Basic concepts and possible applications to space flight and astronautics; principle of M.SCHULER pendulum and accelerometers; mathematic solution for hypothetical system, consisting of three accelerometers and three gyros; other possible configurations are pendulums employed as accelerometers using gravity as restoring torque; digital computer required. (formerly J Astronautics)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Fundamentals of inertial guidance and navigation


    Additional title:

    J Astronautical Sciences


    Contributors:
    Frye, W.E. (author)

    Published in:

    Publication date :

    1958


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Fundamentals of inertial navigation

    Litton, Guidance and Control Systems Division, Technical Training | TIBKAT | 1980


    Fundamentals of inertial navigation

    Litton Systems, Aero Products | SLUB | 1971


    Fundamentals of inertial navigation

    Litton Systems, Aero Products | SLUB | 1975


    Fundamentals of Satellite and Inertial Navigation

    Grewal, Mohinder S. / Weill, Lawrence R. / Andrews, Angus P. | Wiley | 2007


    Fundamentals of Satellite and Inertial Navigation

    Grewal, Mohinder S. / Weill, Lawrence R. / Andrews, Angus P. | Wiley | 2000