Email this article Synthesis of control laws for aircraft lateral motion at the lack of data on the slip angle: Analytical solution
- Authors: Zubov N.E.1, Mikrin E.A.1, Ryabchenko V.N.1, Fomichev A.V.1
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Affiliations:
- Bauman Moscow State Technical University
- Issue: Vol 60, No 1 (2017)
- Pages: 64-73
- Section: 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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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.
About the authors
N. E. Zubov
Bauman Moscow State Technical University
Author for correspondence.
Email: Nikolay.Zubov@rsce.ru
Russian Federation, ul. Vtoraya Baumanskaya 5, Moscow, 105005
E. A. Mikrin
Bauman Moscow State Technical University
Email: Nikolay.Zubov@rsce.ru
Russian Federation, ul. Vtoraya Baumanskaya 5, Moscow, 105005
V. N. Ryabchenko
Bauman Moscow State Technical University
Email: Nikolay.Zubov@rsce.ru
Russian Federation, ul. Vtoraya Baumanskaya 5, Moscow, 105005
A. V. Fomichev
Bauman Moscow State Technical University
Email: Nikolay.Zubov@rsce.ru
Russian Federation, ul. Vtoraya Baumanskaya 5, Moscow, 105005
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