NDLI: UAV airplane control system design via time-scale separation technique

Content Provider	IEEE Xplore Digital Library
Author	Yurkevich, V.D. Blachuta, M. Janusz, W. Czyba, R.
Copyright Year	2013
Description	Author affiliation: Novosibirsk State Tech. Univ., Novosibirsk, Russia (Yurkevich, V.D.) \|\| Silesian Univ. of Technol., Gliwice, Poland (Blachuta, M.; Janusz, W.; Czyba, R.)
Abstract	The problem of UAV airplane trajectory tracking control system design is treated in the presence of uncertain aerodynamics and unknown external wind disturbances. The cascaded control system structure is considered where the feedback loop of the each cascade is designed by inducing of two-time-scale motions in the closed-loop system such that the controller dynamics is a singular perturbation with respect to the airplane dynamics. The time-scale separation method is used to analyze of fast and slow motions in the closed-loop system and in order to get explicit expressions for evaluation of the controller parameters. Stability of fast-motion transients is maintained by selection of controller parameters while the slow motion behavior of such controlled variables as Euler angels and angular velocities exhibit the desired transient's performances for a large range of aerodynamic characteristics variations and external wind disturbances. Simulation results are included to validate the effectiveness of the discussed design methodology.
Starting Page	349
Ending Page	355
File Size	527468
Page Count	7
File Format	PDF
ISBN	9781479907618
ISSN	2325419X
e-ISBN	9781479907625
DOI	10.1109/EDM.2013.6642012
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2013-07-01
Publisher Place	Russia
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Closed loop systems Equations Transient analysis Noise Mathematical model Nonlinear systems trajectory tracking UAV control singular perturbation
Content Type	Text
Resource Type	Article

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