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Desain kontrol altitude hold pada Miniature Aerial Vehicle (MAV)

Darmawan, Adytia and Setiaji, One and D., Bima Sena Bayu (2010) Desain kontrol altitude hold pada Miniature Aerial Vehicle (MAV). EEPIS Final Project.

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    The unmanned aerial vehicle (UAV) technology has been attracts the interest of many researchers in the past decades for development. Considering the lack of research on this field and the huge potentials use UAV in Indonesia, we hoped that this research will be a stepping stone for UAV development in Indonesia. On this final project, Miniature Aerial Vehicle(MAV) coaxial is the UAV’s type being used. MAV in the final project controlled from the Ground Segment to set manually to the motion of the elevator, roll, or yaw. Sensor data and control data in the experiment are sent to the ground segment. PID is used to control autonomous MAVs to maintain altitude with the feedback data from the sonar sensors. Experiment shows altitude hold MAV that error average 31,91% . Keywords: Ground Segment, sensors, MAV helicopter, PID control, Experiments.

    Item Type: Article
    Subjects: Q Science > QA Mathematics > QA75 Electronic computers. Computer science
    Q Science > QA Mathematics > QA76 Computer software
    Divisions: Faculty of Engineering, Science and Mathematics > School of Electronics and Computer Science
    Depositing User: Ms Gita Amelia
    Date Deposited: 15 Apr 2011 21:50
    Last Modified: 15 Apr 2011 21:50

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