The popularity, development and promising performance in orbit for small satellite make it’s trends of mission to be run by the satellite become more complex. Since the small satellites may brought payload with higher power requirement to run its mission. This payload may not be able supported by the power system, in which is a combination of solar panel with batteries. Small satellite also has size and mass constraints which made it won’t be able to bring active motion mechanism for the solar panel. A natural question to be answered is where the best installation position (placement) of the deployable solar panel with respect to the body satellite such that the power system can acquire maximal solar energy. This paper proposes simulation based method to determine placement (position) of the fixed installed deployable solar panel system such that maximal power can be provided. To validate this method, simulations data summary is presented in this paper where concerns in two different orbits of satellites and eleven cases that accommodates. Based in the simulation results, options for the position of the fixed installed deployable solar panel is provided.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Simu1ation Approach to Determine Position of the Fixed Installed Deployable Solar Panel


    Beteiligte:
    Septanto, Harry (Autor:in) / Sudjana, Oetomo (Autor:in)


    Erscheinungsdatum :

    01.09.2018


    Format / Umfang :

    150976 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    DEPLOYABLE SOLAR PANEL MECHANISM

    FIRTIN MURAT BERK / SOYER EMIN BIREY / GÜNDOĞDU ALI | Europäisches Patentamt | 2024

    Freier Zugriff

    Deployable satellite solar panel hinge mechanism

    SPARK WILLIAM JOEL | Europäisches Patentamt | 2023

    Freier Zugriff

    DEPLOYABLE SOLAR PANEL ARRAY FOR SPACECRAFT

    MARKS GEOFFREY W / ROHWELLER DAVID J / PEDERSEN CHRISTIAN J | Europäisches Patentamt | 2016

    Freier Zugriff

    Elastically deployable panel structure solar arrays

    SPENCE BRIAN R / WHITE STEPHEN F / DOUGLAS MARK V | Europäisches Patentamt | 2015

    Freier Zugriff

    DEPLOYABLE SATELLITE SOLAR PANEL HINGE MECHANISM

    SPARK WILLIAM JOEL | Europäisches Patentamt | 2020

    Freier Zugriff