A Study on Control Surface Actuation using Smart Actuator

摘要：

INTRODUCTION In this study,a new type of control surface for a small missile was designed and manufactured using piezo-composite actuator.This study attempted to replace theconventional heavyweight hydraulic or electromagnetic motor actuator by lightweight and simple piezo-composite smart actuator.One side of the actuator was fixed at the aft of the missile fin.A simple prototypewas manufactured and evaluated in an experiment.The result showed that the bimorph type actuator could produce more stable angle of attack without the influence of load.

作者: Ki-Hoon Park Bum-Soo Yoon Kwang Joon Yoon

作者单位: Department of Aerospace Information System Artificial Muscle Research Center,Smart Robot Center in Institute of Intelligent Vehicle ＆ System Tech.Konkuk University Seoul,143-701,Korea

会议类型: 国际会议

会议名称: International Symposium on Nature-Inspired Technology 2008 & International Symposium on Intelligent Unmanned Systems 2008(国际仿生科学会议暨智能无人系统国际研讨会)

会议地点: 南京

会议语种:英文

页码: 70-71

在线出版日期: 2008-10-01（万方平台首次上网日期，不代表论文的发表时间）