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    Titel :

    Flight Testing of a Gain-Scheduled Stability and Control Augmentation System for a Quad-Tilt-Wing UAV (AIAA 2016-0084)


    Beteiligte:
    Totoki, Hironori (Autor:in) / Ochi, Yoshimasa (Autor:in) / Sato, Masayuki (Autor:in) / Muraoka, Koji (Autor:in)

    Kongress:

    Guidance, navigation and control (Conference)



    Erscheinungsdatum :

    01.01.2016


    Format / Umfang :

    10 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



    Flight Testing of a Gain-Scheduled Stability and Control Augmentation System for a Quad-Tilt-Wing UAV

    Totoki, Hironori / Ochi, Yoshimasa / Sato, Masayuki et al. | AIAA | 2016


    Design of Gain Scheduled Stability and Control Augmentation System for Quad-Tilt-Wing UAV (AIAA 2015-0606)

    Totoki, Hironori / Ochi, Yoshimasa / Sato, Masayuki et al. | British Library Conference Proceedings | 2015


    Design of Gain Scheduled Stability and Control Augmentation System for Quad-Tilt-Wing UAV

    Totoki, Hironori / Ochi, Yoshimasa / Sato, Masayuki et al. | AIAA | 2015


    Design of flight control system for quad tilt-wing UAV

    Mikami, Takahito / Uchiyama, Kenji | IEEE | 2015


    Flight Test Verification of Flight Controller for Quad Tilt Wing Unmanned Aerial Vehicle (AIAA 2013-5100)

    Sato, M. / Muraoka, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013