NDLI: Output tracking of VTOL aircraft with delayed attitude measurements

Content Provider	IEEE Xplore Digital Library
Author	Bo Zhu Xinhua Wang Kai-Yuan Cai
Copyright Year	2009
Description	Author affiliation: National Key Laboratory of Science and Technology on Integrated Control, the Department of Automatic Control, Beijing University of Aeronautics and Astronautics, 100191, China (Bo Zhu; Xinhua Wang; Kai-Yuan Cai)
Abstract	In this paper we consider the flight-trajectory tracking problem of an input-disturbed non-minimum phase vertical takeoff and landing (VTOL) aircraft with delayed attitude measurements. By applying the first-order Padé approximation method to deal with the time delays, the problem is reduced to the output tracking of a new high-order non-minimum phase system without delay, whose dynamics are then separated into minimum-phase and non-minimum-phase parts. By using Devasia's stable noncausal inversion method, the ideal internal states of the non-minimum-phase subsystem are obtained and two error subsystems are ultimately constructed. We propose two low-dimensional sliding mode controllers to stabilize the error subsystems, which can render the overall closed-loop system stable in spite of the existence of disturbances. Simulations are performed to show the main results of this paper.
Starting Page	2528
Ending Page	2533
File Size	687444
Page Count	6
File Format	PDF
ISBN	9781424438716
ISSN	01912216
DOI	10.1109/CDC.2009.5399997
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2009-12-15
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Aerospace control Delay effects Sliding mode control Aircraft manufacture Extraterrestrial measurements Phase measurement Stability Automatic control Delay systems Control systems
Content Type	Text
Resource Type	Article

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