A general geometric theory of spacecraft attitude determination from external reference direction sensors was presented. Outputs of different sensors are reduced to two kinds of basic directional measurements. Errors in these measurement equations are studied in detail. The partial derivatives of measurements with respect to the spacecraft orbit, the spacecraft attitude, and the error parameters form the basis for all orbit and attitude determination schemes and error analysis programs and are presented in a series of tables. The question of attitude observability is studied with the introduction of a graphical construction which provides a great deal of physical insight. The result is applied to the attitude observability of the IMP-8 spacecraft. (Author)


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    Title :

    A General Geometric Theory of Attitude Determination from Directional Sensing


    Contributors:
    B. T. Fang (author)

    Publication date :

    1976


    Size :

    36 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English