Title :
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
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;
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
DOI :
10.1109/CCDC.2009.5192168
