Forces applied to large aerospace vehicle to change attitude or velocity of vehicle will often excite significant undesirable vibration; some typical thrust patterns are examined which accomplish desired maneuver and also are constrained to leave some vibratory modes unexcited at conclusion of maneuver; added cost in terms of time for maneuver, complexity of thrust pattern, and fuel or total control effort is examined for optimal maneuvers of this type; techniques for interpreting solutions to these problems in terms of multiple phase plane plots are given.


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    Titel :

    Optimal control of maneuver-induced vibration in flexible aerospace vehicles


    Weitere Titelangaben:

    AIAA/ASME -- Tech Paper


    Beteiligte:
    Karnopp, D. (Autor:in)

    Kongress:

    Meeting of the 8th AIAA/ASME -- Structures, Structural Dynamics and Materials Conference ; 1967 Vibrations



    Erscheinungsdatum :

    1967


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :






    Aerospace ground maneuver light

    HESSLING VON HEIMENDAHL ANDRE / WERNICKE ALEXANDER / JHA ANIL KUMAR et al. | Europäisches Patentamt | 2015

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