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International Journal of Latest Research in Science and Technology

DOI:10.29111/ijlrst   ISRA Impact Factor:3.35

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AUTO LEVEL CONTROL SYSTEMS OF V-TAIL QUADCOPTER

Research Paper Open Access

International Journal of Latest Research in Science and Technology Vol.3 Issue 3, pp 1-6,Year 2014

AUTO LEVEL CONTROL SYSTEMS OF V-TAIL QUADCOPTER

Susilo Adi Widyanto, Achmad Widodo, Yuni Awan Wijonarko

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Received : 16 June 2014; Accepted : 23 June 2014 ; Published : 30 June 2014

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Abstract

This work proposes the auto level control system development of V-tail quadcopter. Orientation control is implemented by PID control technique which used feedback data from the nine d.o.f MARG (Magnetic, Angular Rate, and Gravity) sensors. These sensors are used to estimate the orientation angle by using quaternion algorithm represented Kalman based on fusion sensor. The experimental results shows that the optimum control system in x axis is achieved by determining Kp, Ki, KD and KDd are 8.0, 2.2, 0.316 and 10, respectively. Whereas for y axis: Kp, Ki, KD and KDd are 7.04, 1.72, 0.340 and 10, respectively. The steady state error of controll system is less than one degree for x axis as well as y axis.

Key Words   
V-tail Quadcopter, PID control system, MARG, quaternion algorithm

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References
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To cite this article

Susilo Adi Widyanto, Achmad Widodo, Yuni Awan Wijonarko , " Auto Level Control Systems Of V-tail Quadcopter ", International Journal of Latest Research in Science and Technology . Vol. 3, Issue 3, pp 1-6 , 2014

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