In this article, the proposed method first evaluates the effects on aerodynamic force caused by flight velocity and angular velocity of the parafoil delivery system and performs an active disturbance rejection control in the horizontal direction. Moreover, a glide-ratio controller is designed based on the characteristics of the symmetrical flap deflection. For resisting its disturbance, a feedforward compensation unit is designed with the glide-ratio controller. The performance is effectively validated through hardware-in-the-loop simulation.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Accurate Homing of Parafoil Delivery Systems Based Glide-Ratio Control


    Contributors:
    Sun, Hao (author) / Sun, Qinglin (author) / Zeng, Xianyi (author) / Luo, Shuzhen (author) / Wu, Wannan (author) / Chen, Zengqiang (author)


    Publication date :

    2020-06-01


    Size :

    5905325 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Coordinated Payload Delivery using High Glide Parafoil Systems

    Kaminer, Isaac / Yakimenko, Oleg / Pascoal, Antonio | AIAA | 2005



    Parafoil Glide Slope Control Using Canopy Spoilers

    Gavrilovski, A. / Ward, M. / Costello, M. et al. | British Library Conference Proceedings | 2011


    Parafoil Glide Slope Control Using Canopy Spoilers

    Gavrilovski, Alek / Ward, Michael / Costello, Mark | AIAA | 2011


    Adaptive Glide Slope Control for Parafoil and Payload Aircraft

    Ward, Michael / Costello, Mark | AIAA | 2013