system for level maintenance and lowering life-cycle cost of Integrated Modular Avionics (IMA). HUMS can be implemented in software or directly on an integrated circuit. The effectiveness of such an approach is investigated through the optimization of embedded HUMS architecture for known reliability and economic dependence during life cycle of IMA.

• Record URL:
  https://doi.org/10.1016/j.proeng.2017.01.081
• Record URL:
  http://www.sciencedirect.com/science/article/pii/S1877705817300814
• Availability:
  • Find a library where document is available. Order URL: http://worldcat.org/issn/18777058
• Supplemental Notes:
  • © 2017 Igor Kabashkin. Published by Elsevier Ltd.
• Authors:
  • Kabashkin, Igor
• Conference:
  • 16th International Scientific Conference Reliability and Statistics in Transportation and Communication (RelStat-2016)
  • Location: Riga , Latvia
  • Date: 2016-10-19 to 2016-10-22
• Publication Date: 2017

Language

• English

Media Info

• Media Type: Digital/other
• Features: Figures; References; Tables;
• Pagination: pp 419-426
• Serial:
  • Procedia Engineering
  • Volume: 178
  • Issue Number: 0
  • Publisher: Elsevier
  • ISSN: 1877-7058
  • Serial URL: http://www.sciencedirect.com/science/journal/18777058
• Publication flags:

  Open Access (libre)

Subject/Index Terms

• TRT Terms: Aeronautical engineering; Avionics; Decision making; Diagnostic tests; Life cycle costing; Maintenance; Monitoring; System architecture
• Subject Areas: Aviation; Design; Maintenance and Preservation;

Filing Info

• Accession Number: 01632792
• Record Type: Publication
• Files: TRIS
• Created Date: Mar 9 2017 1:52PM