Robust quasi NID aircraft 3D flight control under sensor noise

Marian J. Błachuta; Valery D. Yurkevich; Konrad Wojciechowski

Kybernetika (1999)

  • Volume: 35, Issue: 5, page [637]-650
  • ISSN: 0023-5954

Abstract

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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.

How to cite

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Błachuta, Marian J., Yurkevich, Valery D., and Wojciechowski, Konrad. "Robust quasi NID aircraft 3D flight control under sensor noise." Kybernetika 35.5 (1999): [637]-650. <http://eudml.org/doc/33450>.

@article{Błachuta1999,
abstract = {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.},
author = {Błachuta, Marian J., Yurkevich, Valery D., Wojciechowski, Konrad},
journal = {Kybernetika},
keywords = {dynamic contraction method; tracking problem; aircraft motion controller; low-order linear dynamical system; decoupled output transients; sensor noise; dynamic contraction method; tracking problem; aircraft motion controller; low-order linear dynamical system; decoupled output transients; sensor noise},
language = {eng},
number = {5},
pages = {[637]-650},
publisher = {Institute of Information Theory and Automation AS CR},
title = {Robust quasi NID aircraft 3D flight control under sensor noise},
url = {http://eudml.org/doc/33450},
volume = {35},
year = {1999},
}

TY - JOUR
AU - Błachuta, Marian J.
AU - Yurkevich, Valery D.
AU - Wojciechowski, Konrad
TI - Robust quasi NID aircraft 3D flight control under sensor noise
JO - Kybernetika
PY - 1999
PB - Institute of Information Theory and Automation AS CR
VL - 35
IS - 5
SP - [637]
EP - 650
AB - 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.
LA - eng
KW - dynamic contraction method; tracking problem; aircraft motion controller; low-order linear dynamical system; decoupled output transients; sensor noise; dynamic contraction method; tracking problem; aircraft motion controller; low-order linear dynamical system; decoupled output transients; sensor noise
UR - http://eudml.org/doc/33450
ER -

References

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