Structural analysis approach to fault diagnosis with application to fixed-wing aircraft motion

Proceedings of the American Control Conference

Volumn 5, Issue , 2002, Pages 3949-3954

  Izadi Zamanabadi, Roozbeh ^a  

^a AALBORG UNIVERSITY   (Denmark)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CONSTRAINT THEORY; FAULT TREE ANALYSIS; MATHEMATICAL MODELS; STRUCTURAL ANALYSIS; WINGS;

FAULT DIAGNOSIS; FIXED WING AIRCRAFT MOTION;

CONTROL SYSTEM ANALYSIS;

EID: 0036061017     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/acc.2002.1024546     Document Type: Conference Paper

References (10)

1. What is fault-tolerant control?
2. Approche structurelle de la conception de systèmes de surveillance pour des procédé industriels complexes
3. Applied and algorithmic graph theory
4. Characterization of the canonical components of a structural graph for fault detection in large scale industrial plants
5. Coverings of bipartite graphs
6. A structural analysis method formulation for fault-tolerant control system designntr
7. A geometric approach to failure detection and identification in linear systems
8. Analysis of the techniques of robust eigenstructure assignment with application to aircraft control