Design of robust redundancy relations for a semi-scale YF-22 aircraft model

Control Engineering Practice

Volumn 17, Issue 7, 2009, Pages 773-786

  Fravolini, Mario Luca ^a   Campa, Giampiero ^b  

^a UNIVERSITY OF PERUGIA   (Italy)

^b West Virginia University   (United States)

Author keywords

Fault diagnosis; Fault isolation; Nonlinear filters; Sensors; Symbolic computation; Unmanned aerial vehicles

Indexed keywords

DIAGNOSTIC SOFTWARES; ELIMINATION METHODS; FAULT DETECTION AND ISOLATIONS; FAULT DIAGNOSIS; FAULT ISOLATION; FAULT SIGNATURES; FLIGHT DATUM; HIGH ORDER DERIVATIVES; MEASUREMENT NOISE; MINIMUM COSTS; MODELING ERRORS; NON-LINEAR UNCERTAINTIES; NONLINEAR DYNAMIC EQUATIONS; NONLINEAR FILTERS; NUMERICAL COMPUTATIONS; PERFORMANCE CRITERION; RESIDUAL EQUATIONS; ROBUSTIFICATION; SENSORS AND ACTUATORS; SYMBOLIC COMPUTATION;

ACOUSTIC NOISE; ELECTRIC FAULT CURRENTS; FAULT DETECTION; FIR FILTERS; MEASUREMENT ERRORS; NEURAL NETWORKS; NONLINEAR FILTERING; REMOTELY OPERATED VEHICLES; RESEARCH AIRCRAFT; SENSORS; SPURIOUS SIGNAL NOISE; STRUCTURAL ANALYSIS; UNCERTAINTY ANALYSIS; UNMANNED AERIAL VEHICLES (UAV);

NONLINEAR EQUATIONS;

EID: 67349256091     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.conengprac.2008.12.006     Document Type: Article

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