A computer program which determines the tangential acceleration and sight angle of a collimation controlled missile approaching a target is described. Limiting values of the variables associated with this type of missile control are examined. Radial and tangential accelerations, and the coordinates of missile and target, entered at the computer terminal as initial data are discussed. The results are presented in tabular form using the horizontal distance as an independant parameter.


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    Title :

    Collimation Control Kinematics Kollimationsstyrningskinematik


    Contributors:
    J. Agerberg (author)

    Publication date :

    1979


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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