Title :
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
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;
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.2009.5192169