DocumentCode
2001785
Title
Robust Receding Horizon Control of A Tri-Turbofan Airship
Author
Trevino, Roseann ; Frye, Michael ; Franz, Justin A. ; Qian, Chunjiang
Author_Institution
Univ. of Texas at San Antonio, San Antonio
fYear
2007
fDate
May 30 2007-June 1 2007
Firstpage
671
Lastpage
676
Abstract
This paper examines the use of receding horizon control technique to stabilize a 6 degree-of-freedom model of a tri-turbofan remote controlled indoor airship. The lateral-directional dynamics of the airship are simulated using a linear parameter varying force model that has been verified against actual flight test data. Due to the varying dynamics of the airship as it transitions between different flight modes, the problem of developing robust controllers due to model uncertainty becomes challenging. A receding horizon control implementation formulated as a linear matrix inequality optimization problem is implemented in order to introduce robustness to the changing dynamics of the airship model.
Keywords
aircraft control; linear matrix inequalities; optimisation; predictive control; remotely operated vehicles; robust control; vehicle dynamics; lateral-directional dynamics; linear matrix inequality optimization problem; linear parameter varying force model; model uncertainty; remote controlled indoor airship; robust receding horizon control; tri-turbofan airship; Analytical models; Automatic control; Cybernetics; Laboratories; Linear matrix inequalities; Mathematical model; Robust control; Testing; Uncertainty; Vehicle dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Automation, 2007. ICCA 2007. IEEE International Conference on
Conference_Location
Guangzhou
Print_ISBN
978-1-4244-0817-7
Electronic_ISBN
978-1-4244-0818-4
Type
conf
DOI
10.1109/ICCA.2007.4376439
Filename
4376439
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