This report develops a guidance formulation with general applicability to the problem of the IFR landing of aircraft of any type; however, the formulation is specialized in this document to the case of a non-decelerating approach to the landing point. The control problem considered is the computer simulation of the automatic landing of a mini-RPV of the delta wing variety. (Author)


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    Title :

    An Approach Guidance System for Remotely-Piloted Vehicles


    Contributors:
    N. K. Shupe (author)

    Publication date :

    1977


    Size :

    71 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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