Design and Implementation of Linear Actuator in Dual Pilot Ultra-Light Aircraft

碩士 === 國立成功大學 === 航空太空工程學系 === 103 === In the sky-net project, previous study proposes the dual-pilot system because of the demand for switching control mode. Previous electronic control system applies the clutch to switch the control mode. However, the clutch has the problem that it cannot connect...

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Bibliographic Details
Main Authors: Wei-HsunLai, 賴韋勳
Other Authors: Chin E. Lin
Format: Others
Language:en_US
Published: 2015
Online Access:http://ndltd.ncl.edu.tw/handle/51514274087936217661