A missile control system can avoid instability at high angles of attack by cross-coupling roll and steering sensor signals between the steering and roll channels. The control law for the system is derived by use of the Model-in-the-Performance Index Technique which makes the system respond at high angles as it does at low angles with desired response times, bandwidths, and stability.


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    Title :

    High Angle-of-Attack Missile Control System for Aerodynamically Controlled Missiles


    Contributors:
    D. J. Yost (author) / A. Arrow (author) / R. L. Konigsberg (author)

    Publication date :

    1978


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English