System developed by Ling-Temco-Vought, Inc for Electric Propulsion Space Test System project (WS-661A); principal characteristics of concept and key features; concept, intended as actuation device for attitude control, incorporates features making it possible to be used as measuring device to measure torques imparted to space vehicle; installation and construction considerations; advantages include availability of direct, accurate readout of applied torque, use of off-the-shelf components, good dynamic response characteristics, redundancy, low power requirements, and low weight for angular momentum capacity.


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    Title :

    Twin gyro attitude control system designed for disturbance instrumentation of space vehicle


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1964 Control



    Publication date :

    1964


    Size :

    6 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :



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