The six-degree-of-freedom control of hypersonic flight vehicles (HFVs) faces great challenges due to complex aerodynamics, inherent couplings, and multiple constraints. This article investigates the six-degree-of-freedom guidance and attitude control problem for unpowered gliding HFVs. The guidance loop is based on the predictor–corrector method with three improvements: intelligent prediction acceleration, path constraint accommodation, and no-fly zone circumvention. To quickly respond to guidance commands, three attitude channels (i.e., roll, pitch, and yaw) are completely decoupled by nonlinear dynamic inverse, based on which a high-performance low-complexity attitude controller is proposed. This benefits from the appropriate integration of barrier function and sliding-mode control, while design conditions of three alternative performances (i.e., asymptotic, exponential, and preset-time convergences) are discussed. Servo dynamics and physical constraints of aerodynamic control surfaces are also well handled.


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    Titel :

    Six-Degree-of-Freedom Intelligent Control of Hypersonic Flight Vehicle


    Beteiligte:
    An, Hao (Autor:in) / Wang, Yiming (Autor:in) / Zhong, Xinyu (Autor:in) / Ye, Yongfeng (Autor:in)


    Erscheinungsdatum :

    01.08.2025


    Format / Umfang :

    7454731 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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