Title :
Research of Handling Characteristics of Pilot in Carrier Landing
Author :
Qidan Zhu ; Enjiao Zhao ; Wen Zhang ; Zhi Zhang
Author_Institution :
Coll. of Autom., Harbin Eng. Univ. Harbin, Harbin, China
Abstract :
The pilot control characteristics are key influence factors of the carrier landing security, so it is very necessary to study the pilot control model. The control structure of the longitudinal carrier landing system based on the typical modeling theory is established by MATLAB/Simulink on the basis of the plane model of F/A-18A. The pilot control laws are studied by simulation, the method of selecting parameter is also presented, and the tracking ability of pilot control system is verified through simulation. The carrier aft flow and movement model of aircraft carriers are also introduced into the control model, and the handing characteristics of pilot is researched in this case. The simulation results show that the designed control system have a good tracking control ability, the anti-interfere ability is also strong, and can effectively restrain the carrier aft flow influence, meet the requirements of carrier landing safely.
Keywords :
aircraft control; control engineering computing; control system synthesis; mathematics computing; position control; F-A-18A plane model; MATLAB-Simulink; aircraft carriers; anti-interfere ability; carrier aft flow; carrier landing security; control structure; control system design; handling characteristics; longitudinal carrier landing system; movement model; pilot control characteristics; tracking control ability; typical modeling theory; Aerodynamics; Aerospace control; Aircraft; Atmospheric modeling; Mathematical model; Tracking; Transfer functions; Aft flow; Pilot Model; deck movement;
Conference_Titel :
Instrumentation, Measurement, Computer, Communication and Control (IMCCC), 2012 Second International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4673-5034-1
DOI :
10.1109/IMCCC.2012.162
