The problem of a low-thrust spacecraft controlled to a reference orbit is addressed in this paper. A simple and explicit low-thrust guidance scheme with constrained thrust magnitude is developed by combining the fundamental equations of motion for constrained systems from analytical dynamics with a Lyapunov-based method. Examples are given for a spacecraft controlled to a reference trajectory in the circular restricted three body problem.


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    Titel :

    Explicit Low-Thrust Guidance for Reference Orbit Targeting


    Beteiligte:
    Lam, Try (Autor:in) / Udwadia, Firdaus E. (Autor:in)

    Kongress:

    AAS/AIAA Astrodynamics Specialist Conference ; 2013 ; Hilton Head, SC, United States


    Erscheinungsdatum :

    11.08.2013


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Iterative explicit guidance for low thrust spacecraft.

    Jacobson, R. A. / Powers, W. F. | NTRS | 1972


    Iterative Explicit Guidance for Low Thrust Spaceflight

    ROBERT A. JACOBSON AND WILLIAM F. POWERS | AIAA | 1974


    Iterative explicit guidance for low thrust spacecraft

    JACOBSON, R. / POWERS, W. | AIAA | 1972