Attitude control using an extended calssifier system algorithm for offline auto-tuning of a PID controller

2014 ◽  
Author(s):  
Ehsan Abbasi ◽  
Mohammad Mahjoob ◽  
Ali Shafiekhani
Keyword(s):  
Attitude Control ◽  
Pid Controller ◽  
Auto Tuning

Attitude Control of a Quadrotor with Optimized PID Controller

2013 ◽  
Vol 04 (03) ◽  
pp. 342-349 ◽  
Author(s):  
Hossein Bolandi ◽  
Mohammad Rezaei ◽  
Reza Mohsenipour ◽  
Hossein Nemati ◽  
S. M. Smailzadeh
Keyword(s):  
Attitude Control ◽  
Pid Controller

A design of auto-tuning PID controller using fuzzy logic

2003 ◽  
Author(s):  
Hyeong-Pyo Hong ◽  
Suk-Joon Park ◽  
Sang-Joon Han ◽  
Kyeong-Young Cho ◽  
Young-Chul Lim ◽  
...  
Keyword(s):  
Fuzzy Logic ◽  
Pid Controller ◽  
Auto Tuning

PID-controller with predictor and auto-tuning algorithm: study of efficiency for thermal plants

2017 ◽  
Vol 64 (9) ◽  
pp. 694-702 ◽  
Author(s):  
V. F. Kuzishchin ◽  
E. I. Merzlikina ◽  
Van Va Hoang
Keyword(s):  
Pid Controller ◽  
Auto Tuning

scholarly journals Development of Vehicle Path Control Model Using Auto-tuning PID Controller with Deep Learning Technique

2021 ◽  
Vol 29 (1) ◽  
pp. 1-9
Author(s):  
Shengpeng Zhang ◽  
Hyoyeong Heo ◽  
Jeongyeol Baek ◽  
Sangwoo Ahn ◽  
Taeoh Tak
Keyword(s):  
Deep Learning ◽  
Pid Controller ◽  
Control Model ◽  
Path Control ◽  
Learning Technique ◽  
Auto Tuning ◽  
Vehicle Path

scholarly journals Development of attitude control system for hybrid airship vehicle

2018 ◽  
Vol 7 (4.13) ◽  
pp. 99
Author(s):  
Azizi Malek ◽  
M F Sedan ◽  
A S M Harithuddin
Keyword(s):  
Control System ◽  
Attitude Control ◽  
Pid Controller ◽  
Control Mechanism ◽  
Attitude Control System ◽  
Flight Tests ◽  
Aerial Vehicle ◽  
The Mathematical Model ◽  
Monitoring Software ◽  
Acquisition Method

This paper documents and presents the development of attitude control system of Hybrid Airship Unmanned Aerial Vehicle (HAU) that should be able to change its attitude condition based on the response processed from the provided input. This is accomplished by data acquisition method that retrieves data from a flight controller and processes it into the control system without looking in deep on the mathematical model of the airship. Besides that, PID controller is used in order to create a good stable response for the hybrid airship. A working hybrid airship prototype was successfully developed and built, which is five meters in length and has four propellers that is symmetrically distanced to each other. A quadcopter attitude control mechanism is adopted into the hybrid airship to allow for good hovering capability and direct pure attitude control. Outdoor flight tests have been conducted to prove its stability in responding to attitude input given to the hybrid airship attitude controller. A data monitoring software is also written to make the data observation on the behaviour of the hybrid airship response to be easier and understandable. Result demonstrates that the hybrid airship does response to pitch, roll and yaw input from the operator, albeit the lack response stability and speed which can be improved in conservative continuation of research on the airship attitude control system.  

Auto-tuning of PID controller according to fractional-order reference model approximation for DC rotor control

Mechatronics ◽  
2013 ◽  
Vol 23 (7) ◽  
pp. 789-797 ◽  
Author(s):  
Baris Baykant Alagoz ◽  
Abdullah Ates ◽  
Celaleddin Yeroglu
Keyword(s):  
Fractional Order ◽  
Pid Controller ◽  
Reference Model ◽  
Model Approximation ◽  
Auto Tuning ◽  
Rotor Control

scholarly journals An adaptive PID controller with an online auto-tuning by a pretrained neural network

2019 ◽  
Vol 1359 ◽  
pp. 012090
Author(s):  
P A Chertovskikh ◽  
A V Seredkin ◽  
O A Gobyzov ◽  
A S Styuf ◽  
M G Pashkevich ◽  
...  
Keyword(s):  
Neural Network ◽  
Pid Controller ◽  
Auto Tuning
Sign in / Sign up

Export Citation Format

Share Document