Helicopters are theoretically unstable aircraft, but they are widely used in many fields, because of their high maneuverability. The goal of this paper is to build two different real-time control systems for vehicle stabilization and for control to track the desired points or paths. This control system was designed in Matlab/Simulink to control a single RC coaxial helicopter. In the system, four pilot inputs (the desired thrust and the desired roll, pitch, and yaw rates) were calculated from LQR and H∞ control system, and those signals were sent to the RC helicopter's microcontroller using the RC transmitter and receiver.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Modeling of real-time flight control system for small coaxial helicopter


    Beteiligte:
    Lee, Seong-Jin (Autor:in)


    Erscheinungsdatum :

    2014-03-01


    Format / Umfang :

    1641858 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Small-scale coaxial armed unmanned helicopter flight dynamics investigation

    Wu, Meiliwen / Chen, Ming / Wang, Fang et al. | AIAA | 2016


    Small-scale Coaxial Armed Unmanned Helicopter Flight Dynamics Investigation (AIAA 2016-3377)

    Wu, Meiliwen / Chen, Ming / Wang, Fang et al. | British Library Conference Proceedings | 2016


    CONTROL SYSTEM OF COAXIAL HELICOPTER

    GUBAREV BORIS ANATOLEVICH / MIKHAJLOV ALEKSANDR VLADIMIROVICH | Europäisches Patentamt | 2017

    Freier Zugriff

    Robust Control and Flight Test of a Coaxial Helicopter UAV

    Jeaong, Hoijo / Suk, Jinyoung / Kim, Seungkeun | TIBKAT | 2023


    Robust Control and Flight Test of a Coaxial Helicopter UAV

    Jeaong, Hoijo / Suk, Jinyoung / Kim, Seungkeun | AIAA | 2023