In this paper, bifurcation analysis of a full six degrees of freedom model of an airship is carried out both in unconstrained and constrained conditions. Equations of motion of airship are first modified to a suitable form and a standard as well as constrained bifurcation analysis performed with respect to airship control and design parameters. Typical modes of airship dynamics and regions of stable flights are identified via this analysis. Loss of stability and mode responsible for onset of instability at critical parameter values are also identified.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Airship trim and stability analysis using bifurcation techniques


    Beteiligte:
    Tiwari, Anshul (Autor:in) / Vora, Anuj (Autor:in) / Sinha, Nandan Kumar (Autor:in)


    Erscheinungsdatum :

    01.07.2016


    Format / Umfang :

    937611 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Airship pitch trim and directional control system

    SMITH MICHAEL SCOTT / SCOTT RANDY E | Europäisches Patentamt | 2017

    Freier Zugriff

    Airship pitch trim and directional control system

    SMITH MICHAEL SCOTT / SCOTT RANDY E | Europäisches Patentamt | 2016

    Freier Zugriff

    AIRSHIP PITCH TRIM AND DIRECTIONAL CONTROL SYSTEM

    SMITH MICHAEL SCOTT / SCOTT RANDY E | Europäisches Patentamt | 2016

    Freier Zugriff

    Trim and Stability Analysis of Parafoil/Payload System Using Bifurcation Methods

    Prakash, Om / Daftary, Avani / Ananthkrishnan, N. | AIAA | 2005


    Trim and Stability Analysis of Parafoil/Payload System using Bifurcation Methods

    Prakash, O. / Daftary, A. / Ananthkrishnan, N. et al. | British Library Conference Proceedings | 2005