The stationary hovering characteristic of elliptical orbit was analyzed in two cases in this paper. In the first case, the short-time hovering at the R-bar and V-bar were analyzed by calculating the drift coefficient of the relative acceleration. The approximate uncontrolled hovering region was obtained by computing the variation of the drift coefficient with the orbital elements (semimajor axis, eccentricity, true anomaly). In the second case, the long-time hovering was analyzed by calculating the velocity increment costs in an orbit period using an open-loop controller. Analytical and numerical analysis showed that it is easier for high orbit with low eccentricity to achieve hovering for a long-duration flight. The V-bar hovering (H-bar hovering) is the most energy-saving way when eccentricity is less (more) than 0.65.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Characteristic Analysis for Elliptical Orbit Hovering Based on Relative Dynamics


    Beteiligte:
    Jingrui Zhang (Autor:in) / Shuge Zhao (Autor:in) / Yongzhao Yang (Autor:in)


    Erscheinungsdatum :

    01.10.2013


    Format / Umfang :

    2508217 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Hovering Formation Design and Control Based on Relative Orbit Elements

    Rao, Yinrui / Yin, Jianfeng / Han, Chao | AIAA | 2016



    Impulsive Hovering Formation Based on Relative Orbit Elements (AAS 13-395)

    Yin, J. / Han, C. / American Astronautical Society et al. | British Library Conference Proceedings | 2013


    RELATIVE LAMBERT TRANFER FOR ELLIPTICAL REFERENCE ORBIT BASED ON RELATIVE ORBIT ELEMENTS

    Chen, Huan / Han, Chao / Rao, Yinrui et al. | British Library Conference Proceedings | 2016