| Summary: | 碩士 === 明志科技大學 === 機電工程研究所 === 102 === The thesis purpose for analysis and implementation of Quadrocopter Aerial Vehicle, The confirmed from analysis and the implementation result, The structural strength of Quadrocopter Aerial Vehicle by Self-made, Can withstand the Quadrocopter Aerial Vehicle to carry on the flights of various attitude variations, For example fast taking off、landing、head-wind flight and the external disturbance.
This article first by Pro/Engineer 3D Graphic Application,, The design model and establishes the aviation board, the Emission Control System, battery and motor related size of Quadrocopter Aerial Vehicle, To Design for mechanical structure of Quadrocopter Aerial Vehicle, Using the finite element method Application ANSYS develops the analysis and simulation, Analysis result confirmation structural strength security of Quadrocopter Aerial Vehicle, Then using the Computer-aided manufacturing (CAM) technology and computer numerical control (CNC) engraving machine manufacturing institutions designed and assembled parts to complete of Quadrocopter Aerial Vehicle mechanical system.
This article has realized of Quadrocopter Aerial Vehicle organization system analysis, from analysis result definite intensity of Quadrocopter Aerial Vehicle, and implementation of Quadrocopter Aerial Vehicle, after many times outdoors flight, The Quadrocopter Aerial Vehicle Definite can withstand any flight attitude change.
|
|---|
