Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    AN INTEGRATED FLEXIBLE AIRCRAFT MODEL FOR OPTIMAL CONTROL SURFACE SCHEDULING OF MANOEUVRE LOAD ALLEVIATION AND WING SHAPE CONTROL FUNCTIONS


    Contributors:
    Kier, T. (author)

    Conference:

    International Forum on Aeroelasticity and Structural Dynamics ; 19. ; 2022 ; Madrid



    Publication date :

    2023


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



    Performance Optimizing Gust Load Alleviation Control of Flexible Wing Aircraft

    Hashemi, Kelley E. / Nguyen, Nhan T. / Drew, Michael C. et al. | AIAA | 2018


    Aircraft wing load alleviation device and aircraft wing load alleviation method

    HIRABAYASHI DAISUKE / AKIBA KOUSABUROU | European Patent Office | 2020

    Free access

    AIRCRAFT WING LOAD ALLEVIATION DEVICE AND AIRCRAFT WING LOAD ALLEVIATION METHOD

    HIRABAYASHI DAISUKE / AKIBA KOUSABUROU | European Patent Office | 2019

    Free access


    Design of a Flying Demonstrator Wing for Manoeuvre Load Alleviation with Cruise Shape Constraint (AIAA 2018-2153)

    Sodja, Jurij / Werter, Noud / De Breuker, Roeland | British Library Conference Proceedings | 2018