Among flourishing control studies on air-breathing hypersonic vehicles (AHVs), actuator characteristics have not been fully accommodated. This study gives a comprehensive consideration to physical actuators of AHVs that have transient dynamics and magnitude/rate constraints by introducing an adaptive reference governor and an optimizing allocation module. After implementing a tangent tracking error-based back-stepping design, the derived control algorithm is low-complexity, whose effectiveness is verified by simulations.


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    Titel :

    Optimizing Allocation-Enhanced Hypersonic Flight Control with Actuator Dynamics and Constraints


    Beteiligte:
    An, Hao (Autor:in) / Wang, Changhong (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.01.2022




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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