The ballistic design of interplanetary missions consists of a choice of control programs and associated trajectories that ensure the achievement of the objective while meeting a variety of constraints. The use of solar-sails spacecraft for interplanetary missions imposes additional restrictions on mission parameters. These include limitations on the flight duration, the minimum distance from the Sun, the maximum angular velocity of spacecraft’s rotation and many others. Obtaining an exact optimal solution to such complex problem is associated with significant theoretical and computational difficulties. In this paper, they describe a technique for designing interplanetary missions of a solar sail spacecraft, based on the use of locally optimal control laws. This method allows determining such a combination of these laws, which ensures all mission’s requirements. An example of the application of the described technique to the calculation of the research mission associated with the exit from the Solar system is given.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    The mission’s design of solar sail spacecraft based on locally-optimal control laws


    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



    Heliocentric Solar Sail Orbit Transfers with Locally Optimal Control Laws

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




    Spacecraft solar sail processing method and solar sail

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

    Freier Zugriff

    Analytical control laws of the heliocentric motion of the solar sail spacecraft

    Gorbunova, Irina / Starinova, Olga | American Institute of Physics | 2014