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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creator Lungu, R.
Lungu, M.
Grigorie, L. T.
description 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.
doi_str_mv 10.1109/TAES.2013.6494418
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subjects Aerospace control
Aircraft
Aircraft components
Automatic control
Computer simulation
Equations
Fuzzy
Landing
Mathematical model
Nonlinear dynamical systems
Proportional integral derivative
Trajectory
Vectors
Wind shear
title Automatic Control of Aircraft in Longitudinal Plane During Landing
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