New types of aircrafts embody all the most advanced technical and technological solutions. Architecting commercial aircraft has been always challenging due to the complexity of the product (Li et al. in Architecting commercial aircraft with a Domain Specific Language extended from SysML, 2021). The introduction of new technologies is associated with risks in terms of reliability and resiliency. Using traditional design methods in the development of an aircraft, it is impossible to determine all possible scenarios for the aircraft functioning and its systems itself and, as a consequence, to analyze all possible risky states of the aircraft. Each aircraft must meet the requirements that were established to it. This work is devoted to the processes of establishing and verifying these requirements. The principles and methods of integration, verification and validation of technical systems are considered in detail, the importance of these criteria is assessed. This work aims to cr prerequisites for the development of an automatic algorithm for verification program and construction of a test certification basis for the aircraft as a whole and its subsystems in particular.


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    Titel :

    Methodology for Formation of an Optimized Verification, Validation and Integration Program for an Aircraft Based on Models of Its Architecture


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Jing, Zhongliang (Herausgeber:in) / Strelets, Dmitry (Herausgeber:in) / Konstantinov, I. A. (Autor:in) / Kaigorodova, V. A. (Autor:in) / Shavelkin, D. S. (Autor:in)

    Kongress:

    International Conference on Aerospace System Science and Engineering ; 2021 July 14, 2021 - July 16, 2021



    Erscheinungsdatum :

    2022-07-09


    Format / Umfang :

    7 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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