Abstract The problem on restriction of aircraft motion parameters is considered. The special features are noted of constructing the logical dynamic systems of automatic control with algebraic selectors for different control channels of aircraft angular motion. The problems of synthesizing such systems are considered. The simulation results are presented.


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    Title :

    Method for constructing automatic control systems with restriction on aircraft critical parameters


    Contributors:

    Published in:

    Publication date :

    2015-07-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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