The instantaneous thrust-direction for a spacecraft to perform a minimum-time rendezvous with another (nonmaneuvering) spacecraft is determined as a function of instantaneous relative velocity and position. The magnitude of the thrust acceleration is assumed constant and the acceleration due to external forces is neglected. (Author)


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    Titel :

    Nonlinear Feedback Solution for Minimum Rendezvous with Constant Thrust Acceleration


    Beteiligte:
    A. E. Bryson (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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