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Title: PID self tuning control based on Mamdani fuzzy logic control for quadrotor stabilization

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.
Authors:
;  [1] ;  [2] ;  [3]
  1. Aerospace and Aeronautics Electronics Research Group, Universitas Gadjah Mada, Yogyakarta (Indonesia)
  2. (Indonesia)
  3. Department of Computer Science and Electronics, Universitas Gadjah Mada, Yogyakarta (Indonesia)
Publication Date:
OSTI Identifier:
22494567
Resource Type:
Journal Article
Resource Relation:
Journal Name: AIP Conference Proceedings; Journal Volume: 1705; Journal Issue: 1; Conference: 1. conference on progress in applied mathematics in science and engineering (PIAMSE) 2015, Bali (Indonesia), 29 Sep - 1 Oct 2015; Other Information: (c) 2016 AIP Publishing LLC; Country of input: International Atomic Energy Agency (IAEA)
Country of Publication:
United States
Language:
English
Subject:
43 PARTICLE ACCELERATORS; CONTROL SYSTEMS; FUZZY LOGIC; INTEGRALS; MANUALS; PITCHES; STABILIZATION; TUNING