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Non-functional Attribute Modeling and Verification Method for Integrated Modular Avionics System

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Abstract

Aiming at the shortcomings of standardized design and early verification of integrated modular avionics systems, this paper proposes a non-functional attribute modeling and verification method for integrated modular avionics system. We extract an architecture-centric design process for integrated modular avionics system, propose automatic transformation from SysML-based functional models to AADL-based architecture models, design AADL-Hazard sub-language, put forward AADL-based scheduling analysis for ARINC 653 system and safety analysis based on FMECA. Finally, aviation air compressor control system is chosen as a case to verify the correctness and feasibility of the method proposed in this paper. The method in this paper improves the AADL’s ability to model and verify for integrated modular avionics system, help engineersuse standardized design, multi-dimensional analysis methods in the early stage of the product, and reduces later product rework.

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References

  1. Baldonado, M., Chang, C.-C.K., Gravano, L., Paepcke, A.: The Stanford digital library metadata architecture. Int. J. Digit. Libr.1, 108–121 (1997)

    Article  Google Scholar 

  2. Aeronautical Radio Incorporated: Avionics Application Software Standard Interface (2013)

    Google Scholar 

  3. Delange, J., Feiler, P., Gluch, D.P.: AADL Fault Modeling and Analysis Within an ARP4761 Safety Assessment. Software Engineering Institute Carnegie Mellon University (2014)

    Google Scholar 

  4. Chilenski, J.J., Kerstetter, M.S.: SAVI AFE 61S1 Report. Aerospace Vehicle Systems Institute (2015)

    Google Scholar 

  5. SAE International Group: SAE Architecture Analysis and Design Language (AADL) Annex Volume 2: Annex F: ARINC653 Annex (2011)

    Google Scholar 

  6. SAE International Group: SAE Architecture Analysis and Design Language (AADL) Annex Volume 3: Annex E: Error Model Annex (2013)

    Google Scholar 

  7. Singhoff, F., Legrand, J., Nana, L., Marcé, L.: Cheddar: A Flexible Real Time Scheduling Framework. University of Brest

    Google Scholar 

  8. OMG: Systems Modeling Language (2016).https://www.omg.org/spec/SysML/20161101

  9. Feiler, P., Rugina, A.: Dependability Modeling with the Architecture Analysis & Design Language (AADL). Software Engineering Institute (2007, July)

    Google Scholar 

  10. Robati, T., El Kouhen, A., Gherbi, A., Hamadou, S., Mullins, J.: An Extension for AADL to Model Mixed-Criticality Avionic Systems Deployed on IMA Architectures with TTEthernet. ACVI at MoDELS (2014)

    Google Scholar 

  11. Lafaye, M., Gatti, M., Faura, D., Pautet, L.: Model driven early exploration of IMA execution platform. In: Digital Avionics Systems Conference (DASC), IEEE/AIAA 30th (2010)

    Google Scholar 

  12. SAE International: ARP-5580—Recommended Failure Modes and Effects Analysis (FMEA) Practices for Non-automobile Applications. SAE International (2001)

    Google Scholar 

  13. SAE International: ARP-4761—Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne Systems and Equipment. SAE International (1996)

    Google Scholar 

  14. Yang, Z., Hu, K., Ma, D., Bodeveix, J.-P., Pi, L., Talpin, J.-P.: From AADL to timed abstract state machines: a verified model transformation. J. Syst. Softw. (2014)

    Google Scholar 

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Authors and Affiliations

  1. Aviation Key Laboratory of Science and Technology on Airborne and Missileborne Computer, School of Computer Science and Technology, Computing Technique Research Institute, AVIC, Nanjing University of Aeronautics and Astronautics, Room 15, JinYe2 Road, Xi’an, Shaanxi, China

    Peng Guo, Na Wu, Yahui Li & Ning Hu

  2. Computing Technique Research Institute, AVIC, Room 15, JinYe2 Road, Xi’an, Shaanxi, China

    Feiyang Liu

Authors
  1. Peng Guo

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  2. Feiyang Liu

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  3. Na Wu

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  4. Yahui Li

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  5. Ning Hu

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Corresponding author

Correspondence toPeng Guo.

Editor information

Editors and Affiliations

  1. CESAMES, Paris, France

    Daniel Krob

  2. Tsinhua University, Beijing, China

    Lefei Li

  3. Chinese Society for Aeronautics, Beijing, China

    Junchen Yao

  4. CSSC Systems Engineering Research Institute, Beijing, China

    Hongjun Zhang

  5. Tsinhua University, Beijing, China

    Xinguo Zhang

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© 2021 The Author(s), under exclusive license to Springer Nature Switzerland AG

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Guo, P., Liu, F., Wu, N., Li, Y., Hu, N. (2021). Non-functional Attribute Modeling and Verification Method for Integrated Modular Avionics System. In: Krob, D., Li, L., Yao, J., Zhang, H., Zhang, X. (eds) Complex Systems Design & Management . Springer, Cham. https://doi.org/10.1007/978-3-030-73539-5_25

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JPY 19447
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Softcover Book
JPY 24309
Price includes VAT (Japan)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
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Hardcover Book
JPY 24309
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Purchases are for personal use only


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