The paper considers a three-dimension nonlinear motion of a spacecraft with frame-type solar sail. The mathematical model of a guided heliocentric motion is described within combined polar coordinate system. The locally optimal control laws of orbital element maintenance and correction are formulated. The solar sail spacecraft guided motion is analyzed. The flight trajectory, dependency graphs of flight parameters against duration are obtained.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Nonlinear analysis of three-dimensional guided motion of solar sail spacecraft


    Beteiligte:

    Kongress:

    ICNPAA 2018 WORLD CONGRESS: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences ; 2018 ; Yerevan, Armenia


    Erschienen in:

    Erscheinungsdatum :

    04.12.2018


    Format / Umfang :

    8 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Spacecraft solar sail processing method and solar sail

    REN ZHONGJING / LI CHENGYANG / XIE KECAI et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Solar Sail Spacecraft Development

    Danielle R DaCosta | NTRS


    SOLAR SAIL AND SOLAR SAIL SPACECRAFT USING THE SAME

    NAGAI MASATAKA | Europäisches Patentamt | 2016

    Freier Zugriff

    Gyromesh solar sail spacecraft and sail panel assemblies

    SIPPEL TIMOTHY N | Europäisches Patentamt | 2024

    Freier Zugriff