Quadcopter Main Board Design with PID Algorithm as Controller

  • Mochamad Bachtiar Department of Informatics and Computer Engineering, Politeknik Elektronika Negeri Surabaya
  • Iwan Kurnianto Wibowo Department of Informatics and Computer Engineering, Politeknik Elektronika Negeri Surabaya
  • Nur Cahyo Ihsan Prastyawan Department of Informatics and Computer Engineering, Politeknik Elektronika Negeri Surabaya
  • Maretha Ruswiansari Department of Informatics and Computer Engineering, Politeknik Elektronika Negeri Surabaya
  • Hendy Briantoro Department of Informatics and Computer Engineering, Politeknik Elektronika Negeri Surabaya
  • Nofria Hanafi Department of Informatics and Computer Engineering, Politeknik Elektronika Negeri Surabaya
  • Niam Tamami Department of Informatics and Computer Engineering, Politeknik Elektronika Negeri Surabaya
  • Hendhi Hermawan Department of Informatics and Computer Engineering, Politeknik Elektronika Negeri Surabaya
  • Eko Budi Utomo Department of Informatics and Computer Engineering, Politeknik Elektronika Negeri Surabaya
https://doi.org/10.25139/inform.v7i2.4687
Abstract views: 403 , PDF downloads: 388
Keywords: Main Board, Quadcopter, PID Algorithm, UAV, IMU

Abstract

Kontes Robot Terbang Indonesia (KRTI) Flight controller division has a mission to independently make an unmanned aerial vehicle (UAV) controller. UAV controllers are usually made by non-local manufacturers, who have a package between the controller and the aircraft. Due to limited pins and specific functions, most controllers cannot adapt to user requirements. For this reason, in this study, we made a UAV controller with a more significant number of pins that can be programmed independently. Main Controller is a master board device used to control the stability of the UAV when flying. The main controller has been designed specifically for certain products so that the UAV cannot be modified. In this study, it is proposed to make the main controller that is specifically designed to fly a Quadcopter UAV. Movement control for quadcopter stability when flying using the Proportional Integral Derivative (PID) method. The main controller has a function that is to regulate the entire course of flight on unmanned vehicles. PID control can adapt to changes so that the system becomes stable. The PID control on the Main Controller is intended to balance the quadcopter concerning its orientation angle. The Main Controller is also tasked with recording data from sensors such as the Inertial Measurement Unit (IMU) and reading data from the remote. The controller successfully flew the quadcopter with a P value of 0.245, an I value of 0.0139, and a D value of 0.0085.

References

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Published
2022-07-31
How to Cite
Bachtiar, M., Iwan Kurnianto Wibowo, Nur Cahyo Ihsan Prastyawan, Maretha Ruswiansari, Hendy Briantoro, Nofria Hanafi, Niam Tamami, Hendhi Hermawan, & Eko Budi Utomo. (2022). Quadcopter Main Board Design with PID Algorithm as Controller . Inform : Jurnal Ilmiah Bidang Teknologi Informasi Dan Komunikasi, 7(2), 148-155. https://doi.org/10.25139/inform.v7i2.4687
Issue
Vol. 7 No. 2 (2022)
Section
Articles

Copyright (c) 2022 Mochamad Bachtiar

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