Present and future roles of strapped-down inertial systems are analyzed by differential comparison of various mechanizations based on size, weight, power, reliability, and ease of maintenance; inertial systems are divided into those using rate sensing devices and those employing free gyros or other types of stable attitude reference; computer vs gimbal trade-off is discussed; impact of electrically supported accelerometer (ESA) and laser rate sensor on future systems is considered.


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    Titel :

    Present and future roles of strapped-down inertial systems


    Weitere Titelangaben:

    Symposium Ballistic Missile Space Technology


    Beteiligte:
    Powell, J.C. (Autor:in)

    Kongress:

    8th Symposium on Ballistic Missile and Space Technology Transactions ; 1963 Control



    Erscheinungsdatum :

    1963


    Format / Umfang :

    18 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Inertial sensor performance in a strapped-down environment

    THOMPSON, J.A. / UNGER, F.G. | AIAA | 1966


    Inertial Attitude Sensors in a Strapped-Down System

    ZAGONE, PETER / HESSE, JR., CAPTAIN | AIAA | 1965



    A GENERALIZED DESIGN CRITERION FOR STRAPPED-DOWN INERTIAL SENSOR LOOPS

    ROANTREE, JAMES / KORNIANIK, NICHOLAS | AIAA | 1966