this paper presents the design and dynamic analysis of a variable-span, variable-sweep morphing UAV. The construction of a morphing wing test model is discussed followed by the aerodynamic modeling of a morphing wing UAV using the vortex lattice method. The variation of the longitudinal aerodynamic coefficients as a function of span and sweep change is discussed in detail. A nonlinear dynamic model is then developed and used to simulate and analyze the response of the UAV to morphing at different rates. The variation in the longitudinal dynamic modes resulting from different morphing configurations is also presented.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Dynamic analysis of a variable-span, variable-sweep morphing UAV


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.03.2015


    Format / Umfang :

    3183046 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Linear Parameter-Varying Control of Variable Span-Sweep Morphing Aircraft

    Lee, Jihoon / Kim, Seong-hun / Jung, Seungyun et al. | AIAA | 2019


    VARIABLE SPAN MORPHING WING

    BAE JAE SUNG / HWANG JAI HYUK / CHOI SOO MIN | Europäisches Patentamt | 2015

    Freier Zugriff



    A Centrifugal Force Actuated Variable Span Morphing Helicopter Rotor

    Prabhakar, T. / Gandhi, F. / Steiner, J. et al. | British Library Conference Proceedings | 2007