The purpose of this paper is to present the topic of control computers diagnostics. They are part of an unmanned aerial vehicle (UAV) control system implemented in a modified version of MP-2 Czajka aircraft.

    Design/methodology/approach

    The algorithms were designed as a basic version of the diagnostic system. The system is open and will be developed.

    Findings

    First results show that the diagnostic system works properly. The system is easy for implementation and burdens the control computers only insignificantly.

    Research limitations/implications

    The system presented can detect only computers out of work. In its present version, it cannot detect such errors as improper calculations of control signals. After first in-flight testing, the system will be further developed.

    Practical implications

    The diagnostic system is implemented in an UAV technology demonstrator.

    Originality/value

    The designed system is the part of an UAV control system, designed for ground observation. Such technology demonstrator and flying laboratory enable different type of research in the area of aviation.


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    Titel :

    Control computers diagnostics for UAV flight control system


    Beteiligte:


    Erscheinungsdatum :

    03.05.2016


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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