This report shows the feasibility and characteristics of a low-cost, strapped-down inertial guidance system for a tactical, short flight time missile. The guidance system incorporates only state-of-the-art hardware, specifically: (1) a whole number, vector, digital computer solving a three parameter Euler angle body axis to inertial coordinate transformation, and (2) existing enertial sensors and associated operating electronics specifically designed to achieve the requirements of a strapped-down system for this type of application. (Author)


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    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


    Inertial sensor performance in a strapped-down environment

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


    Present and future roles of strapped-down inertial systems

    Powell, J.C. | Engineering Index Backfile | 1963