Research on Trajectory Tracking Control of Aircraft in Carrier Landing

Author

Qidan Zhu ; Bing Qiu

Author_Institution

Coll. of Autom., Harbin Eng. Univ., Harbin, China

fYear

2013

fDate

21-23 Sept. 2013

Firstpage

1452

Lastpage

1455

Abstract

Since the landing of carrier aircraft is of high risk and difficulty, it is necessary to design a locus-tracking control system to ensure the safety of crew on board. In this paper, in reference to the parameters of F/A-18A, the models of lateral and longitudinal motions are built and linearized, respectively. And then, the design of locus-tracking control system in lateral and longitudinal is proposed. A PID controller is introduced into such a system to realize the locus-tracking control of aircraft landing. On basis of attenuation curve method, the parameters of PID controller are obtained. Finally, the design of locus-tracking control system with PID is validated by the simulation results.

Keywords

aerospace safety; aircraft control; control system synthesis; entry, descent and landing (spacecraft); military aircraft; three-term control; tracking; trajectory control; F/A-18A; PID controller; attenuation curve method; carrier aircraft landing; crew safety; lateral motion; locus-tracking control system design; longitudinal motion; trajectory tracking control; Aerospace control; Aircraft; Aircraft propulsion; Atmospheric modeling; Control systems; Force; Mathematical model; PID controller; carrier aircraft; lateral and longitudinal model; trajectory tracking;

fLanguage

English

Publisher

ieee

Conference_Titel

Instrumentation, Measurement, Computer, Communication and Control (IMCCC), 2013 Third International Conference on

Conference_Location

Shenyang

Type

conf

DOI

10.1109/IMCCC.2013.324

Filename

6840714