Abstract
The problem is analytically solved of synthesis of the longitudinal motion stabilization law of a single-rotor helicopter at the lack of information about the vertical speed of its motion. The solution is based on the method of output control synthesis of the MIMO-system motion spectrum to be used as a basis of an especially designed multilevel decomposition of the dynamic system model in the state space. The results of numerical simulation are presented.
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03 December 2020
An Erratum to this paper has been published: https://doi.org/10.3103/S1068799820030319
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Zubov, N.E., Ryabchenko, V.N. & Sorokin, I.V. Output Control of the Longitudinal Motion Spectrum of a Single-Rotor Helicopter. Russ. Aeronaut. 63, 249–259 (2020). https://doi.org/10.3103/S1068799820020099
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DOI: https://doi.org/10.3103/S1068799820020099