The use of conventional (non-nuclear) weapons in a standoff mode has been receiving significant attention during the past few years. The guidance requirements are quite rigorous; therefore, weapons will require in-flight updates to achieve the necessary accuracies. The Boeing Military Airplane Company is constructing a large scale digital simulation for developing and evaluating missile guidance systems for conventional standoff capability. This paper summarizes the structure of the simulator and the guidance algorithm development and analysis. The simulation will contain carrier, missile, target, radar geometry, wind, terrain, target seeker, and guidance computer models. Both 'truth' behavior and 'perturbed' behavior with system error are computed. To provide flexibility and versatility, the missile guidance computer model will use virtual target paths that are cubic splines. This provides a method for completely specifying an initial trajectory and updated trajectories to the missile with a minimal number of parameters.


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    Title :

    Missile guidance simulation


    Additional title:

    Flugkoerpersteuerungssimulation


    Contributors:
    Funk, J.E. (author) / Johnson, H.D. (author) / Schmidt, G.C. (author)


    Publication date :

    1984


    Size :

    7 Seiten, 9 Bilder, 1 Quelle


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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