Performance specifications for accelerometer to be used during launching phase of space vehicle; limitations of present-day types and possible future developments are outlined. (See also p 227-228 + 230 + 232 + 234 + 238 + 240)


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    Titel :

    Which accelerometers for spacecraft guidance


    Weitere Titelangaben:

    Space/Aeronautics


    Beteiligte:
    Slater, J.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1960


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Estimation of Spacecraft Angular Acceleration Using Linear Accelerometers (AAS 13-366)

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    Spacecraft Guidance Systems

    Tewari, Ashish | Wiley | 2011


    Spacecraft navigation and guidance

    Noton, Maxwell | TIBKAT | 1998


    Conceptual Spacecraft-Guidance Algorithm

    Mccormick, Bernell R. / Compton, James W. | NTRS | 1988


    Spacecraft guidance and control

    Scull, J. R. | TIBKAT | 1966