Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

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


    Contributors:

    Conference:

    Guidance; Navigation; Control ; 2015 ; Kissimmee, FL



    Publication date :

    2015-01-01


    Size :

    17 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



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

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


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

    Totoki, Hironori / Ochi, Yoshimasa / Sato, Masayuki et al. | British Library Conference Proceedings | 2016


    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


    Towards gain-scheduled Hinfinity control design for a tilt-wing aircraft

    Mix, D.R. / Koenig, J.S. / Linda, K.M. et al. | Tema Archive | 2004


    CONTROL AUGMENTATION SYSTEM DESIGN FOR THE QUAD TILT-WING UAV VIA H□‡ STRUCTURE WITH GWO

    Deveerasetty, K. / Oka, K. / Harada, A. | British Library Conference Proceedings | 2022