Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Output Feedback Variable Structure Adaptive Control Approach to Missile Autopilot Design



    Conference:

    AIAA Guidance, Navigation, and Control Conference ; 2011 ; Portland, OR



    Publication date :

    2011-01-01


    Size :

    18 pages


    Remarks:

    Includes bibliographical references and index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    ICAS2016_0474: MISSILE AUTOPILOT DESIGN USING CONTRACTION THEORY-BASED OUTPUT FEEDBACK CONTROL

    Kwon, H.-H. / Choi, H.-L. | British Library Conference Proceedings | 2016



    A Robust Adaptive Nonlinear Control Approach to Missile Autopilot Design

    Kim, S. H. / Song, C. H. / International Federation of Automatic Control | British Library Conference Proceedings | 1999


    Discrete Variable Structure Controller for Missile Autopilot

    Powly, A. A. / Bhat, M. S. / Centre for Electronics Design and Technology of India, Calicut | British Library Conference Proceedings | 2002