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Alternative TitleDesign of Flow Field Control System for a Flapping Wing Aircraft Wind Tunnel
杨孝松1; 盖文1; 江涛2
Source Publication计算机测量与控制
Contribution Rank2
Keyword风洞流场 串级控制 前馈控制 分段PI


Other Abstract

A flow field control system is designed to meet the requirement of aerodynamic performance test for the flapping wing aircraft. Based on the hardware of PLC and converter, a cascade control system composed of a motor speed loop and a wind speed loop is given. And in order to improve the fast response, the motor speed feedforwad method is proposed. Due to the reasonable control regulator and feedforward function, the flow field control has achieved a good result. The test results show that the precision of motor speed is superior to 0.2%,the precision of wind speed is superior to 0.2m/s, the system has smooth adjustment process and good disturbance rejection. The system has been applied successfully to the aerodynamic performance test for the flapping wing aircraft.

Document Type期刊论文
Corresponding Author杨孝松
Recommended Citation
GB/T 7714
杨孝松,盖文,江涛. 某扑翼飞行器风洞流场控制系统设计[J]. 计算机测量与控制,2019,27(11):91-95.
APA 杨孝松,盖文,&江涛.(2019).某扑翼飞行器风洞流场控制系统设计.计算机测量与控制,27(11),91-95.
MLA 杨孝松,et al."某扑翼飞行器风洞流场控制系统设计".计算机测量与控制 27.11(2019):91-95.
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