Design of Scale Model Mechanism in Low Speed Wind Tunnel

被引:1
|
作者
AHMAD Aldarouich [1 ]
机构
[1] School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics
关键词
position control servo system; proportional-integral-differential control; wind tunnel test; MATLAB;
D O I
10.19583/j.1003-4951.2008.02.009
中图分类号
V211.74 [风洞];
学科分类号
0801 ; 080103 ; 080104 ;
摘要
Motion control can be considered as the synergistic collaboration of mechanical and electrical engineering, computer science and information technology to apply a controlled force to achieve useful motion in fluid or soiled electromechanical systems. With the development of computer, electronics, and automatic control theory, motion control comes to a new stage. Great applications are based on the characteristics, stemming from advantages of electronics and modern control technology achievements, having a very good load matching property. Currently, microprocessor-based controllers are invariably used in most applications of drive electronics. The object of this work is to design a position control mechanism system, which can be used in test section of low speed wind tunnel. System load specifications and performance requirements are given. A comprehensive study of mathematical modeling of the mechanism components is given. Procedure for selection of various components with optimum parameters is discussed. After selection and calculation of system parameters to meet the performance requirements, a PID control method is adopted.
引用
收藏
页码:57 / 64
页数:8
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