DocumentCode
2858979
Title
Nonlinear aircraft modeling and controller design for target tracking
Author
Rizwan, Y. ; Waslander, S.L. ; Nielsen, C.
Author_Institution
Dept. of Me chanical & Mechatron. Eng., Univ. of Waterloo, Waterloo, ON, Canada
fYear
2011
fDate
June 29 2011-July 1 2011
Firstpage
3191
Lastpage
3196
Abstract
In order to provide a novel perspective for videography of high speed sporting events, a highly capable trajectory tracking control methodology is developed for small scale Unmanned Aerial Vehicles (UAVs). The proposed controller combines dynamic inversion with linear tracking control using the internal model approach, and relies on a trajectory generating exosystem generated from available target training data. Three different aircraft models are presented each with increasing levels of complexity, in an effort to identify the simplest controller that yields acceptable performance. The dynamic inversion and linear tracking control laws are derived for each model, and simulation results are presented for tracking of elliptical and periodic trajectories.
Keywords
aerospace robotics; aircraft control; control system synthesis; mobile robots; nonlinear control systems; periodic control; position control; remotely operated vehicles; sport; target tracking; UAV; controller design; dynamic inversion; elliptical trajectory; high speed sporting event; internal model approach; linear tracking control; nonlinear aircraft modeling; periodic trajectory; small scale unmanned aerial vehicle; target tracking; trajectory generating exosystem; trajectory tracking control; videography; Aerodynamics; Aerospace control; Aircraft; Atmospheric modeling; Mathematical model; Target tracking; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference (ACC), 2011
Conference_Location
San Francisco, CA
ISSN
0743-1619
Print_ISBN
978-1-4577-0080-4
Type
conf
DOI
10.1109/ACC.2011.5991514
Filename
5991514
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