Quadrotor as one type of UAV have the ability to perform Vertical Take Off and Landing (VTOL). It allows the Quadrotor to be stationary hovering in the air. PID (Proportional Integral Derivative) control system is one of the control methods that are commonly used. It is usually used to optimize the Quadrotor stabilization at least based on the three Eulerian angles (roll, pitch, and yaw) as input parameters for the control system. The three constants of PID can be obtained in various methods. The simplest method is tuning manually. This method has several weaknesses. For example if the three constants are not exact, the resulting response will deviate from the desired result. By combining the methods of PID with fuzzy logic systems where human expertise is implemented into the machine language is expected to further optimize the control system.
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1 February 2016
PROGRESS IN APPLIED MATHEMATICS IN SCIENCE AND ENGINEERING PROCEEDINGS
29 September–1 October 2015
Bali, Indonesia
Research Article|
February 01 2016
PID self tuning control based on Mamdani fuzzy logic control for quadrotor stabilization
Tri Kuntoro Priyambodo;
Tri Kuntoro Priyambodo
a)
1Aerospace and Aeronautics Electronics Research Group,
Universitas Gadjah Mada
, Yogyakarta, Indonesia
2Department of Computer Science and Electronics,
Universitas Gadjah Mada
, Yogyakarta, Indonesia
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Andi Dharmawan;
Andi Dharmawan
b)
2Department of Computer Science and Electronics,
Universitas Gadjah Mada
, Yogyakarta, Indonesia
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Agfianto Eko Putra
Agfianto Eko Putra
1Aerospace and Aeronautics Electronics Research Group,
Universitas Gadjah Mada
, Yogyakarta, Indonesia
2Department of Computer Science and Electronics,
Universitas Gadjah Mada
, Yogyakarta, Indonesia
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a)
Corresponding author: [email protected], IEEE Member
AIP Conf. Proc. 1705, 020013 (2016)
Citation
Tri Kuntoro Priyambodo, Andi Dharmawan, Agfianto Eko Putra; PID self tuning control based on Mamdani fuzzy logic control for quadrotor stabilization. AIP Conf. Proc. 1 February 2016; 1705 (1): 020013. https://doi.org/10.1063/1.4940261
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