Stabilization of n integrators in cascade with bounded input with experimental application to a VTOL laboratory system
G Sanahuja, P Castillo… - International Journal of …, 2010 - Wiley Online Library
This paper presents a global stabilization of a chain of n integrators in cascade. The control
strategy is obtained using the Lyapunov approach and separated saturation functions …
strategy is obtained using the Lyapunov approach and separated saturation functions …
Robust control scheme for trajectory generation and tracking for quadcopters vehicles: Experimental results
J Betancourt-Vera, P Castillo… - … on Unmanned Aircraft …, 2018 - ieeexplore.ieee.org
A robust control scheme for aerial path generation and tracking is proposed in this paper.
The control structure is based on the MPC-Model Predictive Control-and the UDE …
The control structure is based on the MPC-Model Predictive Control-and the UDE …
Co-design of a safe network control quadrotor
C Berbra, S Lesecq, S Gentil, JM Thiriet - IFAC Proceedings Volumes, 2008 - Elsevier
This paper deals with the co-design of a Network Control System (NCS) and its diagnosis.
Residuals are shown to be affected by network packet losses. A new indicator, sensitive to …
Residuals are shown to be affected by network packet losses. A new indicator, sensitive to …
Quadrotor attitude estimation with data losses
S Lesecq, S Gentil, N Daraoui - 2009 European Control …, 2009 - ieeexplore.ieee.org
This paper deals with the attitude estimation of a quadrotor in the presence of measurement
losses. This situation may appear when the quadrotor is controlled through a network. The …
losses. This situation may appear when the quadrotor is controlled through a network. The …
Tail-sitter UAV having one tilting rotor: Modeling, Control and Real-Time Experiments
In this paper we address the development of a single-rotor tail-sitter Unmanned Aerial
Vehicle (UAV), whose configuration provides structural benefits for flight stabilization. The …
Vehicle (UAV), whose configuration provides structural benefits for flight stabilization. The …
Control of a PVTOL with tilting rotors
A Offermann, P Castillo… - … Conference on Unmanned …, 2019 - ieeexplore.ieee.org
This paper introduces the modeling and control of a Planar Vertical Take Off and Landing
(PVTOL) aircraft with tilting rotors. The mathematical model is obtained step by step using …
(PVTOL) aircraft with tilting rotors. The mathematical model is obtained step by step using …
Linear and nonlinear control strategies to stabilize a VTOL aircraft: Comparative analysis
In this paper a comparative analysis of a linear and nonlinear control laws to stabilize a
VTOL aircraft is presented. A linear control law using LQR method is obtained and …
VTOL aircraft is presented. A linear control law using LQR method is obtained and …
A new experimental ground vehicle with hybrid control and hybrid vision sensor
JM Rendón-Mancha, G Sanahuja, P Castillo… - Journal of applied …, 2010 - scielo.org.mx
This paper presents a new hybrid control algorithm based on saturation functions and its
real–time application to a ground vehicle. The hybrid control is developed from a nonlinear …
real–time application to a ground vehicle. The hybrid control is developed from a nonlinear …
[PDF][PDF] HEUDIASYC UMR CNRS
R Lozano - 2012 - umi.cinvestav.mx
Curriculum Vitae Page 1 Curriculum Vitae Rogelio Lozano HEUDIASYC UMR CNRS University
of Technology of Compiegne Compiegne, France. February 2012 1 Page 2 1 Curriculum Vitae …
of Technology of Compiegne Compiegne, France. February 2012 1 Page 2 1 Curriculum Vitae …
[引用][C] Nested saturation control for stabilizing the PVTOL aircraft
I Fantoni, A Palomino - Unmanned Aerial Vehicles: Embedded …, 2013 - Wiley Online Library
Nested Saturation Control for Stabilizing the PVTOL Aircraft Page 1 Chapter 2 Nested
Saturation Control for Stabilizing the PVTOL Aircraft 2.1. Introduction Within the research …
Saturation Control for Stabilizing the PVTOL Aircraft 2.1. Introduction Within the research …