The implementation of procedures used to calculate the attitude of a rocket from its transmitted gyroscopic roll, pitch, and yaw signals is discussed. The differences and the angular conversions of the output from various inertial attitude systems are presented. Also, a synopsis of the mathematical analysis used to compute attitude is presented. In addition, analyses and data reduction techniques are developed to determine the attitude of the Ute-Tomahawk rocket A09.209-1, fired 16 April 1973 at White Sands Missile Range, New Mexico.


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    Titel :

    Attitude Determination Techniques for Rockets with Inertial Measuring Systems


    Beteiligte:
    B. F. Sullivan (Autor:in) / M. E. Stick (Autor:in) / R. J. Marcou (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    69 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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