Facing the increasingly complex space environment, it is particularly important to approach and capture non cooperative space targets such as uncontrolled spacecraft. In order to solve the rendezvous guidance problem of continuous small-thrust non-cooperative space targets in near-circular orbits, a zero effort convex optimization guidance strategy was proposed by using the rolling convex optimization method and the rolling zero effort miss target distance estimation. It is suitable for both fixed time rendezvous tasks and adaptive time rendezvous tasks. The simulation results show that the fixed-time rendezvous task has a better rendezvous effect than the traditional differential countermeasure method, and the adaptive time rendezvous can complete the rendezvous task in a shorter time, and the method has stable performance and engineering application potential.


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    Titel :

    Space Rendezvous Guidance Method for Non-Cooperative Targets Based on Convex Optimization


    Beteiligte:
    Wang, Jirui (Autor:in) / Xia, Fengling (Autor:in)


    Erscheinungsdatum :

    22.03.2024


    Format / Umfang :

    1552935 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Rendezvous guidance of space vehicles

    Tschauner, J. / Hempel, P. | Engineering Index Backfile | 1964


    Rendezvous guidance

    Mcguire, Andrew T. | NTRS | 1990


    Terminal guidance for rendezvous in space

    Wiltshire, R.S. / Clohessy, W.H. | Engineering Index Backfile | 1960


    Rendezvous Guidance

    A. T. Mcguire | NTIS | 1990


    Terminal guidance for rendezvous in space

    Wiltshire, R.S. / Clohessy, W.H. | Engineering Index Backfile | 1959