On The Gain Synthesis of Dynamic and Integral Sliding Mode Controllers for Quad Rotorcraft Trajectory Tracking
Authors
Daniel Benítez
Academic Department of Computing and Electronics, Autonomous University of the State of Hidalgo, Hidalgo, Mexico
Jovani Ortega
Academic Department of Computing and Electronics, Autonomous University of the State of Hidalgo, Hidalgo, Mexico
Patricio Ordaz
Academic Department of Computing and Electronics, Autonomous University of the State of Hidalgo, Hidalgo, Mexico
Eduardo S. Espinoza
Directorate of Support for the Consolidation of the Scientific and Humanistic Community Secretariat of Science, Humanities, Technology, and Innovation, Mexico City, Mexico
Department of Research and Multidisciplinary Studies Center For Research and Advanced Studies of the National Polytechnic Institute, Mexico City, Mexico
Language: English
Page range: 23 - 35
Submitted on: May 15, 2025
Accepted on: Nov 21, 2025
Published on: Mar 21, 2026
Published by: University of Zielona Góra
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year
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© 2026 Daniel Benítez, Jovani Ortega, Patricio Ordaz, Eduardo S. Espinoza, published by University of Zielona Góra
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.