DocumentCode :
2490293
Title :
Experiment and study of electric loading simulator for linear rudder
Author :
Chen, Kang ; Wang, Jianhua ; Yan, Jie ; Huang, Yong
Author_Institution :
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´´an
fYear :
2008
fDate :
25-27 June 2008
Firstpage :
4798
Lastpage :
4802
Abstract :
This paper discussed the design of electric load simulator (ELS) for liner rudder. The ELS uses permanent magnet DC motors as its actuators, and provides aerodynamic force for these aircraftspsila linear servo rudders. The development, architecture and modeling of the ELS are introduced firstly. Then the ELSpsilas dynamic character is studied, and the key technology and the difficulty is analyzed. Next, the control system is designed, using PID control with forward feed control to eliminate the plus force. Subsequently, a simulation is made in MATLAB. In the end, the algorithm of the control system is finished in MS VC++, and is used in the actual loading system. Simulation and experiment results demonstrate that the closed system has less than 5% error between the command force and feedback force and shows the good tracking performance.
Keywords :
DC motors; aircraft control; feedforward; permanent magnet motors; three-term control; MATLAB; MS VC++; PID control; aerodynamic force; aircraft linear servo rudders; command force; electric loading simulator; feedback force; forward feed control; linear rudder; permanent magnet DC motors; Aerodynamics; Control systems; DC motors; Force control; Force feedback; Hydraulic actuators; Magnetic analysis; Mathematical model; Servomechanisms; Three-term control; Computer control; Electric Loading Simulator; System modeling; feed Forward control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Control and Automation, 2008. WCICA 2008. 7th World Congress on
Conference_Location :
Chongqing
Print_ISBN :
978-1-4244-2113-8
Electronic_ISBN :
978-1-4244-2114-5
Type :
conf
DOI :
10.1109/WCICA.2008.4593701
Filename :
4593701
Link To Document :
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