DocumentCode :
3283312
Title :
Transitions between level flight and hovering for a fixed-wing mini aerial vehicle
Author :
Myrand-Lapierre, Vincent ; Desbiens, A. ; Gagnon, E. ; Wong, Francis ; Poulin, E.
Author_Institution :
Dept. of Electr. & Comput. Eng., Univ. Laval, Quebec City, QC, Canada
fYear :
2010
fDate :
June 30 2010-July 2 2010
Firstpage :
530
Lastpage :
535
Abstract :
This article describes a control strategy to bridge the autonomous transition between level and hovering flight of a fixed-wing mini-aerial vehicle. These autonomous transitions, combined with the level-flight and hovering modes, would permit dangerous missions like reconnaissance in hostile or restricted areas. Then, there are four flight modes during a mission : the level-flight, the level-flight to hovering (L2H), the hovering, and the hovering to level-flight (H2L). The model structures for both level-flight and hovering modes are based on the linearization of a six-degree-of-freedom rigid body model of a fixed-wing mini-aerial vehicle. Controllers for both main flying modes are presented. The L2H mode is managed by the level-flight controller, whereas the H2L is managed by the hovering controller. A systematic approach based on a logic-based switching supervisor is developed to manage the transition between modes. Experimental results of a mini-aerial vehicle testbed which uses the switching supervisor are presented.
Keywords :
aerospace control; aircraft; remotely operated vehicles; autonomous transition; fixed-wing mini aerial vehicle; hovering controller; level-flight controller; logic-based switching; Adaptive control; Aircraft; Linear feedback control systems; Marine vehicles; Mobile robots; Programmable control; Reconnaissance; Remotely operated vehicles; Testing; Unmanned aerial vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2010
Conference_Location :
Baltimore, MD
ISSN :
0743-1619
Print_ISBN :
978-1-4244-7426-4
Type :
conf
DOI :
10.1109/ACC.2010.5530875
Filename :
5530875
Link To Document :
بازگشت