Adaptive two-axis acceleration control and roll stabilization of air-to-air missile is analyzed and simulated; adaptive principle consists of relocating open loop zeros to region of S-plane having prescribed damping and frequency characteristics, and cyclically increasing forward loop gain to drive control surface actuator poles across imaginary axis at fixed frequency; factors to consider in application and mechanization of control system are presented.


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    Titel :

    Design, analysis and simulation of self-adaptive acceleration flight control system


    Weitere Titelangaben:

    AIAA -- Simulation Aerospace Flight Conference -- Tech Papers


    Beteiligte:
    Kinney, R.V. (Autor:in)

    Kongress:

    AIAA -- Simulation for Aerospace Flight Conference ; 1963 Control



    Erscheinungsdatum :

    1963


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :