Adaptive actuator failure compensation for parametric strict feedback systems and an aircraft application.
type: Item
instance of: scholarly article
title: Adaptive actuator failure compensation for parametric strict feedback systems and an aircraft application.
zbMATH Open document ID: 1048.93043
DOI: 10.1016/S0005-1098(03)00219-X
author: Xidong Tang
author: Suresh M. Joshi
author: Gang Tao
published in: Automatica
publication date: 2004-01-26T00:00:00Z
review text: The actuator failure compensation problem is formulated for a nonlinear plant model which is linear in constant parameters and inputs. Two adaptive state feedback control schemes based on two structure conditions are presented which ensure asymptotic output tracking and closed-loop signal boundedness. The nonlinear longitudinal dynamic model of a twin otter aircraft is studied and an adaptive control scheme is applied to this model for output tracking in the presence of unknown parameters and actuator failures. The simulation results are presented.
Mathematics Subject Classification ID: 93B51
Mathematics Subject Classification ID: 93C40
Mathematics Subject Classification ID: 93C95
Mathematics Subject Classification ID: 90B25
zbMATH DE Number: 2032786
zbMATH Keywords: actuator failure
zbMATH Keywords: adaptive control
zbMATH Keywords: aircraft dynamics
zbMATH Keywords: failure compensation
zbMATH Keywords: nonlinear systems
zbMATH Keywords: output tracking
zbMATH Keywords: stability
MaRDI profile type: Publication
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description: scientific article; zbMATH DE number 2032786