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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    Title :

    Digital adaptive flight control system for aerospace vehicles


    Additional title:

    AIAA J


    Contributors:

    Published in:

    AIAA Journal ; 1 , n 5


    Publication date :

    1963


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    DIGITAL ADAPTIVE FLIGHT CONTROL SYSTEM FOR AEROSPACE VEHICLES

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    Self-organizing adaptive control of aerospace vehicles

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