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Disturbance rejection in a fixed wing UAV using nonlinear H∞ state feedback | IEEE Conference Publication | IEEE Xplore

Disturbance rejection in a fixed wing UAV using nonlinear H∞ state feedback


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 More

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
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Conference Location: Santiago, Chile

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