Proceedings of the International Conference on Science and Technology (ICST 2018)

AUTONOMOUS QUADCOPTER STABILITY WITH PID CONTROL

Authors
Sri Wahyuni, M. Izar Bahroni, Faikul Umam
Corresponding Author
Sri Wahyuni
Available Online December 2018.
DOI
https://doi.org/10.2991/icst-18.2018.110How to use a DOI?
Keywords
UAV; Quadcopter; PID; Autonomous
Abstract

Unmanned Aerial Vehicle (UAV) has many uses, including aerial photography, aerial mapping and monitoring activities. Quadcopter is a type of UAV that uses four rotors. The speed of each rotor has a considerable influence on the movement. The quadcopter movement can be done in this research, namely the process of arming, taking off, hover, and landing on decisions made by the system (autonomous). How the quadcopter achieves a balance in its movement to be stable and responsive requires a method. One method that is suitable for processing stability is the method (PID). The PID method has three main parameters, namely Proportional (Kp), Integral (Ki), Derivatives (Kd), with the determination of the constant through the trial and error process to obtain the optimal stability value as the purpose of this study. But the load of the quadcopter and the wind tightness around it is very influential to get the quadcopter movement to survive in stable conditions. Through a series of experimental processes carried out to produce the best constant values, at Kp = 1.3, Ki = 0.04, and Kd = 18, where the quadcopter is able to survive for 20 sec at the same relative point from the time of departure. The addition of GPS sensors in advanced research will be able to make this quadcopter move stable with the monitored position.

Copyright
© 2018, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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Volume Title
Proceedings of the International Conference on Science and Technology (ICST 2018)
Series
Atlantis Highlights in Engineering
Publication Date
December 2018
ISBN
978-94-6252-650-1
ISSN
2589-4943
DOI
https://doi.org/10.2991/icst-18.2018.110How to use a DOI?
Copyright
© 2018, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

Cite this article

TY  - CONF
AU  - Sri Wahyuni
AU  - M. Izar Bahroni
AU  - Faikul Umam
PY  - 2018/12
DA  - 2018/12
TI  - AUTONOMOUS QUADCOPTER STABILITY WITH PID CONTROL
BT  - Proceedings of the International Conference on Science and Technology (ICST 2018)
PB  - Atlantis Press
SP  - 527
EP  - 531
SN  - 2589-4943
UR  - https://doi.org/10.2991/icst-18.2018.110
DO  - https://doi.org/10.2991/icst-18.2018.110
ID  - Wahyuni2018/12
ER  -