Abstract In this paper, a prescribed performance integral sliding mode control (ISMC) algorithm is proposed to realize high precision and rapid response for an inertial reference unit (IRU). To ensure rapid response, a tracking differentiator (TD) is introduced to arrange a transition process for a desired signal. Tracking error is limited within two prescribed performance function (PPF) bounds to improve transient performance of the IRU. By a prescribed performance error transformation, an error transformation system is established to transform the original constrained system into an equivalent unconstrained one for the IRU. A prescribed performance integral sliding mode controller is designed for the error transformation system to ensure stead-state accuracy. Stability of the prescribed performance ISMC algorithm is proved by a Lyapunov method. Comparative experiments are given to verify effectiveness and robustness of the prescribed performance ISMC algorithm for the IRU.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Research on inertial reference units prescribed performance integral sliding mode angle control


    Beteiligte:
    Zhao, Ling (Autor:in) / He, Minghui (Autor:in) / Cao, Xinyue (Autor:in)

    Erschienen in:

    Advances in Space Research ; 71 , 10 ; 4210-4221


    Erscheinungsdatum :

    2023-01-02


    Format / Umfang :

    12 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






    Integral Global Sliding Mode Guidance for Impact Angle Control

    He, Shaoming / Lin, Defu / Wang, Jiang | IEEE | 2019


    Impact Time Constrained Sliding Mode Guidance with Prescribed Performance

    Majumder, Kakoli / Kumar, Shashi Ranjan | TIBKAT | 2023


    Impact Time Constrained Sliding Mode Guidance with Prescribed Performance

    Majumder, Kakoli / Kumar, Shashi Ranjan | AIAA | 2023