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.
Automatic Control of Aircraft in Longitudinal Plane During Landing
IEEE Transactions on Aerospace and Electronic Systems ; 49 , 2 ; 1338-1350
01.04.2013
15550699 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch