In this paper, an integrated control problem is investigated for the Air-breathing hypersonic vehicle (AHSV). The coupling dynamic model of AHSV is first provided by the Quasi One-dimensional flow theory, and the mechanical properties is analyzed. Furthermore, the integrated guidance and control laws are presented based on the proposed model and analysis result. Finally, the comparison simulation results show that the proposed integrated control approach has the better control performance against the decoupled control approach.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    An Integrated Control Approach for Air-breathing Hypersonic Vehicle


    Beteiligte:
    Li, Jiaxin (Autor:in) / Liu, Kai (Autor:in) / Wang, Yongsheng (Autor:in) / Nie, Wentian (Autor:in)


    Erscheinungsdatum :

    27.11.2020


    Format / Umfang :

    616756 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Design of Air-Breathing Hypersonic Vehicle Control System

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


    Air-Breathing Hypersonic Flight Control

    Fidan, B. / Mirmirani, M. / Ioannou, P. A. et al. | British Library Conference Proceedings | 2004



    Control-Oriented Modeling of an Air-Breathing Hypersonic Vehicle

    Jason Parker / Andrea Serrani / Stephen Yurkovich et al. | AIAA | 2007


    Analytical Modeling and Design for an Air-Breathing Hypersonic Cruise Vehicle Using an Integrated Approach

    Priyamvada, K S / Singh, Yogendra / Thakor, Nimesh et al. | AIAA | 2015