251. Avionic Air Data Sensors Fault Detection and Isolation by means of Singular Perturbation and Geometric Approach
- Author
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Paolo Castaldi, Nicola Mimmo, Silvio Simani, Castaldi, Paolo, Mimmo, Nicola, and Simani, Silvio
- Subjects
Autopilot avionics ,0209 industrial biotechnology ,Singular perturbation ,Engineering ,Aircraft ,Air data sensors, Aircraft, Autopilot avionics, Fault detection and isolation, Nonlinear geometric approach, singular perturbation ,media_common.quotation_subject ,Fidelity ,02 engineering and technology ,lcsh:Chemical technology ,Biochemistry ,Article ,Fault detection and isolation ,Analytical Chemistry ,Economica ,020901 industrial engineering & automation ,Control theory ,singular perturbation ,NonLinear Geometric Approach ,fault detection and isolation ,aircraft ,autopilot avionics ,air data sensors ,0202 electrical engineering, electronic engineering, information engineering ,lcsh:TP1-1185 ,Isolation (database systems) ,Electrical and Electronic Engineering ,Autopilot avionic ,Instrumentation ,media_common ,Air data sensor ,business.industry ,Ambientale ,Control engineering ,Nonlinear geometric approach ,Avionics ,Atomic and Molecular Physics, and Optics ,Nonlinear system ,Scale separation ,Air data sensors ,020201 artificial intelligence & image processing ,Phugoid ,business - Abstract
Singular Perturbations represent an advantageous theory to deal with systems characterized by a two-time scale separation, such as the longitudinal dynamics of aircraft which are called phugoid and short period. In this work, the combination of the NonLinear Geometric Approach and the Singular Perturbations leads to an innovative Fault Detection and Isolation system dedicated to the isolation of faults affecting the air data system of a general aviation aircraft. The isolation capabilities, obtained by means of the approach proposed in this work, allow for the solution of a fault isolation problem otherwise not solvable by means of standard geometric techniques. Extensive Monte-Carlo simulations, exploiting a high fidelity aircraft simulator, show the effectiveness of the proposed Fault Detection and Isolation system.
- Published
- 2017