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Fuzzy gain scheduling control apply to an RC Hovercraft

International Journal of Electrical and Computer Engineering (IJECE) · Vol. 10 No. 3 (2020)

DOI
10.11591/ijece.v10i3.pp2434-2440
ISSN
2088-8708, 2088-8708
Published
2020-06-01
Publisher
Institute of Advanced Engineering and Science
License
creativecommons.org/licenses/by-nc/4.0

Abstract

The Fuzzy Gain Scheduling (FGS) methodology for tuning the Proportional – Integral – Derivative (PID) traditional controller parameters by scheduling controlled gains in different phases, is a simple and effective application both in industries and real-time complex models while assuring the high achievements over pass decades, is proposed in this article. The Fuzzy logic rules of the triangular membership functions are exploited on-line to verify the Gain Scheduling of the Proportional – Integral – Derivative controller gains in different stages because it can minimize the tracking control error and utilize the Integral of Time Absolute Error (ITAE) minima criterion of the controller design process. For that reason, the controller design could tune the system model in the whole operation time to display the efficiency in tracking error. It is then implemented in a novel Remote Controlled (RC) Hovercraft motion models to demonstrate better control performance in comparison with the PID conventional controller.

Collaboration network of the authors

15 authors · 42 co-authorship links · 31 across different organisations

Hover or tap a name to highlight its co-authors. Double-click to open the author's page.

  • Ton Duc Thang University
  • Ho Chi Minh City University of Industry and Trade
  • National Taiwan University of Science and Technology
  • Trường ĐH Nguyễn Tất Thành
  • Phòng Thí nghiệm Trọng điểm Quốc gia Điều khiển số và Kỹ thuật hệ thống
  • Saigon University
  • Industrial University of Ho Chi Minh City
  • Other organisations
  • Affiliation unknown
  • Different organisations
  • Same organisation
  • Affiliation unknown
  • Thicker line = more joint articles · bigger circle = more articles
Show as table
Co-authorOrganisationJoint articles
Phu Tran TinIndustrial University of Ho Chi Minh City5
Minh TranAffiliation unknown3
Van-Duc PhanVan Lang University2
Tran Hoang Quang MinhTon Duc Thang University1
Nguyễn Quang DũngTon Duc Thang University1
Thanh Trang TranHo Chi Minh City University of Industry and Trade1
Tan Nhat NguyenTon Duc Thang University1
Duy-Hung HaTon Duc Thang University1
Thanh-Long NguyenHo Chi Minh City University of Industry and Trade1
Anh Vu LeTon Duc Thang University1

Affiliations come from OpenAlex; journal OAI-PMH metadata carries none. Authors without an OpenAlex ID are matched by name, which can merge or split people.

This record comes from Crossref (what the publisher deposited), because the journal's own OAI-PMH endpoint could not be harvested.

Metadata source: Crossref API (cadangan, berdasarkan ISSN) https://api.crossref.org/journals/2088-8708/works, first harvested 27 Okt 2026, last seen 27 Okt 2026.
Metadata as oai_dc, converted from Crossref
<oai_dc:dc xmlns:dc="http://purl.org/dc/elements/1.1/" xmlns:oai_dc="http://www.openarchives.org/OAI/2.0/oai_dc/"><dc:title>Fuzzy gain scheduling control apply to an RC Hovercraft</dc:title><dc:creator>Tran, Huu Khoa</dc:creator><dc:creator>Lam, Pham Duc</dc:creator><dc:creator>Trang, Tran Thanh</dc:creator><dc:creator>Nguyen, Xuan Tien</dc:creator><dc:creator>Nguyen, Hoang-Nam</dc:creator><dc:description>&lt;jats:p&gt;The Fuzzy Gain Scheduling (FGS) methodology for tuning the Proportional – Integral – Derivative (PID) traditional controller parameters by scheduling controlled gains in different phases, is a simple and effective application both in industries and real-time complex models  while assuring the high achievements over pass decades, is proposed in this article. The Fuzzy logic rules of the triangular membership functions are exploited on-line to verify the Gain Scheduling of the Proportional – Integral – Derivative controller gains in different stages because it can minimize the tracking control error and utilize the Integral of Time Absolute Error (ITAE) minima criterion of the controller design process.  For that reason, the controller design could tune the system model in the whole operation time to display the efficiency in tracking error. It is then implemented in a novel Remote Controlled (RC) Hovercraft motion models to demonstrate better control performance in comparison with the PID conventional controller.&lt;/jats:p&gt;</dc:description><dc:publisher>Institute of Advanced Engineering and Science</dc:publisher><dc:date>2020-06-01</dc:date><dc:type>info:eu-repo/semantics/article</dc:type><dc:format>application/pdf</dc:format><dc:identifier>https://doi.org/10.11591/ijece.v10i3.pp2434-2440</dc:identifier><dc:identifier>10.11591/ijece.v10i3.pp2434-2440</dc:identifier><dc:source>International Journal of Electrical and Computer Engineering (IJECE); Vol 10 No 3 (2020); 2434</dc:source><dc:source>2088-8708</dc:source><dc:source>2088-8708</dc:source><dc:relation>http://ijece.iaescore.com/index.php/IJECE/article/viewFile/20443/pdf</dc:relation><dc:rights>http://creativecommons.org/licenses/by-nc/4.0</dc:rights></oai_dc:dc>