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Title: Robust quasi NID aircraft 3D flight control under sensor noise (English)
Author: Błachuta, Marian J.
Author: Yurkevich, Valery D.
Author: Wojciechowski, Konrad
Language: English
Journal: Kybernetika
ISSN: 0023-5954
Volume: 35
Issue: 5
Year: 1999
Pages: [637]-650
Summary lang: English
Category: math
Summary: In the paper the design of an aircraft motion controller based on the Dynamic Contraction Method is presented. The control task is formulated as a tracking problem for Euler angles, where the desired decoupled output transients are accomplished under assumption of high-level, high-frequency sensor noise and incomplete information about varying parameters of the system and external disturbances. The resulting controller has a simple form of a combination of a low-order linear dynamical system and a matrix whose entries depend nonlinearly on certain measurable flight variables. (English)
Keyword: dynamic contraction method
Keyword: tracking problem
Keyword: aircraft motion controller
Keyword: low-order linear dynamical system
Keyword: decoupled output transients
Keyword: sensor noise
MSC: 93B35
MSC: 93B51
MSC: 93C73
MSC: 93C95
idZBL: Zbl 1274.93094
idMR: MR1728472
Date available: 2009-09-24T19:28:33Z
Last updated: 2015-03-27
Stable URL:
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