The study of actuator controller based on fuzzy self-adaptive PID

Author

Luo, Yunlin ; Liu, Xiaohua

Author_Institution

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

fYear

2009

fDate

17-19 June 2009

Firstpage

3327

Lastpage

3331

Abstract

Aiming at requirement of the driving and control system in the plane actuator, teaching the mechanical & electrical system of aircraft and improving students´ hands-on capacity, we introduce a design Actuator Loop system´s control, which is designed on the basis of a SPCE061 A MCU. This article briefly introduced Actuator Loop system´s hardware structure, software design which consists of network deliver and serial communication and Fuzzy adaptive incremental PID control simulation in detail in the paper. Through Simulation and experiments we can make a conclusion that the controller has a tight structure, a low cost, and also has a good reliability and practicability.

Keywords

actuators; adaptive control; aircraft control; control engineering education; control system synthesis; fuzzy control; intelligent control; three-term control; SPCE061A MCU; adaptive control; aircraft; control system; design actuator loop system control; driving system; electrical system; fuzzy control; fuzzy self-adaptive PID; incremental PID control simulation; mechanical system; network delivery; plane actuator; serial communication; student hands-on capacity; Actuators; Aerospace control; Aircraft; Communication system control; Control systems; Education; Fuzzy control; Hardware; Software design; Three-term control; Electric Actuator; Fuzzy self-adaptive PID; SPCE061A;

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.2009.5192169

Filename

5192169