Facing the difficulty of flight dynamics modeling about flexible hypersonic flight vehicles, from view on the Lagrange’s equations based on dynamic first principle, this paper firstly developed kinetic energy and flexibility potential energy of the vehicle, then achieved concise flight dynamics equations by quasi-coordinates which could fully include coupling characteristics of flight dynamics, and lastly made necessary analysis about the equations. The result of study illustrates that flight dynamics equations of flexible hypersonic flight vehicles based on quasi-coordinates can satisfy the research of dynamics, stability, control,couplings and so on.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Flight Dynamics Modeling and Analysis of Flexible Hypersonic Flight Vehicles



    Erschienen in:

    Erscheinungsdatum :

    11.01.2013


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Flight Dynamics Modeling Environment for Controller Design and Analysis of Hypersonic Vehicles

    Holzapfel, F. / Heller, M. / Zahringer, C. et al. | British Library Conference Proceedings | 2001




    Flight dynamics modeling environment for controller design and analysis of hypersonic vehicles

    Holzapfel, F. / Heller, M. / Zaehringer, C. et al. | AIAA | 2001


    Flight-Corridor Analysis for Hypersonic Glide Vehicles

    Li, Guanghua / Zhang, Hongbo / Tang, Guojian | ASCE | 2016