Two distinct methods to effect control action are described and two arrangements illustrated; factors which affect dynamic characteristics of aircraft can be classified as environmental, geometrical, flight-mode, and internal factors; direct method of providing variable-parameter controller and its disadvantages; requirements for self-adaptive system and description of system developed by Aviation Div of Smiths Industries Ltd; method of obtaining autostabilizer parameters by direct measurement of aircraft characteristics and operation of system; effect of finite snr; applications.


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    Title :

    Self-adaptive control of aircraft


    Additional title:

    Flight


    Contributors:

    Published in:

    Publication date :

    1967


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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