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On The Gain Synthesis of Dynamic and Integral Sliding Mode Controllers for Quad Rotorcraft Trajectory Tracking Cover

On The Gain Synthesis of Dynamic and Integral Sliding Mode Controllers for Quad Rotorcraft Trajectory Tracking

Open Access
|Mar 2026

Authors

Daniel Benítez

be409784@uaeh.edu.mx

Academic Department of Computing and Electronics, Autonomous University of the State of Hidalgo, Hidalgo, Mexico

Jovani Ortega

jovani_ortega@uaeh.edu.mx

Academic Department of Computing and Electronics, Autonomous University of the State of Hidalgo, Hidalgo, Mexico

Patricio Ordaz

jesus_ordaz@uaeh.edu.mx

Academic Department of Computing and Electronics, Autonomous University of the State of Hidalgo, Hidalgo, Mexico

Eduardo S. Espinoza

eespinoza@secihti.mx

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
DOI: https://doi.org/10.61822/amcs-2026-0003 | Journal eISSN: 2083-8492 | Journal ISSN: 1641-876X
Language: English
Page range: 23 - 35
Submitted on: May 15, 2025
|
Accepted on: Nov 21, 2025
|
Published on: Mar 21, 2026
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 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.