The aim of this paper is to analyze optimal trajectories of a solar sail-based spacecraft in missions towards the outer Solar System region. The paper proposes a simplified approach able to estimate the minimum flight time required to reach a given (sufficiently high) heliocentric distance. In particular, the effect of a set of solar photonic assists on the overall mission performance is analyzed with a simplified numerical approach. A comparison with results taken from the existing literature show the soundness of the proposed approach.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Solar Sail Simplified Optimal Control Law for Reaching High Heliocentric Distances


    Weitere Titelangaben:

    Aerotec. Missili Spaz.


    Beteiligte:

    Erschienen in:

    Aerotecnica Missili & Spazio ; 100 , 4 ; 337-344


    Erscheinungsdatum :

    2021-12-01


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Heliocentric Solar Sail Orbit Transfers with Locally Optimal Control Laws

    Malcolm Macdonald / Colin McInnes / Bernd Dachwald | AIAA | 2007



    Solar Sail Heliocentric Earth-Following Orbits

    Heiligers, Jeannette / McInnes, Colin R. | AIAA | 2015


    Solar Sail Heliocentric Elliptic Displaced Orbits

    Gong, Shengping / Li, Junfeng | AIAA | 2014


    Solar Sail Heliocentric Earth-Following Orbits

    Jeannette Heiligers | Online Contents | 2015