Please use this identifier to cite or link to this item: http://scholarbank.nus.edu.sg/handle/10635/115477
Title: Reliable H∞ Aircraft flight controller design against faults with state/Output feedback
Authors: Feng, L.
Wang, J.
Poh, E.
Liao, F. 
Keywords: Control
Control Surface impairment; State/Output Feedback
Flight control
H∞
Linear Matrix Inequalities
Lyapunov Function
Outage Fault
Issue Date: 2005
Source: Feng, L.,Wang, J.,Poh, E.,Liao, F. (2005). Reliable H∞ Aircraft flight controller design against faults with state/Output feedback. Proceedings of the American Control Conference 4 : 2664-2669. ScholarBank@NUS Repository.
Abstract: This paper presents a novel H∞ formulation to design a reliable tracking controller for a discrete LTI aircraft system against actuator outage faults and control surface impairment modelled as polytopic uncertainties. Both the state-feedback and output-feedback cases are considered. The approach is based on multiobjective optimization using several parameter dependent Lyapunov functions, each corresponding to a vertex of the uncertainty polytope. The main advantage of this approach with respect to the other well-known techniques is the reduced conservativeness. In the output-feedback case, a new Linear Matrix Inequality (LMI) formulation is derived and solved by an iterative LMI (ILMI) algorithm. Finally, the application to a nonlinear F-16 aircraft model with actuator outage faults and control surface impairment illustrates the effectiveness of the proposed approach. © 2005 AACC.
Source Title: Proceedings of the American Control Conference
URI: http://scholarbank.nus.edu.sg/handle/10635/115477
ISSN: 07431619
Appears in Collections:Staff Publications

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