碩士 / 國防大學理工學院 / 電子工程碩士班 / 99 / In this research, we had tried to develop a low-cost and highly integrated unmanned aerial vehicles (Unmanned Aerial Vehicle, UAV) flight computer. Based on the size of small RC aircraft, we had designed and integrated flight control and navigation into small RC aircraft.
We have chosen the Microchip's 16-bit DSP microcontroller for the core controller of flight computer, it's DSP engine provide more efficiency for UAV attitude estimate and flight control function. We also followed concept of systems engineering to develop flight computer, based on system architecture to determine system functional requirements, software requirements, and hardware specification limits.
Referring the UAV autopilot flight computer products of commercial and community, we believe it is trend flight computer design via microcontroller.
| Identifer | oai:union.ndltd.org:TW/099CCIT0428059 |
| Date | January 2011 |
| Creators | Chi,Ting Wei, 紀廷謂 |
| Contributors | Liu, Chiang Lung, Shih, Ta Ming, 劉江龍, 石大明 |
| Source Sets | National Digital Library of Theses and Dissertations in Taiwan |
| Language | zh-TW |
| Detected Language | English |
| Type | 學位論文 ; thesis |
| Format | 78 |
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