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Journal of Automation and Information Sciences

Publicou 12 edições por ano

ISSN Imprimir: 1064-2315

ISSN On-line: 2163-9337

SJR: 0.173 SNIP: 0.588 CiteScore™:: 2

Indexed in

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

Volume 41, Edição 5, 2009, pp. 29-40
DOI: 10.1615/JAutomatInfScien.v41.i5.40
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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.

CITADO POR
  1. Aliev F. A., Larin V. B., Stabilization problems for a system with output feedback (review), International Applied Mechanics, 47, 3, 2011. Crossref

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