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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    Title :

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


    Contributors:
    An, Hao (author) / Wang, Changhong (author)

    Published in:

    Publication date :

    2022-01-01




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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