This paper presents sliding mode control (SMC) to aircraft automatic landing system (ALS), and uses genetic algorithm (GA), particle swarm optimization (PSO) and chaos particle swarm optimization (CPSO) to adjust controller parameters. When wind shear is encountered, the aircraft automatic landing system can not be used in such environment during serious wind speed changes. The proposed intelligent control scheme can help the pilots guide the aircraft to a safe landing in wind shear condition. PID control and cerebella model articulation controller (CMAC) are applied to the controller design.
A Hybrid Intelligent System for Wind Shear Encountered Aircraft Landing Control
Applied Mechanics and Materials ; 764-765 ; 592-596
2015-05-28
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Control of aircraft landing approach in wind shear
AIAA | 1987
|Predictive Controller for Aircraft Landing under Wind Shear
Trans Tech Publications | 2014
|Wind Shear Effects on the Landing of Aircraft
AIAA | 1975
|Some Fatigue Problems Encountered in the Design of an Aircraft Landing Gear
Emerald Group Publishing | 1968
|