A variable-structure control system designed to enable a fuselage-heavy airplane to recover from spin has been demonstrated in a hand-launched, instrumented model glider airplane. Variable-structure control is a high-speed switching feedback control technique that has been developed for control of nonlinear dynamic systems.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Variable-Structure Control of a Model Glider Airplane


    Contributors:


    Publication date :

    2008-07-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Flight instructor : airplane, rotorcraft, glider, instrument

    USA, Flight Standards Service | SLUB | 1973


    Multi-Modal Flying Airplane and Underwater Glider

    EDWARDS DANIEL J / BOOK JEFFREY W / YOUNG TRENT et al. | European Patent Office | 2019

    Free access

    Multi-modal flying airplane and underwater glider

    EDWARDS DANIEL J / BOOK JEFFREY W / YOUNG TRENT et al. | European Patent Office | 2020

    Free access

    Variable Structure Control of a Hand-Launched Glider

    Anderson, Mark / Waszak, Martin | AIAA | 2005


    Motion Control of Autonomous Underwater Glider with Sliding Variable Structure Control

    You, Yue / Zhang, Ping / Feng, Jingxiang et al. | Springer Verlag | 2022