Jairo Olguin Roque

Dr. Jairo Olguin Roque

Sistemas Autonomos de Navegacion Aerea y Submarina, Centro de Investigación y de Estudios Avanzados del IPN, Mexico City, Ciudad de México, Mexico
orcid

Research Focus & Metrics

Academic Career Length

4Years (2023-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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28 April 2023 in Algorithms
Verified
Journal Article
Open access
PDF file
Jairo Olguin RoqueJairo Olguin Roque
Jairo Olguin Roque
SSSalaza Sergio
Salaza Sergio
IGIván González-Hernández
Iván González-Hernández
Rogelio LozanoRogelio Lozano
Rogelio Lozano
This paper proposes a robust algorithm based on a fixed-time sliding mode controller (FTSMC) for a Quadrotor aircraft. This approach is based on Lyapunov theory, which guarantees system stability. Nonlinear error dynamics techniques are used to achieve accurate trajectory tracking in the presence of disturbances. The performance of the FTSMC is compared with the typical non-singular terminal sliding mode controller (NTSMC) to evaluate its effectiveness. The numerical results show that FTSMC is more efficient than the typical NTSMC in disturbance reduction.

4 May 2026 in IEEE Access
Verified
Journal Article
Open access
JHJhonatan Fernando Eulopa Hernandez
Jhonatan Fernando Eulopa Hernandez
Jairo Olguin RoqueJairo Olguin Roque
Jairo Olguin Roque
DPDiego-Alfredo Padilla-Pérez
Diego-Alfredo Padilla-Pérez
PAPablo-Alejandro Arizpe-Carreón
Pablo-Alejandro Arizpe-Carreón
CCCarlos Couder-Castañeda
Carlos Couder-Castañeda
This paper presents the design and numerical validation of a robust fixed-time sliding mode controller (FTSMC) for a thrust-vectored planar vertical takeoff and landing (PVTOL) system with strongly coupled nonlinear dynamics. Unlike conventional PVTOL models assuming aligned thrust, the proposed system explicitly incorporates thrust vectoring, resulting in significant inter-axis coupling. A fixed-time sliding-mode control law with smooth nonlinear terms is developed to ensure practical fixed-time convergence to a predefined boundary layer, independently of initial conditions, while mitigating chattering. Numerical simulations under bounded disturbances demonstrate that the proposed FTSMC outperforms a non-terminal sliding mode controller (NTSMC), achieving a reduction of approximately 38% in settling time, more than 80% reduction in pitch overshoot, and up to 60% decrease in control effort. These results highlight the robustness and efficiency of the proposed control strategy for safety-critical UAV and rocket-based platforms that require rapid, precise maneuvering.

31 October 2025
Verified
Book Chapter
Closed access
PDF file
Jairo Olguin RoqueJairo Olguin Roque
Jairo Olguin Roque
JEJhonatan-Fernando Eulopa-Hernandez
Jhonatan-Fernando Eulopa-Hernandez
CCCarlos Couder-Castañeda
Carlos Couder-Castañeda
PAPablo Alejandro Arizpe
Pablo Alejandro Arizpe
DPDiego Padilla-Pérez
Diego Padilla-Pérez

1 September 2026
Verified
Conference Paper
Closed access
Jairo Olguin RoqueJairo Olguin Roque
Jairo Olguin Roque
JHJhonatan Fernando Eulopa Hernandez
Jhonatan Fernando Eulopa Hernandez
LCLevi Emmanuel Cruz-Vázquez
Levi Emmanuel Cruz-Vázquez
ARAlondra Ruiz-Vidal
Alondra Ruiz-Vidal

15 April 2026 in Symmetry
Verified
Journal Article
Open access
PDF file
JHJesús Antonio Herrera-Pérez
Jesús Antonio Herrera-Pérez
CACarlos Ortiz Aleman
Carlos Ortiz Aleman
SLSebastian López-Juárez
Sebastian López-Juárez
JHJhonatan Fernando Eulopa Hernandez
Jhonatan Fernando Eulopa Hernandez
CCCarlos Couder-Castañeda
Carlos Couder-Castañeda
DPDiego Padilla-Pérez
Diego Padilla-Pérez
Reverse time migration (RTM) exploits time-reversal symmetry and adjoint duality to focus wavefields and reconstruct subsurface reflectivity, but large surveys remain limited by the cost of forward and backward propagation. We present a Graphics Processing Unit (GPU)-accelerated adjoint RTM workflow for depth imaging of the Chicxulub impact structure using the marine A0/A1 composite profile (1996). The processed stacked section contains 14,172 traces with 6.25 m Common Depth Point (CDP) spacing, 1 ms sampling, and 18 s record length. Forward and adjoint wavefields are computed with a staggered-grid finite-difference scheme (fourth order in space, second in time) and Convolutional Perfectly Matched Layers (CPMLs), which provide stable finite-domain simulations while introducing controlled symmetry breaking through absorption. The solver is verified with the Lamb half-space analytical benchmark and applied through five interpretation-guided velocity/density updates. The final depth image improves reflector continuity and interpretability of crater-scale elements, including post-impact sedimentary fill, melt and breccia units, terrace fault blocks, and deep uplift-related structure. Compute Unified Device Architecture (CUDA) acceleration reduces runtime from ∼32.36 h on a CPU baseline to ∼34.10 min on an RTX 3070 (≈56.9×), enabling practical, reproducible iterative RTM on accessible hardware.