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Carlos Aguilar-Ibanez

Researcher at Instituto Politécnico Nacional

Publications -  87
Citations -  1074

Carlos Aguilar-Ibanez is an academic researcher from Instituto Politécnico Nacional. The author has contributed to research in topics: Lyapunov function & Control theory. The author has an hindex of 15, co-authored 82 publications receiving 834 citations. Previous affiliations of Carlos Aguilar-Ibanez include AmeriCorps VISTA.

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A chaotic system in synchronization and secure communications

TL;DR: This paper proposes a receiver system which tends to follow asymptotically the unknown Rikitake system, refereed as transmitter system, and adjusts the gains of the receiver system continually according to a convenient high order sliding-mode adaptative controller (HOSMAC), until the measurable output errors converge to zero.
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Stability of active disturbance rejection control for uncertain systems: A Lyapunov perspective

TL;DR: In this paper, a simple stability analysis to justify the active disturbance rejection control method, used in the feedback regulation of a substantially uncertain plant, is presented, and a criterion is obtained that allows to define under what conditions closed-loop stability can be assured.
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The trajectory tracking problem for an unmanned four-rotor system: flatness-based approach

TL;DR: A flatness-based controller that solves the trajectory tracking problem for an unmanned four-rotor aircraft using a simple version of the dynamical system obtained from a suitable coordinate transformation of the Euler–Lagrange model of the system.
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A trajectory planning based controller to regulate an uncertain 3D overhead crane system

TL;DR: A control strategy to solve the regulation control problem, from the perspective of trajectory planning, for an uncertain 3D overhead crane is introduced based on an adaptive control approach that takes advantage of the passivity properties found in this kind of systems.
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Stabilization of the PVTOL aircraft based on a sliding mode and a saturation function

TL;DR: In this article, a feedback control strategy for the regulation of a planar vertical takeoff and landing aircraft is presented, where two controllers are designed to stabilize the vertical variable and stabilize both the horizontal and angular variables to the desired rest position.