An approach to the development of a hybrid high-speed rotary-wing aircraft reconfiguration system is considered. The stages of system concept development, justification of its functionality, architecture formation and technical appearance are considered.


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    Title :

    Concept of Hybrid Reconfiguration of High-speed Rotary-wing Aircraft Flight Control System




    Publication date :

    2022-04-14


    Size :

    1471722 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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