DESIGN OF QUADCOPTER HOVER CONTROL USING HYBRID FUZZY AND PROPORTIONAL INTEGRAL DERIVATIVE (PID) CONTROLLER

  • Ahmad Faizal Department of Electrical Engineering, Faculty of Science and Technology, UIN Suska Riau
  • Ewi Ismaredah Department of Electrical Engineering, Faculty of Science and Technology, UIN Suska Riau
  • Imam Fadjar Ridho Department of Electrical Engineering, Faculty of Science and Technology, UIN Suska Riau
DOI: https://doi.org/10.33019/ecotipe.v5i2.647

Abstract

Hover quadcopter system able to free fly hover simpl, because it have a small shape and a light mass then make it easy. However it because quadcopter have a light mass then quadcopter have a weakness that is quadcopter easy to get disturbance from external like wind attack. this simulation of quadcopter using MATLAB R2013a software with controller using hybrid fuzzy-PID. Fuzzy Logic Control is a high intelegance control and able to make interaction with around conditions that might be happened, and it works by given rules input and output based on the conditions. The analysis shown hybrid fuzzy-PID controller have a good responses and faster than a single fuzz logic control. In the fuzzy logic control shown successful to reach setpoint 0.1 rad, but have a longer time responses than hybrid fuzzy-PID controller. Fuzzy Logic Control (FLC) at Roll angle position  shown response 3.2088 s, pitch with 3.256 s and yaw with 3.3045 s. While on hybrid fuzzy-PID controller shown at the angle position of Roll with 0.02896 s, pitch angle position is 2.3138 s and yaw angle position with 0.2611 s. However when quadcopter given disturbance, fuzzy logic control shown better than hybrid fuzzy-PID controller. Fuzzy Logic Control when given a disturbance a time 10 untul 11 second successful to solve the disturbance without an problem. While on hybrid fuzzy-PID when given a disturbance it needs more longer time to reach back the setpoint.

Keywords: Fuzzy, Hover, Hybrid, PID, Pitch, Quadcopter, Roll, Yaw

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Published
2018-10-18
How to Cite
[1]
A. Faizal, E. Ismaredah, and I. Ridho, “DESIGN OF QUADCOPTER HOVER CONTROL USING HYBRID FUZZY AND PROPORTIONAL INTEGRAL DERIVATIVE (PID) CONTROLLER”, JurnalEcotipe, vol. 5, no. 2, pp. 19-28, Oct. 2018.
Issue
Vol 5 No 2 (2018): Jurnal Ecotipe, October 2018
Section
Articles

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