CONTROL OF WING ROCK MOTION USING ADAPTIVE FEEDBACK LINEARIZATION

Authors
MONAHEMI MM KRSTIC M
Citation
Mm. Monahemi et M. Krstic, CONTROL OF WING ROCK MOTION USING ADAPTIVE FEEDBACK LINEARIZATION, Journal of guidance, control, and dynamics, 19(4), 1996, pp. 905-912
Citations number
19
Categorie Soggetti
Instument & Instrumentation","Aerospace Engineering & Tecnology
Journal title
Journal of guidance, control, and dynamics → ACNP
ISSN journal
07315090
Volume
19
Issue
4
Year of publication
1996
Pages
905 - 912
Database
ISI
SICI code
0731-5090(1996)19:4<905:COWRMU>2.0.ZU;2-9
Abstract
The theory of adaptive control of feedback linearizable systems is app lied to designing the control of wing rock motion with the extension o f the technique to include tracking. The adaptation law is designed to adjust the aerodynamic parameters in the model. Precise tracking and maximum performance can be achieved if sufficient rolling moment deriv ative because of lateral control components are available. Case studie s and simulation are carried out to illustrate the results.