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    Synthesis of control laws for aircraft lateral motion at the lack of data on the slip angle: Analytical solution

    Synthesis of control laws for aircraft lateral motion at the lack of data on the slip angle: Analytical solution


    Abstract The problem of lateral motion stabilization is analytically solved for the fourth-order model of aircraft motion using the method of output signal control synthesis that is based on the control object decomposition. Numerical simulation data are presented.

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    Title :

    Synthesis of control laws for aircraft lateral motion at the lack of data on the slip angle: Analytical solution

    Contributors:
    Zubov, N. E. (author) / Mikrin, E. A. (author) / Ryabchenko, V. N. (author) / Fomichev, A. V. (author)
    Published in:

    Russian Aeronautics ; 60 , 1 ; 64-73

    Publication date :

    2017-01-01

    Size :

    10 pages

    ISSN :

    1934-7901 , 1068-7998

    DOI :

    https://doi.org/10.3103/S106879981701010X

    Type of media :

    Article (Journal)

    Type of material :

    Electronic Resource

    Language :

    English

    Keywords :

    MIMO-system , aircraft , lateral motion , output signal control , specified spectrum of closed-loop system Engineering , Automotive Engineering

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