Journal of Automation and Information Sciences
Published 12 issues per year
ISSN Print: 1064-2315
ISSN Online: 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,
Issue 5, 2009,
pp. 29-40
DOI: 10.1615/JAutomatInfScien.v41.i5.40
ABSTRACT
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.
KEY WORDS: stabilizing the helicopter in a hovering flight, atmospheric disturbances, suppression, static feedback by output variables, method of linear matrix inequalities
CITED BY
-
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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