Direct fuzzy logic controller combined with fast terminal sliding mode for a bicopter

Jennan, Nailae; Mellouli, El Mehdi; Žuraulis, Vidas

doi:10.1109/IRASET60544.2024.10548643

Use this URL to cite this publication: https://hdl.handle.net/20.500.14911/210153

Direct fuzzy logic controller combined with fast terminal sliding mode for a bicopter

Details

Publication Type (CRIS)

Straipsnis konferencijos medžiagoje Scopus duomenų bazėje / Article in conference proceedings in Scopus database (P1a2)

Publication Type (eLABa)

Straipsnis konferencijos darbų leidinyje Scopus DB / Article in conference proceedings Scopus DB (P1b)

VILNIUS TECH Research Priorities and Topics

Autonominis sausumos ir oro transportas / Autonomous land and air transport (TD0101)

Lithuanian Intelligent Specialization

Transportas, logistika ir informacinės ir ryšių technologijos (IRT) / Transport, logistic and information and communication technologies (L106)

Author(s)

Author	Affiliation
Jennan, Nailae	Sidi Mohamed Ben Abdellah University
Mellouli, El Mehdi	Sidi Mohamed Ben Abdellah University
Žuraulis, Vidas	Automobilių inžinerijos katedra / Department of Automobile Engineering (0745)

Title

Direct fuzzy logic controller combined with fast terminal sliding mode for a bicopter

[en]

Nailae Jennan, El Mehdi Mellouli, Vidas Žuraulis

Is part of

IRASET 2024 : The 4th International Conference on Innovative Research in Applied Science, Engineering and Technology, 16-17 May 2024, Fez, Morocco

Published In

Year	Start Page	End Page
2024	1	6

Publisher

IEEE, 2024

Referenced in Database(s)(DBs)

SCOPUS

IEEE Xplore

Extent

p. 1-6

URI

URI	Access Rights
https://hdl.handle.net/20.500.14911/210153
https://ieeexplore.ieee.org/document/10548643	Viso teksto dokumentas (prieiga prenumeratoriams) / Full Text Document (Access for Subscribers)

DOI

10.1109/IRASET60544.2024.10548643

Cited references

Science / Art Area

Technologijos mokslai / Technological sciences (T)

Field of Science / Art

Transporto inžinerija / Transport engineering (T003)

Keywords (en)

Abstract (en)

This work relates to the modelling and control of an unmanned aerial vehicle (UAV), a bicopter, using a direct Takagi-Sugeno (T-S) fuzzy logic controller adapted to fast terminal sliding mode control (FTSMC) method, which aims to reduce the high nonlinearity problem and uncertainties faced in the design of the bicopter system. The primary step is the mathematical model determination, then we apply the fuzzy system to directly control the bicopter system based on FTSMC. The control laws related to the system states are generated by the analysis of the system stability through the Lyapunov approach. Finally, the flight attitude tracking of the bicopter is evaluated by simulating the obtained outcomes and thus verifying the robustness and accuracy of the provided control approach.