The problem of estimating the angular rate of a satellite is considered. A nonlinear observer based on the state-dependent Riccati equation method is proposed. A sufficient stability condition for the convergence of the estimation error is presented. This condition is related to a state-dependent algebraic Riccati equation. The Riccati equation is derived by transforming nonlinear error dynamics into a Lipschitz nonlinearity. Observer gains are obtained from this state-dependent algebraic Riccati equation. Numerical simulations are presented to demonstrate the proposed method.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Observer design for satellite angular rate estimation using the state-dependent riccati equation method


    Beteiligte:
    Jaehyun Jin, (Autor:in)


    Erscheinungsdatum :

    2015-07-01


    Format / Umfang :

    986830 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Exponential nonlinear observer based on the differential state-dependent Riccati equation

    Beikzadeh, H. / Taghirad, H. D. | British Library Online Contents | 2012


    State-Dependent Riccati Equation Filter

    Zarchan, Paul / Musoff, Howard | AIAA | 2015