Diagnosis of actuator faults using LPV-gain scheduling techniques

We present a new approach for the synthesis of robust fault detection lters for the model based diagnosis of actuator faults. The underlying synthesis model is a linear parameter varying (LPV) description obtained using a combination of analytic and numerical parameter tting techniques. The actuator LPV model contains uncertain parameters which are partly measurable, thus can be used for gain scheduling, and partly not measurable, for which robustness must be ensured. The detector synthesis approach is basically a parametric nullspace method combined with min-max parameter tting. The synthesis technique is applied to the diagnosis of two classes of actuator faults for a civil aircraft: elevator runaway and elevator jamming at null position.

[1]  H.-D. Joos,et al.  A multiobjective optimisation-based software environment for control systems design , 2002, Proceedings. IEEE International Symposium on Computer Aided Control System Design.

[2]  Guilhem Puyou,et al.  Clearance Benchmark for a Civil Aircraft , 2012 .

[3]  J. Doyle,et al.  Robust and optimal control , 1995, Proceedings of 35th IEEE Conference on Decision and Control.

[4]  G. Vinnicombe Frequency domain uncertainty and the graph topology , 1993, IEEE Trans. Autom. Control..

[5]  Andras Varga,et al.  On parametric solution of fault detection problems , 2011 .

[6]  Harald Pfifer,et al.  Generation of Optimal Linear Parametric Models for LFT-Based Robust Stability Analysis and Control Design , 2011, IEEE Transactions on Control Systems Technology.

[7]  Ali Zolghadri,et al.  Nonlinear Observer-Based OFC Detection for A380 Aircraft. , 2009 .