Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Robust Attitude Control System Design for a Distributed Propulsion Tilt-Wing UAV in Flight State Transition


    Contributors:
    Wang, Siqi (author) / Song, Bifeng (author) / He, Lei (author)

    Conference:

    Asia-Pacific international symposium



    Publication date :

    2019-01-01


    Size :

    20 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English