PAR (Position and Rate) gyro, developed by Guidance Technology, Inc, is used as single sensor for heading-hold performance and lateral mode stability in Beech KDB-1 target and Douglas A4D-1 aircraft; single degree of freedom gyro with internal electromechanical integrator provides desired yaw attitude signal for performing straight azimuth courses and senses aircraft lateral rates for Dutch roll stability augmentation; principle, examples of uses, and available designs.


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    Title :

    Directional stability and control with single gyro


    Additional title:

    Aerospace Eng


    Contributors:

    Published in:

    Publication date :

    1961


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :