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Mekhatronika, Avtomatizatsiya, Upravlenie, 2018, vol. 19, no. 4, pp. 273—281
DOI: 10.17587/mau.19.273-281

Synthesis of Stabilization Laws of a Single-Airscrew Helicopter's Lateral Motion for Lack of Information about its Lateral Speed: Analytical Solution

N. E. Zubov, Professor, Nikolay.Zubov@rsce.ru, V. N. Ryabchenko, Professor, I. V. Sorokin, Professor, Moscow State Technical University after N. E. Bauman, Moscow, 105005, Russian Federation

Corresponding author: Zubov Nikolai E., D. Sc., Professor, Moscow State Technical University after N. E. Bauman, Moscow, 105005, Russian Federation, e-mail: Nikolay.Zubov@rsce.ru

Accepted on Deсember 15, 2017

The problem of stabilization law synthesis of a single-airscrew helicopter's lateral motion for lack of information about the lateral speed of its motion is analytically solved. The solution is based on the method of output vector control synthesis, which provides a specified spectrum of a dynamic system motion to be used as the basis of an especially designed multilevel decomposition of the system model in state space. Numerical simulation data that confirm the results are presented.
Keywords: linear MIMO-system, output vector control synthesis, modal synthesis

Acknowledgments: This work was supported financially by the Russian Science Foundation (Project № 18-19-00004).

For citation:
Zubov N. E., Ryabchenko V. N., Sorokin I. V. Synthesis of Stabilization Laws of a Single-Airscrew Helicopter's Lateral Motion for Lack of Information about its Lateral Speed: Analytical Solution, Mekhatronika, Avtomatizatsiya, Upravlenie, 2018, vol. 19, no. 4, pp. 273—281.

DOI: 10.17587/mau.19.273-281

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