This paper presents the results of a novel sensor fault tolerant control scheme based on a robust sliding mode observer. In order to ensure wide coverage of the flight envelope and robustness against uncertainty, the observer is designed using a robust LPV model based method. Fault tolerance is achieved by exploiting the capability of the robust LPV sliding mode observer to provide f ault reconstruction. This allows the faulty measurement to be corrected before it is used in the controller computations, and therefore enables the controller to maintain the required performance. The correction of the faulty measurement means that there is no requirement for the development of a new controller in order to achieve tolerance to faults. Two sets of results are presented to highlight the potential of the proposed scheme -one using a single run at three chosen flight conditions (to provide details of performance of the scheme across the flight envelope) and the second is based on parametric runs developed for an industrial evaluation process. All the results are obtained using a nonlinear benchmark model and demonstrate the potential of the proposed scheme.
NomenclatureADDSAFE = Advanced Fault Diagnosis for Sustainable Flight Guidance and Control FDI, FDD, FTC = Fault detection and isolation, fault detection and diagnosis, fault tolerant control LTI, LPV = Linear time invariant, linear parameter varying p, r = roll and yaw rate Vtas, Vcas = true and conventional air speed ϕ, β, ψ = roll, sideslip, yaw angle h = altitude IR = field of real numbers ρ = LPV parameter ρ, ρ = minimum and maximum value