The problem of guiding an instrumented aircraft to follow a pre-assigned trajectory using the Portable Automatic Calibration Tracker (PACT) data is considered in this paper. Guidance control is formulated as an optimal linear state regulator problem for a discrete time-delayed system. Responses to some flight courses of interest have, been achieved through computer system simulation. Post-flight test data obtained from the PACT confirm the basic validity of the theoretical results.


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    Title :

    Automatic Flight Guidance Using the Portable Automatic Calibration Tracker Data


    Contributors:

    Published in:

    Publication date :

    1975-11-01


    Size :

    937316 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English






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