NDLI: Nonlinear adaptive control design for non-minimum phase hypersonic vehicle models with minimal control authority

Content Provider	IEEE Xplore Digital Library
Author	Fiorentini, L. Serrani, A.
Copyright Year	2009
Description	Author affiliation: The Ohio State University, Columbus, 43210, USA (Fiorentini, L.; Serrani, A.)
Abstract	The design of a nonlinear robust controller for a non-minimum phase model of the longitudinal dynamics of an air-breathing hypersonic vehicle is presented in this work. When flight-path angle is selected as a regulated output and the elevator is the only control surface available for the pitch dynamics, longitudinal models of air-breathing hypersonic vehicle dynamics exhibit unstable zero-dynamics. The approach proposed in this paper uses a combination of small-gain arguments and adaptive control techniques for the design of a state-feedback controller that achieves asymptotic tracking of velocity and flight-path angle reference trajectories in spite of model uncertainties. The method reposes upon a suitable redefinition of the internal dynamics of a control-oriented model of the vehicle dynamics and uses a time-scale separation between the controlled variables to manage the peaking phenomenon occurring in the system. Simulation results on a full nonlinear vehicle model illustrate the effectiveness of the methodology.
Starting Page	1405
Ending Page	1410
File Size	737386
Page Count	6
File Format	PDF
ISBN	9781424438716
ISSN	01912216
DOI	10.1109/CDC.2009.5400744
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	Adaptive control Vehicle dynamics Aerodynamics Elevators Uncertainty Stability analysis Robust control Feedback Programmable control Thermal stresses
Content Type	Text
Resource Type	Article

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