Abstract:
In this paper, the control of a quad-rotor helicopter is considered. The nonlinear model of the quad-rotor is transformed to a linear model subject to time-varying parame...Show MoreMetadata
Abstract:
In this paper, the control of a quad-rotor helicopter is considered. The nonlinear model of the quad-rotor is transformed to a linear model subject to time-varying parameters called linear parameter-varying (LPV) systems. Then, the composite quadratic Lyapunov function and the quadratic cost function are used to find the optimal state feedback gain. To obtain the optimal solution, the LPV control problem is cast to the semi-definite programing problem with a set of Linear Matrix Inequality (LMI) constraints. The simulation results are provided to demonstrate the effectiveness of the proposed method.
Date of Conference: 16-18 May 2012
Date Added to IEEE Xplore: 02 August 2012
ISBN Information:
Department of Electrical Engineering, Faculty of Engineering, Chulalongkorn University, Bangkok, Thailand
Department of Electrical Engineering, Faculty of Engineering, Chulalongkorn University, Bangkok, Thailand
Department of Electrical Engineering, Faculty of Engineering, Chulalongkorn University, Bangkok, Thailand
Department of Electrical Engineering, Faculty of Engineering, Chulalongkorn University, Bangkok, Thailand