The space net is a novel and effective approach in solving the spacecraft capturing problem. In this chapter, the attitude control problem of parent satellite is addressed. At first, the disturbance imposed on the parent satellite is analyzed, and the dynamic process of mass ejection is investigated. In addition, the main factors that affect the performance of the net are analyzed, and based on which, the model of the disturbance torque is developed. At the end of this chapter, the numerical simulations are implemented, and the corresponding results validate the effectiveness of the proposed algorithm.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Attitude Disturbance and Control of Satellite During Space Net Projecting


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Xing, Song (Herausgeber:in) / Chen, Suting (Herausgeber:in) / Wei, Zhanming (Herausgeber:in) / Xia, Jingming (Herausgeber:in) / Gao, Zhijie (Autor:in) / Yang, Dongfang (Autor:in) / Sun, Fuchun (Autor:in)


    Erscheinungsdatum :

    15.06.2013


    Format / Umfang :

    9 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch