A convexification method originating from second order cone programming is applied to multiple satellites formation reconfiguration problems with concave collision avoidance constraints. Geometric relative orbit elements are introduced to straightforward depict formation configurations. Algorithm consists of external convexification iterations and the Gauss pseudospectral method is presented for coping with nonconvex transfer trajectories planning. Numerical examples are implemented for validating the proposed approach, and contrast simulations separately with spherical and rectangular approximations of concave inequality constraints are carried out, results indicate a manifestly improvement in energy optimization with the algorithm presented here.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Multiple spacecraft formation reconfiguration planning with nonconvex collision avoidance constraints


    Beteiligte:
    Zhou, Ding (Autor:in) / Hu, Yuting (Autor:in) / Li, Shunli (Autor:in)


    Erscheinungsdatum :

    01.08.2016


    Format / Umfang :

    137840 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Spacecraft Formation Reconfiguration with Collision Avoidance

    Schlanbusch, R. / Kristiansen, R. / Nicklasson, P.J. et al. | British Library Conference Proceedings | 2008




    Finite-Time Formation Reconfiguration of Multiple Spacecraft with Collision Avoidance Problems

    Xia, Yuanqing / Zhang, Jinhui / Lu, Kunfeng et al. | Springer Verlag | 2018


    Adaptive Finite-Time Reconfiguration Control for Spacecraft Formation with Collision Avoidance

    Yang, Xicheng / Zong, Qun / Zhang, Xiuyun et al. | Springer Verlag | 2021