System uses identification and synthesis processes to determine what changes in control parameters are required to adapt to changes in dynamics of vehicle as it experiences wide range of flight conditions; identification of vehicle dynamics is accomplished by improved identification technique; digital computer simulation of digital adaptive pitch rate flight control system was performed which included identification of fourth-order aerospace vehicle and actuation system and synthesis of fourth-order digital compensator.


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    Titel :

    Digital adaptive flight control system for aerospace vehicles


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Andeen, R.E. (Autor:in) / Shipley, P.P. (Autor:in)

    Erschienen in:

    AIAA Journal ; 1 , n 5


    Erscheinungsdatum :

    1963


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    DIGITAL ADAPTIVE FLIGHT CONTROL SYSTEM FOR AEROSPACE VEHICLES

    ANDEEN, R. E. / SHIPLEY, P. P. | AIAA | 1963


    Aerospace vehicles and adaptive flight control

    Reed, M.W. | Engineering Index Backfile | 1962


    Introduction to Aerospace Flight Vehicles

    J. Gordon Leishman | OERSI | 2025

    Freier Zugriff

    Adaptive control applications to aerospace vehicles

    EHLERS, H. L. / SMYTH, R. K. | AIAA | 1970


    Self-organizing adaptive control of aerospace vehicles

    Barron, R.L. / Schalkowsky, S. / Davies, J.M. | Engineering Index Backfile | 1965