Title :
The dual diagnosis of an airplane command
Author :
Grigore-Muler, O.
Author_Institution :
Fac. of Aerosp. Eng., Univ. Politeh. Bucharest, Bucharest
Abstract :
As part of a programme investigating the design of new airplanes the aeronautics and automatics engineers are studying aircraft and systems which would operate with greatly reduced stability margins and would, as a result, be totally dependent on computer control for the safety of a flight. Therefore these computer systems generally used to provide active control are required to have efficient diagnosis systems. A fuzzy dual diagnosis system for the command of a commercial airplane is presented.
Keywords :
aerospace computing; aerospace safety; aircraft; aircraft control; control engineering computing; fault diagnosis; fuzzy control; active control; aircraft; airplane command; computer control; flight. safety; fuzzy dual diagnosis system; stability margins; Aerospace control; Aerospace engineering; Aerospace safety; Air safety; Aircraft propulsion; Airplanes; Automatic control; Control systems; Design engineering; Stability;
Conference_Titel :
Optimization of Electrical and Electronic Equipment, 2008. OPTIM 2008. 11th International Conference on
Conference_Location :
Brasov
Print_ISBN :
978-1-4244-1544-1
Electronic_ISBN :
978-1-4244-1545-8
DOI :
10.1109/OPTIM.2008.4602471
