Robust trajectory tracking control for a laboratory helicopter

被引:23
|
作者
Liu, Hao [1 ,3 ]
Yu, Yao [2 ]
Zhong, Yisheng [3 ]
机构
[1] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China
[2] Univ Sci & Technol Beijing, Sch Automat & Elect Engn, Beijing 100083, Peoples R China
[3] Tsinghua Univ, Dept Automat, TNList, Beijing 100084, Peoples R China
基金
中国国家自然科学基金;
关键词
Laboratory helicopter; Robust nonlinear control; Feedback linearization; COMMAND-FILTERED COMPENSATION; ATTITUDE-CONTROL; CONTROL DESIGN;
D O I
10.1007/s11071-014-1324-2
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper presents a robust nonlinear control strategy to deal with the trajectory tracking control problem for a laboratory helicopter. The helicopter model is considered as a nominal one with uncertainties such as unmodeled nonlinear dynamics, parametric uncertainties, and external disturbances. The proposed control approach incorporates the feedback linearization technique (FLT) and the signal compensation technique. The FLT is first applied to achieve the linearization of the nominal nonlinear model for reducing the conservation of the robust compensator design. A nominal controller based on the linear quadratic regulation method is designed for the linearized nominal system, whereas a robust compensator is introduced to restrain the influences of the uncertainties. It is shown that the trajectory tracking errors of the closed-loop system are ultimately bounded, and the boundaries can be specified by choosing the controller parameters. Simulation and experimental results on the lab helicopter verify the effectiveness of the proposed method.
引用
收藏
页码:621 / 634
页数:14
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