Simultaneous output-feedback stabilization for continuous systems in Banach spaces
Fouad M. AL-Sunni; Frank L. Lewis
Kybernetika (1998)
- Volume: 34, Issue: 2, page [199]-202
- ISSN: 0023-5954
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topAL-Sunni, Fouad M., and Lewis, Frank L.. "Simultaneous output-feedback stabilization for continuous systems in Banach spaces." Kybernetika 34.2 (1998): [199]-202. <http://eudml.org/doc/33347>.
@article{AL1998,
abstract = {A design technique for the stabilization of $M$ linear systems by one constant output-feedback controller is developed. The design equations are functions of the state and the control weighting matrices. An example of the stabilization of an aircraft at different operating points is given.},
author = {AL-Sunni, Fouad M., Lewis, Frank L.},
journal = {Kybernetika},
keywords = {design technique; linear system; feedback stabilization; constant output-feedback controller; control weighting matrices; aircraft stabilization; design technique; linear system; feedback stabilization; constant output-feedback controller; control weighting matrices; aircraft stabilization},
language = {eng},
number = {2},
pages = {[199]-202},
publisher = {Institute of Information Theory and Automation AS CR},
title = {Simultaneous output-feedback stabilization for continuous systems in Banach spaces},
url = {http://eudml.org/doc/33347},
volume = {34},
year = {1998},
}
TY - JOUR
AU - AL-Sunni, Fouad M.
AU - Lewis, Frank L.
TI - Simultaneous output-feedback stabilization for continuous systems in Banach spaces
JO - Kybernetika
PY - 1998
PB - Institute of Information Theory and Automation AS CR
VL - 34
IS - 2
SP - [199]
EP - 202
AB - A design technique for the stabilization of $M$ linear systems by one constant output-feedback controller is developed. The design equations are functions of the state and the control weighting matrices. An example of the stabilization of an aircraft at different operating points is given.
LA - eng
KW - design technique; linear system; feedback stabilization; constant output-feedback controller; control weighting matrices; aircraft stabilization; design technique; linear system; feedback stabilization; constant output-feedback controller; control weighting matrices; aircraft stabilization
UR - http://eudml.org/doc/33347
ER -
References
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