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Fault tolerant flight control system design for UAV's using Nonlinear Model Predictive Control

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4 Author(s)
Rudaba Khan ; Department of Mathematics and Geospatial Sciences at RMIT University, Melbourne, Australia ; Paul Williams ; Robin Hill ; Cees Bil

A design for a reconfigurable fault tolerant flight control system for an unmanned air vehicle has been proposed in this paper. Due to the severe nonlinearities inherent in an aircraft system Non-Linear Model Predictive Control has been chosen for the controller design. The results obtained show good aircraft performance in the event of a control surface failure.

Published in:

Australian Control Conference (AUCC), 2011

Date of Conference:

10-11 Nov. 2011