Paper summarizes progress from direct reading compasses to monitored gyroscopes and concentrates on unique problems in aircraft where space limitations, reliability, and operation at all altitudes are important; it indicates how azimuth indicators and auto pilot controls close to ideal are obtainable by use of special features including novel "non-tumbling" mechanism and electromagnetic type of gimbal adjusting device. (Trans)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Improved azimuth indicating system for aircraft


    Additional title:

    Elec Eng


    Contributors:

    Published in:

    Publication date :

    1946


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Indicating System for Aircraft

    A. W. Story | NTIS | 1971


    Aircraft Indicating Systems

    SAE Technical Papers | 2015


    AIRCRAFT INDICATING SYSTEMS

    SAE Technical Papers | 1991


    Aircraft Indicating Systems

    SAE Technical Papers | 2004