Synthesis of control laws for aircraft lateral motion at the lack of data on the slip angle: Analytical solution
- Авторы: Zubov N.E.1, Mikrin E.A.1, Ryabchenko V.N.1, Fomichev A.V.1
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Учреждения:
- Bauman Moscow State Technical University
- Выпуск: Том 60, № 1 (2017)
- Страницы: 64-73
- Раздел: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/229995
- DOI: https://doi.org/10.3103/S106879981701010X
- ID: 229995
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Аннотация
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.
Об авторах
N. Zubov
Bauman Moscow State Technical University
Автор, ответственный за переписку.
Email: Nikolay.Zubov@rsce.ru
Россия, ul. Vtoraya Baumanskaya 5, Moscow, 105005
E. Mikrin
Bauman Moscow State Technical University
Email: Nikolay.Zubov@rsce.ru
Россия, ul. Vtoraya Baumanskaya 5, Moscow, 105005
V. Ryabchenko
Bauman Moscow State Technical University
Email: Nikolay.Zubov@rsce.ru
Россия, ul. Vtoraya Baumanskaya 5, Moscow, 105005
A. Fomichev
Bauman Moscow State Technical University
Email: Nikolay.Zubov@rsce.ru
Россия, ul. Vtoraya Baumanskaya 5, Moscow, 105005
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