The application and study of fizzy immune PID in DCS fight simulation turntable

Author

Luo, Yunlin ; Gao, Jinglong

Author_Institution

Aeronaut. Autom. Coll., Civil Aviation Univ. of China, Tianjin, China

fYear

2009

fDate

17-19 June 2009

Firstpage

3323

Lastpage

3326

Abstract

In order to study automatic flight control system and inertial navigation system in civil aircraft, and to test the tracking performance in real moving targets, a three-axis fight simulation turntable is devised based on fizzy immune PID. DCS is used in this turntable, which is motivated by DC torque motor. Photoelectric coded disks together with transform coding interface works as feedback components. The system falls into upper and lower computer. It has high location capability, stationary rate, low distortion and excellent dynamics.

Keywords

aircraft control; control system synthesis; discrete systems; inertial navigation; three-term control; DC torque motor; automatic flight control system; civil aircraft; fizzy immune PID; inertial navigation system; photoelectric coded disks; three-axis fight simulation turntable; transform coding interface; Aerospace control; Aerospace simulation; Aircraft navigation; Automatic testing; Computational modeling; Distributed control; Inertial navigation; System testing; Target tracking; Three-term control; DCS; Fizzy Immune PID; Simulation Turntable;

fLanguage

English

Publisher

ieee

Conference_Titel

Control and Decision Conference, 2009. CCDC '09. Chinese

Conference_Location

Guilin

Print_ISBN

978-1-4244-2722-2

Electronic_ISBN

978-1-4244-2723-9

Type

conf

DOI

10.1109/CCDC.2009.5192168

Filename

5192168