This recommended practice covers the requirements for gyroscopically stabilized Directional Indicating Systems, which will operate as a 1°/hour latitude corrected, free directional gyro or as a slaved gyro, magnetic compass with 1/2° accuracy. This Technical Report contains no changes from the previous revision, other than the addition of a Stabilization Notice Page. This document has been determined to contain stable technical information which is not dynamic in nature.


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    Title :

    Directional Indicating System (Turbine Powered Subsonic Aircraft)


    Publication date :

    2020-04-14



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English