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김용영,신준희,이선익,이형곤,임현민,김광진,이상철,Kim, Yongyoung,Shin, Junhee,Lee, Sunik,Lee, Hyounggon,Lim, Hyunmin,Kim, Kwangjin,Lee, Sangchul 항공우주시스템공학회 2010 항공우주시스템공학회지 Vol.4 No.4
Quadrotor is an aircraft which is possible in Vertical Take-off and Landing(VTOL). This aircraft can not only be created as an Unmanned Aerial Vehicle(UAV), but also can be easily used in various fields because of its simplicity of construction. This study is mainly conducted with two main purposes. The first goal is designing the quadrotor focusing on the lightweight and protecting the airframe. The second purpose is stabilizing the quadrotor's attitude by using the PID controller. MATLAB simulation is performed for obtaining PID gain based on equations of motion. We used the compensation filter technique for the calibration of sensor data. PID gain has been drawn out based on the MATLAB simulation. The efficiency of the attitude control is improved by calibration of sensor data.