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


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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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N. Zubov

Bauman Moscow State Technical University

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Email: Nikolay.Zubov@rsce.ru
俄罗斯联邦, ul. Vtoraya Baumanskaya 5, Moscow, 105005

E. Mikrin

Bauman Moscow State Technical University

Email: Nikolay.Zubov@rsce.ru
俄罗斯联邦, ul. Vtoraya Baumanskaya 5, Moscow, 105005

V. Ryabchenko

Bauman Moscow State Technical University

Email: Nikolay.Zubov@rsce.ru
俄罗斯联邦, ul. Vtoraya Baumanskaya 5, Moscow, 105005

A. Fomichev

Bauman Moscow State Technical University

Email: Nikolay.Zubov@rsce.ru
俄罗斯联邦, ul. Vtoraya Baumanskaya 5, Moscow, 105005

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