Email this article Synthesis of Stabilization Laws for Lateral Motion of a Maneuverable Aircraft at the Lack of Data on Its Sideslip and Roll Angles
- Authors: Zubov N.E.1, Mikrin E.A.2, Ryabchenko V.N.1, Sorokin I.V.2
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Affiliations:
- Bauman Moscow State Technical University
- Korolev Rocket and Space Corporation Energiya
- Issue: Vol 62, No 1 (2019)
- Pages: 22-31
- Section: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230814
- DOI: https://doi.org/10.3103/S1068799819010045
- ID: 230814
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Abstract
The problem of synthesizing stabilization laws for lateral motion of a maneuverable aircraft at the lack of data on its sideslip and roll angles is analytically solved. The solution is based on the improved method of output signal control synthesis, which provides the specified spectrum of MIMO-system motion. The results of analytical synthesis of the control law and numerical simulation data are presented.
About the authors
N. E. Zubov
Bauman Moscow State Technical University
Author for correspondence.
Email: nik.zubov@gmail.com
Russian Federation, ul. 2-ya Baumanskaya 5, Moscow, 105005
E. A. Mikrin
Korolev Rocket and Space Corporation Energiya
Email: nik.zubov@gmail.com
Russian Federation, ul. Lenina 4a, Korolev, Moscow region, 141070
V. N. Ryabchenko
Bauman Moscow State Technical University
Email: nik.zubov@gmail.com
Russian Federation, ul. 2-ya Baumanskaya 5, Moscow, 105005
I. V. Sorokin
Korolev Rocket and Space Corporation Energiya
Email: nik.zubov@gmail.com
Russian Federation, ul. Lenina 4a, Korolev, Moscow region, 141070
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