Title :
Robust H-infinity Tracing Control of 3-DOF Helicopter Model
Author :
Wang Xiuyan ; Zhao Changli ; Li Zongshuai
Author_Institution :
Civil Aviation Univ. of China, Tianjin, China
Abstract :
The stability and anti-jamming of 3-DOF helicopter model system are weak because of non-linearity and parameter uncertainty, so H-infinity mixed sensitivity laws are adopted to design trajectory tracking controller. Firstly, the bounded non-linear parameters are transformed into the uncertainty of parameters and added by inherent parameters perturbation it composes the linear uncertainty model. The H-infinity control method based on mixed sensitivity is adopted. By setting the weighting function of sensitivity and complementary sensitivity, the multitask controller of disturbance rejection and robust tracking is translated to a stander H-infinity controller of regulate problem. Simulation results demonstrate that the trajectory of helicopter attitude tracks well and system robust stability is improved.
Keywords :
H¿ control; helicopters; position control; stability; 3DOF helicopter model; parameter uncertainty; robust H-infinity tracing control; robust stability; robust tracking; trajectory tracking controller; weighting function; Equations; Fuzzy logic; H infinity control; Helicopters; Optimal control; Robust control; Robust stability; Trajectory; Uncertain systems; Uncertainty; Mixed Sensitivity and Uncertainty; Three-degree of Freedom Helicopter; Trajectory Tracking;
Conference_Titel :
Measuring Technology and Mechatronics Automation (ICMTMA), 2010 International Conference on
Conference_Location :
Changsha City
Print_ISBN :
978-1-4244-5001-5
Electronic_ISBN :
978-1-4244-5739-7
DOI :
10.1109/ICMTMA.2010.613