A phase modulation method for remote guidance faults in autonomous and quick rendezvous and docking is proposed. According to position and attitude navigation information, ground fault judgment instructions, various fault modes corresponding to different autonomous quick rendezvous and docking fault conditions are given. The chaser spacecraft is guided to the frozen orbit behind the target spacecraft by using the two impulses orbit change strategy for typical fault modes. After the fault is removed, new rendezvous and docking can be achieved by guidance from ground for one or two days according to the current phase angle.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    A Fault Handling Scheme for Remote Guidance of Autonomous Quick Rendezvous and Docking


    Beteiligte:
    Changqing, Chen (Autor:in) / Yongchun, Xie (Autor:in) / Qiang, Zhang (Autor:in) / Hao, Zhang (Autor:in)


    Erscheinungsdatum :

    01.07.2023


    Format / Umfang :

    1084934 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Fast relative guidance approach for autonomous rendezvous and docking control

    Develle, Michael / Xu, Yunjun / Pham, Khanh et al. | SPIE | 2011


    Autonomous spacecraft rendezvous and docking

    Tietz, J. C. / Almand, B. J. | NTRS | 1985


    Space rendezvous guidance and docking techniques

    Denton, C.I. / Sando, R.M. / Monheit, A.T. | Engineering Index Backfile | 1962