Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Impact-Point-Based Guidance of a Spinning Artillery Rocket Using Canard Cyclic Control


    Contributors:
    Yang, Shu (author)

    Published in:

    Publication date :

    2020-10-01




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    AERODYNAMIC CHARACTERIZATION OF A CANARD GUIDED ARTILLERY PROJECTILE

    Su, Wei-Jen / Wilson, Curtis / Farina, Tony et al. | AIAA | 2007



    AERODYNAMIC CHARACTERIZATION OF A CANARD GUIDED ARTILLERY PROJECTILE AIAA Paper

    Su, W. / Wilson, C. / Farina, T. et al. | British Library Conference Proceedings | 2007


    Attitude Guidance and Control for a Spinning, Asymmetrical Rocket Payload

    Creagh, M. / Defence Science and Technology Organisation (Australia); Royal Aeronautical Society; Institution of Engineers Australia | British Library Conference Proceedings | 2011


    Design and Aerodynamic Characterization of Canard Guided Fuze for Dual-Spin Artillery Projectiles

    Jaiswal, Rahul / Kothari, Mangal / Abhishek, Abhishek | AIAA | 2024