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Journal of Automation and Information Sciences
SJR: 0.238 SNIP: 0.464 CiteScore™: 0.27

ISSN Imprimir: 1064-2315
ISSN On-line: 2163-9337

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Journal of Automation and Information Sciences

DOI: 10.1615/JAutomatInfScien.v41.i5.40
pages 29-40

Suppression of Helicopter's Disturbances in a Hovering Flight by Static Output Feedback

Olga D. Gorbatyuk
Electronics and Control Systems Institute of National Aviation University, Kiev, Ukraine
Vladimir B. Larin
S.P. Timoshenko Institute of Mechanics of National Academy of Sciences of Ukraine, Kyiv, Ukraine
Anatoliy A. Tunik
Institute of Electronics and Control Systems of National Aviation University, Kiev, Ukraine

RESUMO

The problem of stabilizing the helicopter in a hovering flight when subjected to external atmospheric disturbances, taking into account the influence of the dynamics of the actuators and incorporation of accelerometers in the measurement unit of the control system. The suppression of external disturbances is carried out by the static feedback by output variables, which is synthesized by the method of linear matrix inequalities. The results of the synthesis are estimated both analytically and by simulation.


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