The interferometer homing system is for steering guided missiles toward a collision with a target. Two separated horn-type antennas are mounted upon the guided missile. The interferometer homing system produces a steering signal in which there appears no false information in the form of biases. The gyroscope compensation factor remains fixed throughout the flight of the missile.


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    Title :

    Inter-Ferometer Homing System


    Contributors:
    J. F. Gulick (author) / T. D. Jacot (author) / H. H. Knapp (author) / H. H. Nall (author)

    Publication date :

    1965


    Size :

    1 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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