Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Output Feedback Variable Structure Adaptive Control Approach to Missile Autopilot Design


    Beteiligte:
    Lee, Keum (Autor:in) / Singh, Sahjendra (Autor:in)

    Kongress:

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



    Erscheinungsdatum :

    01.01.2011




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Output Feedback Variable Structure Adaptive Control Approach to Missile Autopilot Design

    Lee, K. / Singh, S. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011


    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