Nonlinear control design and stability analysis of a small-scale unmanned helicopter

被引:0
|
作者
Zhang, Lin [1 ]
Ding, Zhengtao [1 ]
机构
[1] Univ Manchester, Sch Elect & Elect Engn, Control Syst Ctr, Manchester M13 9PL, Lancs, England
关键词
IMPLEMENTATION;
D O I
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中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
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.
引用
收藏
页码:1662 / 1667
页数:6
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