Design of Quadrotor Rescue System
碩士 === 建國科技大學 === 自動化工程系暨機電光系統研究所 === 102 === This study combined a Quadrotor and a rescue system. In the research process, a set of aircraft control module was designed to control the aircraft is flying gesture. The design also combined the relevant size, aerodynamics, flying moving modes and aircr...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2014
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| Online Access: | http://ndltd.ncl.edu.tw/handle/72131640125795346188 |
| Summary: | 碩士 === 建國科技大學 === 自動化工程系暨機電光系統研究所 === 102 === This study combined a Quadrotor and a rescue system. In the research process, a set of aircraft control module was designed to control the aircraft is flying gesture. The design also combined the relevant size, aerodynamics, flying moving modes and aircraft loading weight of 3D graphics software to test the rotor. According to the aircraft dynamic characteristics, the study establishes a mathematic mode of machinery and inertial coordinates. The study seeks to develop a set of stable and balancing control method to achieve the flying gesture stability of the Quadrotor. The rescue system design applied 3D graphics software to design and test the result. A functional magnetic chuck is used to process the fall off and combine movement. The rescue system combines RF wireless signals to receive function and do a remote control processing in order to drive the power control of the electromagnetic chuck board. The design of this system is a stability control of combining a rescue system assembly and function, several times of flying tests and fall off combine function tests are conducted to verify the application of people livelihood and disaster rescue by using this system design.
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