This paper describes a method of modeling general attitude dynamics of a nonspinning momentum-biased spacecraft under strong influence of solar radiation pressure. This model, called the “generalized sail dynamics model,” can be applied to realistic solar sail spacecraft with nonflat surfaces and nonuniform optical reflectance. A coarse sun-pointing momentum-biased spacecraft is especially of interest, for which an approximate solution of the equations of motion is analytically derived. Stability and fundamental characteristics of momentum-biased spacecraft dynamics as well as theoretical relations with past dynamics models are discussed in detail. Furthermore, unique attitude motion predicted by the novel model is verified with flight data of the Japanese interplanetary probe, Hayabusa 2.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Generalized Attitude Model for Momentum-Biased Solar Sail Spacecraft


    Beteiligte:
    Ono, Go (Autor:in) / Tsuda, Yuichi (Autor:in) / Akatsuka, Kosuke (Autor:in) / Saiki, Takanao (Autor:in) / Mimasu, Yuya (Autor:in) / Ogawa, Naoko (Autor:in) / Terui, Fuyuto (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.07.2016




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Generalized Attitude Model for Spinning Solar Sail Spacecraft

    Tsuda, Yuichi / Saiki, Takanao / Funase, Ryu et al. | AIAA | 2013



    Solar sail attitude adjustment actuator, solar sail assembly and spacecraft

    ZHAO YUJIE / JIN ZILIN / LIAO ZHIFENG et al. | Europäisches Patentamt | 2023

    Freier Zugriff