Design of residual generators and adaptive filters for the FDI of aircraft model sensors

Control Engineering Practice

Volumn 18, Issue 5, 2010, Pages 449-459

  Castaldi, P ^a   Geri, W ^a   Bonfe M ^b   Simani, S ^b   Benini, M ^b  

^a UNIVERSITY OF BOLOGNA   (Italy)

^b UNIVERSITY OF FERRARA   (Italy)

Author keywords

Adaptive filters; Aircraft nonlinear model; Fault estimation; Input output sensor fault detection isolation; Nonlinear geometric approach; Polynomial methods

Indexed keywords

FAULT ESTIMATION; GEOMETRIC APPROACHES; INPUT-OUTPUT; NON-LINEAR MODEL; POLYNOMIAL METHODS; SENSOR FAULT DETECTION;

ADAPTIVE FILTERING; ADAPTIVE FILTERS; AIRCRAFT; COMPUTER SIMULATION; ELECTRIC FILTERS; FAULT DETECTION; FLIGHT SIMULATORS; FUZZY CONTROL; GEOMETRY; MEASUREMENT ERRORS; NONLINEAR ANALYSIS; POLYNOMIALS; SENSORS;

AIRCRAFT DETECTION;

EID: 77952290105     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.conengprac.2008.11.006     Document Type: Article

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