Two figures of merit developed which justify establishing minimum spring rate for gyroscope structure and its mounting bracket.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Rigidity as factor in rate gyro mounting


    Additional title:

    Aeronautical Eng Rev


    Contributors:

    Published in:

    Publication date :

    1957


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





    Mounting structure for enhancing grid rigidity

    ZHU JICHENG / WANG LIANGLIANG / HUANG KANG et al. | European Patent Office | 2024

    Free access

    Rate Gyro Assembly Configuration

    SAE Technical Papers | 2008


    Gyro sensor assembly mounting bracket capable of adjusting course

    XU YAN / XIE HUICI / WAN MING et al. | European Patent Office | 2021

    Free access

    Missile Laser Gyro Rate Sensor

    R. F. Morrison / C. B. Strang | AIAA | 1977