Abstract Guidance law of a homing missile is implemented using an extended high gain observer without the model assumptions on target maneuvers. First, for a class of multi-input–multi-output nonlinear systems, extended high-gain observers are used for output feedback control with partial practical stabilization. Then the method is applied to the guidance law implementation of a homing missile with bearing only measurement. Simulation results show satisfactory performance.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Guidance law implementation with performance recovery using an extended high-gain observer


    Beteiligte:
    Ma, Kemao (Autor:in) / Khalil, Hassan K. (Autor:in) / Yao, Yu (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2011-11-03


    Format / Umfang :

    10 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Extended differential geometric guidance law with extended state observer

    Huang, Jingshuai / Zhang, Hongbo / Tang, Guojian et al. | IEEE | 2017


    Finite-time convergent sliding-mode guidance law based on Extended-State-Observer

    Zhang, Denghui / Chao, Tao / Wang, Songyan et al. | IEEE | 2016


    Recoverable rocket power landing phase guidance method based on extended state observer

    ZHANG RAN / CHEN XINGLUN / XUE WENCHAO et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Robust Guidance Law with L2 Gain Performance

    Zhou, Di | Online Contents | 2001