The Scramjet performance of air-breathing hypersonic vehicle is highly correlated with flight height, Mach and angle of attack (AOA). The violent disturbance of the AOA can cause the engine power off. Consequently the maneuverability of hypersonic vehicle is strictly limited in the phase of cruise. A composite Control system for an air-breathing hypersonic vehicle is presented. The hypersonic vehicle has a configuration with tail control rudders and a set of deflectable wings installed nearby the center of gravity. During the phase of cruise, the precision of AOA is achieved by deflecting tail rudders, and the maneuverable acceleration command is tracked by deflecting wings. A linear quadratic (LQ) track control algorithm with integrator is used to design the composite control system. Simulation results demonstrate that the composite control system has good performance in tracking AOA and acceleration command by respective deflection in cruise.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Design of Composite Control System for an Air-Breathing Hypersonic Vehicle with Wing-Rudder Deflection



    Erschienen in:

    Erscheinungsdatum :

    2015-01-13


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Design of Composite Control System for an Air-Breathing Hypersonic Vehicle with Wing-Rudder Deflection

    Fan, Y. H. / Yu, Y. F. / Li, X. | British Library Conference Proceedings | 2015


    Fixed-wing aircraft rudder deflection angle calibrator

    JIA JUN / YU JIEYONG / FU XIAOMIN et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Rudder wing machining method and rudder wing

    WANG YUEQIANG / ZHANG YING / YOU SONGQING et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Design of Air-Breathing Hypersonic Vehicle Control System

    Hu, Zhu Bing ;Deng, Li Xin ;Li, Bing Bing | Trans Tech Publications | 2015


    Foldable air rudder of hypersonic flight vehicle

    Europäisches Patentamt | 2022

    Freier Zugriff