DocumentCode
9516
Title
Automatic Control of Aircraft in Longitudinal Plane During Landing
Author
Lungu, Romulus ; Lungu, Mircea ; Grigorie, L.T.
Author_Institution
Fac. of Electr. Eng., Univ. of Craiova, Craiova, Romania
Volume
49
Issue
2
fYear
2013
fDate
Apr-13
Firstpage
1338
Lastpage
1350
Abstract
Automatic control of aircraft during landing is discussed and a new structure of automatic landing system (ALS) is designed using the dynamic inversion concept and proportional-integral-derivative (PID) controllers in conventional and fuzzy variants. Theoretical results are validated by numerical simulations in the absence or presence of wind shears and sensor errors.
Keywords
aircraft control; aircraft landing guidance; fuzzy control; sensors; three-term control; ALS; PID; automatic aircraft control; automatic landing system; dynamic inversion concept; fuzzy variants; longitudinal plane; proportional-integral-derivative controllers; sensor errors; wind shears;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.2013.6494418
Filename
6494418
Link To Document