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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

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


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:

    Kongress:

    SAE Meeting ; 1964 Control



    Erscheinungsdatum :

    1964


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Twin-gyro attitude control systems.

    HUSTON, R. L. | AIAA | 1966


    COAXIAL TWIN-GYRO ATTITUDE CONTROL SYSTEM

    LEE HYUCK SIK | Europäisches Patentamt | 2018

    Freier Zugriff

    Results of studies on twin-gyro attitude-control system for space vehicles

    Lopez, A.E. / Ratcliff, J.W. / Havill, J.R. | Engineering Index Backfile | 1964


    RESULTS OF STUDIES ON A TWIN-GYRO ATTITUDE CONTROL SYSTEM FOR SPACE VEHICLES

    Havill, J. R. / Lopez, A. E. / Ratcliff, J. W. | NTRS | 1963