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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    Titel :

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


    Beteiligte:
    D. J. Yost (Autor:in) / A. Arrow (Autor:in) / R. L. Konigsberg (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch