Automatic Control of Aircraft in Longitudinal Plane During Landing

Automatic Control of Aircraft in Longitudinal Plane During Landing

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 si...

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Veröffentlicht in:IEEE transactions on aerospace and electronic systems 2013-04, Vol.49 (2), p.1338-1350
Hauptverfasser: Lungu, R., Lungu, M., Grigorie, L. T.
Format: Artikel
Sprache:eng
Schlagworte:
Aerospace control
Aircraft
Aircraft components
Automatic control
Computer simulation
Equations
Fuzzy
Landing
Mathematical model
Nonlinear dynamical systems
Proportional integral derivative
Trajectory
Vectors
Wind shear
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Beschreibung
Zusammenfassung: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.
ISSN:0018-9251
1557-9603
DOI:10.1109/TAES.2013.6494418