Abstract:
This paper presents a nonlinear H∞ controller for the rejection of input disturbances in a fixed wing UAV. The proposed controller acts in all states of a complete nonlin...Show MoreMetadata
Abstract:
This paper presents a nonlinear H∞ controller for the rejection of input disturbances in a fixed wing UAV. The proposed controller acts in all states of a complete nonlinear dynamic model. Simulation results show that the aircraft is successfully maintained in the desired stable condition after two different disturbances: a finite pulse and noise.
Date of Conference: 19-21 December 2011
Date Added to IEEE Xplore: 26 January 2012
ISBN Information: