DocumentCode
424989
Title
Constrained nonlinear tracking control for small fixed-wing unmanned air vehicles
Author
Ren, Wei ; Beard, Randal W.
Author_Institution
Dept. of Electr. & Comput. Eng., Brigham Young Univ., Provo, UT, USA
Volume
5
fYear
2004
fDate
June 30 2004-July 2 2004
Firstpage
4663
Abstract
This paper considers the problem of constrained nonlinear tracking control for small fixed-wing unmanned air vehicles equipped with longitudinal and lateral autopilots. Four different controllers based on SDRE, Sontag´s formula, geometric mean, and aggressive selection from the feasible control set are proposed and compared to show their strengths and weaknesses under different application scenarios. Issues of measurement noise and input uncertainties are also addressed under the input-to-state stability framework. The effectiveness of the approaches is demonstrated through detailed simulation studies.
Keywords
Riccati equations; aerospace robotics; control system synthesis; nonlinear control systems; remotely operated vehicles; stability; tracking; constrained nonlinear tracking control; geometric mean; input-to-state stability framework; lateral autopilot; longitudinal autopilot; measurement noise; small fixed-wing unmanned air vehicles; state dependent Riccati equation;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2004. Proceedings of the 2004
Conference_Location
Boston, MA, USA
ISSN
0743-1619
Print_ISBN
0-7803-8335-4
Type
conf
Filename
1384048
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