DocumentCode :
622693
Title :
Nonlinear control design and stability analysis of a small-scale unmanned helicopter
Author :
Lin Zhang ; Zhengtao Ding
Author_Institution :
Control Syst. Centre, Univ. of Manchester, Manchester, UK
fYear :
2013
fDate :
12-14 June 2013
Firstpage :
1662
Lastpage :
1667
Abstract :
The main focus of this paper is to design nonlinear controllers and analyse stability for a miniature unmanned helicopter. Our work is to utilize nonlinear control methodology to command dynamics of unmanned helicopter which has been divided into slower translational dynamics (outer-loop) and faster orientation dynamics (inner-loop), thus exhibiting hierarchical structure. The attitude angles and position which separately belong to the inner-loop and the outer-loop can be independently controlled by backstepping control strategy. Stability analysis of the helicopter system including flapping dynamics has been presented after designing controllers.
Keywords :
attitude control; autonomous aerial vehicles; control system synthesis; helicopters; nonlinear control systems; stability; vehicle dynamics; attitude angles; backstepping control strategy; flapping dynamics; helicopter system; hierarchical structure; miniature unmanned helicopter; nonlinear control design; orientation dynamics; small-scale unmanned helicopter; stability analysis; translational dynamics; Dynamics; Equations; Helicopters; Mathematical model; Rotors; Stability analysis; Tunneling magnetoresistance;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Automation (ICCA), 2013 10th IEEE International Conference on
Conference_Location :
Hangzhou
ISSN :
1948-3449
Print_ISBN :
978-1-4673-4707-5
Type :
conf
DOI :
10.1109/ICCA.2013.6565166
Filename :
6565166
Link To Document :
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