The problem of trajectory optimization and control of multistage satellite launchers is discussed. From a proposed strategy for the launching, an optimization problem is formulated which is considered sufficiently realistic for the phase of mission analysis and definition. Following that, a solution scheme is proposed for the open loop and the closed loop problems, using procedures of suboptimal control and of stochastic control, respectively.


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    Titel :

    Guidance and Control of Space Vehicles for Satellite Launching


    Beteiligte:
    A. R. Neto (Autor:in)

    Erscheinungsdatum :

    1982


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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