Design of adaptive roll autopilot for typical air-to-air cruciform interceptor missile with range of 58.5 to 1 in aileron-moment effectiveness; chosen autopilot configuration uses gain-changing loop to control amplitude of quasi-linear limit cycle in main roll-rate loop; flights at three altitudes with widely different aerodynamic histories were successfully simulated; conclusion that design concept is most applicable to tail-controlled surface-to-air, interceptor missile.


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    Title :

    Missile adaptive roll autopilot with small-amplitude limit cycle


    Additional title:

    Joint Automatic Control Conference


    Contributors:

    Conference:

    Joint Automatic Control Conference ; 1965 Control



    Publication date :

    1965


    Size :

    12 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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