Input-dependent threshold function for an actuator fault detection filter

IFAC Proceedings Volumes (IFAC-PapersOnline)

Volumn 16, Issue , 2005, Pages 211-216

  Rotstein, Hector ^b   Ingvalson, Ryan ^a   Keviczky, Tamas ^a   Balas, Gary ^a  

^a UNIVERSITY OF MINNESOTA   (United States)

^b TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

Author keywords

Aerospace computer control; Fault detection; H infinity control; Threshold functions; Uncertainty

Indexed keywords

AIRCRAFT CONTROL; AIRCRAFT DETECTION; FINITE DIFFERENCE METHOD; FLIGHT CONTROL SYSTEMS; FLIGHT SIMULATORS; SAFETY ENGINEERING; UNCERTAINTY ANALYSIS; UNMANNED AERIAL VEHICLES (UAV);

ACTUATOR FAULT DETECTION; CONTROLLER RECONFIGURATION; DETECTION CAPABILITY; FAULT DETECTION FILTER (FDF); H -INFINITY CONTROLS; SAFETY CRITICAL COMPONENTS; THRESHOLD FUNCTIONS; UNCERTAINTY;

FAULT DETECTION;

EID: 79960714657     PISSN: 14746670     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.3182/20050703-6-cz-1902.01996     Document Type: Conference Paper

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