R
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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Proceedings ArticleDOI
Attitude stabilization in hover flight of a mini tail-sitter UAV with variable pitch propeller
TL;DR: A dynamic model is developed and a linear control strategy has been developed to stabilize the platform and the configuration proposed is highly unstable in its natural flight state in vertical mode.
Journal ArticleDOI
Stabilization of the Furuta Pendulum Around Its Homoclinic Orbit
Isabelle Fantoni,Rogelio Lozano +1 more
TL;DR: In this paper, an energy-based control approach to control the Furuta pendulum is presented, where a controller is proposed for swinging the pendulum and raising it to its uppermost unstable equilibrium position.
Journal ArticleDOI
Brief Adaptive control for linear slowly time-varying systems using direct least-squares estimation
TL;DR: A least-squares-based non-recursive identification algorithm capable of dealing with slowly time-varying parameters and its estimation algorithm does not require explicit knowledge on the noise bound or the region where the true parameters lie.
Journal ArticleDOI
Technical Communique: PD control of robot manipulators with joint flexibility, actuators dynamics and friction
TL;DR: The convergence analysis of the proposed PD controller is carried out using passivity and global convergence to a desired fixed angular position is proved using only angular position and velocity measurements.
Journal ArticleDOI
Modeling and Global Control of the Longitudinal Dynamics of a Coaxial Convertible Mini-UAV in Hover Mode
TL;DR: An embedded autopilot is developed to validate the proposed prototype and the control law in hover-mode flight, and it is proposed a nonlinear control law that achieves global stability for the longitudinal vertical-mode motion.