POSITION CONTROL OF VTOL SYSTEM USING ANFIS VIA HARDWARE IN THE LOOP

SINERGI

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Field Value
 
Title POSITION CONTROL OF VTOL SYSTEM USING ANFIS VIA HARDWARE IN THE LOOP
 
Creator Maghfiroh, Hari
Hermanu, Chico
Sitorini Zul Hizmi, Vernanda
 
Subject
ANFIS; HIL; Position control; VTOL;
 
Description Electric motors have been widely applied in various equipment. One application is found in Unmanned Aerial Vehicles (UAVs). An electric motor speed control system that can balance the aircraft's position is one of the mandatory features that must be owned by the aircraft. The position balancer control also supports the Vertical Take-Off Landing (VTOL) system. This study's VTOL position control system uses Hardware-in-the-loop (HIL) method with MATLAB Simulink and Arduino. ANFIS (Adaptive Neuro-Fuzzy Inferences System) is used as a position control algorithm. The controller performance is compared with conventional PID and FLC (Fuzzy Logic Controller). The system is tested as an initial position variation and loading test. The experiment shows that HIL can help fast prototyping by faster changes in the controller algorithms and is easy to program. The result is varied in each experiment. In the ISE (Integral Square of Error) point of view, ANFIS is better than PID by 100 % and has a very small difference from FLC in the initial position test. ANFIS is better by 95.44% and 4.56% compared with PID and FLC in the loading test, respectively.
 
Publisher Universitas Mercu Buana
 
Contributor
 
Date 2021-07-30
 
Type info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
Peer-reviewed Article
 
Format application/pdf
 
Identifier https://publikasi.mercubuana.ac.id/index.php/sinergi/article/view/10018
10.22441/sinergi.2021.3.008
 
Source SINERGI; Vol 25, No 3 (2021); 309-318
24601217
14102331
 
Language eng
 
Relation https://publikasi.mercubuana.ac.id/index.php/sinergi/article/view/10018/4826
https://publikasi.mercubuana.ac.id/index.php/sinergi/article/downloadSuppFile/10018/1702
 
Rights Copyright (c) 2021 SINERGI
 

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