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

  • 賴 韋勳

Student thesis: Master's Thesis

Abstract

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 smoothly or even cannot connect In order to increase the reliability of mechanism this thesis proposes to apply non-contacting type clutch to replace the original contacting type clutch in the new design of the linear actuator control system In addition the thesis proposes some smoothness improvement of mechanism Based on computer aid design to realize the proposed idea the linear actuator control system is manufactured This thesis verifies the clutch test and the response test on the proposed linear actuator control system for its performance improvement The comparison of the test results show that the proposed linear actuator control system has better reliability and controllability
Date of Award2015 Aug 12
Original languageEnglish
SupervisorChin-E. Lin (Supervisor)

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