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Rogelio Lozano
Researcher at University of Technology of Compiègne
Publications - 509
Citations - 15856
Rogelio Lozano is an academic researcher from University of Technology of Compiègne. The author has contributed to research in topics: Control theory & Adaptive control. The author has an hindex of 58, co-authored 496 publications receiving 14570 citations. Previous affiliations of Rogelio Lozano include University of Illinois at Urbana–Champaign & Instituto Politécnico Nacional.
Papers
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Journal ArticleDOI
Robustness of a discrete-time predictor-based controller for time-varying measurement delay
TL;DR: In this paper, a predictor-based controller for time-varying delay systems is presented and its robustness properties for different uncertainties are analyzed, and the experimental results show good performance and robustness of the proposed scheme even in the presence of long delay uncertainties.
Proceedings ArticleDOI
Almost) exact path tracking control for an autonomous helicopter in hover manoeuvres
Robert Mahony,Rogelio Lozano +1 more
TL;DR: A simplified model of the dynamics of an autonomous model helicopter valid for manoeuvres close to hover is considered and the exact tracking problem is solved using input/output linearization techniques.
Journal ArticleDOI
A Vision and GPS-Based Real-Time Trajectory Planning for a MAV in Unknown and Low-Sunlight Environments
TL;DR: A model predictive control approach is developed, which uses the environment information acquired by the navigation system to develop a safe path planning method using the information provided by the GPS and a consumer depth camera.
Proceedings ArticleDOI
Stabilization and nonlinear control for a novel trirotor mini-aircraft
S. Salazar-Cruz,Rogelio Lozano +1 more
TL;DR: A dynamical model of an original trirotor helicopter obtained using the Euler-Lagrange approach is presented and the obtained nonlinear model is then used for designing a nonlinear controller based on nested saturations.
Proceedings ArticleDOI
Modeling and control of a tilt tri-rotor airplane
TL;DR: The aim of this paper is to present the modelling and control of a tilt tri-rotor UAV's configuration that combines the advantages of both rotary wing and fixed wing vehicle.