The optimal control theory of stochastic linear systems is discussed in terms of the advantages of distributed-control systems, and the control of randomly-sampled systems. An optimal solution to longitudinal control is derived and applied to the F-8 DFBW aircraft. A randomly-sampled linear process model with additive process and noise is developed.


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    Title :

    Aircraft adaptive learning control


    Contributors:

    Publication date :

    1979-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


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