As a necessary precursor to a heliogyro solar sail flight demonstration, meaningful ground test experiments are necessary for predicting the linear and nonlinear structural dynamics of the heliogyro membrane blades in flight. This paper describes analytical comparisons of linear and nonlinear behavior of a multi-link discrete model of a heliogyro blade under 1-g gravitational and centrifugal loads, and one setup for experimental validation of 1-g out-of-plane motion. Linear system-identification is performed on the multi-link experimental data to validate the 1-g multi-link model of a heliogyro membrane blade.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Dynamics of a Coupled Pendulum Model of a Heliogyro Membrane Blade


    Weitere Titelangaben:

    Springer Praxis Books (formerly: Springer-Praxis Series)


    Beteiligte:
    Macdonald, Malcolm (Herausgeber:in) / Huang, Yu-Ru (Autor:in) / Juang, Jer-Nan (Autor:in) / Hung, Chung-Han (Autor:in) / Keats Wilkie, W. (Autor:in)


    Erscheinungsdatum :

    04.02.2014


    Format / Umfang :

    18 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Adaptive Control of a Heliogyro Membrane Blade

    Lu, H.-H. / Juang, J.-N. / Horta, L.G. et al. | British Library Conference Proceedings | 2014


    Heliogyro Reloaded

    W. K. Wilkie / J. E. Warren / M. W. Thompson et al. | NTIS | 2011


    Heliogyro Spacecraft

    Ramnath, Rudrapatna V. | AIAA | 2010


    Structural Dynamics of the Heliogyro

    Mac Neal, R. H. | NTRS | 1971


    The Heliogyro Reloaded

    Wilkie, William K. / Warren, Jerry E. / Thompson, M. W. et al. | NTRS | 2011