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  • https://doi.org/10.1109/acc.2005.1470370Copy DOI Icon

Reliable H//sub∞/ aircraft flight controller design against faults with state/output feedback

  • Jun 8, 2005
  • Le Feng +3 more
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Abstract

This paper presents a novel H/spl infin/ 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 style-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.

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