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Hover Position of Quadrotor Based on PD-like Fuzzy Linear Programming

International Journal of Electrical and Computer Engineering (IJECE) · Vol. 6 No. 5 (2016)

DOI
10.11591/ijece.v6i5.pp2251-2261
ISSN
2088-8708, 2088-8708
Published
2016-10-01
Publisher
Institute of Advanced Engineering and Science
License
creativecommons.org/licenses/by-nc/4.0

Abstract

The purpose of this paper is to present the altitude control algorithm for quadrotor to be able to fly at a particular altitude. Several previous researchers have conducted studies on quadrotor altitude by using PID control but there are problems in the overshoot and oscillation. To optimize the control, tunning on PID algorithm must be first conducted to determine proportional and derivative constants. Hence, the paper presents altitude control modification by using PID-like fuzzy without tuning. The PID algorithm is a control algorithm for linear systems. While, system to be controlled is a non-linear, so that linearization is needed by using equilibrium. The proposed algorithm is a modification of the PID algorithm used as an altitude control which enables quadrotor to be stable when hovering. The algorithm used is not PID algorithm with tuning using fuzzy, but this is a single input single output (SISO) control PID-like fuzzy linear programming. The result of the research shows that quadrotor can hover in a rapid raise time, steady state and settling time without performing overshoot and oscillation.

Collaboration network of the authors

23 authors · 53 co-authorship links · 4 across different organisations

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

  • Universitas Gadjah Mada
  • Muhammadiyah University of Yogyakarta
  • Muhammadiyah University of Surakarta
  • Affiliation unknown
  • Different organisations
  • Same organisation
  • Affiliation unknown
  • Thicker line = more joint articles · bigger circle = more articles
Show as table
Co-authorOrganisationJoint articles
Hari MaghfirohAffiliation unknown4
Kuo Lung LianAffiliation unknown4
Bwo Ren KeAffiliation unknown4
Teguh Bharata AdjiUniversitas Gadjah Mada4
Hendri Himawan TriharmintoUniversitas Gadjah Mada4
Igi ArdiyantoUniversitas Gadjah Mada4
Tatiya Padang TunggalMuhammadiyah University of Yogyakarta2
Andi SupriyantoMuhammadiyah University of Yogyakarta2
Nur Mukhammad Zaidatur RochmanMuhammadiyah University of Yogyakarta2
Ibnu FaishalMuhammadiyah University of Yogyakarta2
Imam PambudiMuhammadiyah University of Yogyakarta2
Adhi SusantoUniversitas Gadjah Mada2
Muhammad KusbanMuhammadiyah University of Surakarta2
Almido Haryanto GintingUniversitas Gadjah Mada2
Anna Nur Nazilah ChamimMuhammadiyah University of Yogyakarta1
Muhammad Heru GustamanMuhammadiyah University of Yogyakarta1
Nia Maharani RaharjaMuhammadiyah University of Yogyakarta1
Lasmadi LasmadiUniversitas Gadjah Mada1
Risanuri HidayatUniversitas Gadjah Mada1
Samiadji HerdjunantoUniversitas Gadjah Mada1

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>Hover Position of Quadrotor Based on PD-like Fuzzy Linear Programming</dc:title><dc:creator>Iswanto, Iswanto</dc:creator><dc:creator>Wahyunggoro, Oyas</dc:creator><dc:creator>Imam Cahyadi, Adha</dc:creator><dc:description>&lt;jats:p&gt;&amp;lt;p&amp;gt;The purpose of this paper is to present the altitude control algorithm for quadrotor to be able to fly at a particular altitude. Several previous researchers have conducted studies on quadrotor altitude by using PID control but there are problems in the overshoot and oscillation. To optimize the control, tunning on PID algorithm must be first conducted to determine proportional and derivative constants. Hence, the paper presents altitude control modification by using PID-like fuzzy without tuning. The PID algorithm is a control algorithm for linear systems. While, system to be controlled is a non-linear, so that linearization is needed by using equilibrium. The proposed algorithm is a modification of the PID algorithm used as an altitude control which enables quadrotor to be stable when hovering. The algorithm used is not PID algorithm with tuning using fuzzy, but this is a single input single output (SISO) control PID-like fuzzy linear programming. The result of the research shows that quadrotor can hover in a rapid raise time, steady state and settling time without performing overshoot and oscillation.&amp;lt;/p&amp;gt;&lt;/jats:p&gt;</dc:description><dc:publisher>Institute of Advanced Engineering and Science</dc:publisher><dc:date>2016-10-01</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.v6i5.pp2251-2261</dc:identifier><dc:identifier>10.11591/ijece.v6i5.pp2251-2261</dc:identifier><dc:source>International Journal of Electrical and Computer Engineering (IJECE); Vol 6 No 5 (2016); 2251</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/1152/4210</dc:relation><dc:rights>http://creativecommons.org/licenses/by-nc/4.0</dc:rights></oai_dc:dc>