關鍵字查詢 | 類別:會議論文 | | 關鍵字:Development of a Distributed Multi-MCU Based Flight Control System for Unmanned Aerial Vehicle

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1 103/1 航太系 蕭照焜 教授 會議論文 發佈 Development of a Distributed Multi-MCU Based Flight Control System for Unmanned Aerial Vehicle , [103-1] :Development of a Distributed Multi-MCU Based Flight Control System for Unmanned Aerial Vehicle會議論文Development of a Distributed Multi-MCU Based Flight Control System for Unmanned Aerial Vehicle蕭照焜; 洪為勝淡江大學航空太空工程學系distributed control system; delay compensation; UAV中華民國航空太空學會; 成功大學This paper investigates the design and implementation of a distributed multi-microcontroller based control system development environment. A DSPIC microcontroller (MCU) based system architecture is established first. The system contains three major parts, namely, sensing and attitude determination section, control section, and ground section. The sensing and attitude determination section consists of four circuit boards (master control board, slave control board, sensor board, and power supply board) with identical size ( ). The sensor boards contains three axes inertial measurement unit (include gyro, accelerometer, and electronic compass) and a GPS receiver. The sensors and the DSPIC MCUs are connected over an
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