AUTONOMOUS QUADCOPTER STABILITY WITH PID CONTROL
Sri Wahyuni, M. Izar Bahroni, Faikul Umam
Available Online December 2018.
- https://doi.org/10.2991/icst-18.2018.110How to use a DOI?
- UAV; Quadcopter; PID; Autonomous
- 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.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
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 - 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 -