Nicolas Langlois

Prof. Nicolas Langlois

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Research Focus & Metrics

Academic Career Length

27Years (2000-Present)

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

Representative Publications

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18 February 2016 in IEEE Transactions on Industrial Electronics
Verified
Journal Article
Closed access
SASofiane Ahmed Ali
Sofiane Ahmed Ali
ACArnaud Christen
Arnaud Christen
Steven BeggSteven Begg
Steven Begg
Nicolas LangloisNicolas Langlois
Nicolas Langlois
In this paper, a continuous-discrete time observer which simultaneously estimates the unmeasurable states and the uncertainties for the electro-hydraulic actuator (EHA) system is presented. The main feature of the proposed observer is the use of an intersample output predictor which allows the users to increase the frequency acquisition of the piston position sensor without affecting the convergence performance. The stability analysis of the proposed observer is proved using Lyapunov function adapted to hybrid systems. To show the efficiency of our proposed observer, numerical simulations and experimental validation involving a control application, which combines the designed observer and a proportional-integral (PI) controller for the purpose of piston position tracking problem, are presented.

1 January 2015 in IFAC-PapersOnLine
Verified
Journal Article
Closed access
MGMohamed Guermouche
Mohamed Guermouche
SASofiane Ahmed Ali
Sofiane Ahmed Ali
Nicolas LangloisNicolas Langlois
Nicolas Langlois

1 July 2007 in American Control Conference (ACC)
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Conference Paper
Closed access
APAlexandros Plianos
Alexandros Plianos
AAAli Achir
Ali Achir
RSRichard Stobart
Richard Stobart
Nicolas LangloisNicolas Langlois
Nicolas Langlois
HCHOUCINE CHAFOUK
HOUCINE CHAFOUK
In this paper, a nonlinear control technique based on the property of flatness is proposed to control the diesel engine air system. More precisely, to achieve tracking of suitable references (corresponding to low emissions) for the air-fuel ratio and the fraction of the recirculated exhaust gas. The simulated diesel engine is a six cylinders medium duty Caterpillar 3126 B equipped with a variable geometry turbocharger and an exhaust gas recirculation valve. The proposed controller is designed on the reduced third order mean value model and implemented by endogenous linearizing dynamic feedback on the full order model. The controller is assessed through simulations with a SIL architecture using dSpace simulator. It exhibits good control performance without zero dynamics and ensures global stability and tracking of flat output references.

22 July 2020 in IEEE Transactions on Aerospace and Electronic Systems
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Journal Article
Closed access
SPSergio Perez-Roca
Sergio Perez-Roca
JMJulien Marzat
Julien Marzat
HPHelene Piet-Lahanier
Helene Piet-Lahanier
Nicolas LangloisNicolas Langlois
Nicolas Langlois
MGMarco Galeotta
Marco Galeotta
SGSerge Le Gonidec
Serge Le Gonidec
Reusable liquid-propellant rocket engines (LPREs) imply more demanding robustness requirements than expendable ones due to their extended capabilities. Therefore, the goal of this work was to develop a control loop adapted to all the operating phases of LPRE, including transients, and robust to internal parametric variations. Firstly, thermo-fluid-dynamic simulators representative of the gas-generator-cycle engines were built. These simulators were subsequently translated into nonlinear state-space models. Based on these models, the continuous subphase of the start-up transient is controlled to track precomputed reference trajectories. Beyond the start-up, throttling scenarios are managed with end-state-tracking algorithm. Model Predictive Control has been applied in a linearised manner with robustness considerations to both scenarios, in which a set of hard state and control constraints must be respected. Tracking of pressure (thrust) and mixture-ratio operating points within the design envelope is achieved in simulation while respecting constraints. Robustness to variations in the predominant parameters, to external state perturbations and to the possible impact of an observer on the loop, is demonstrated.

1 August 2015 in Applied Mathematical Modelling
Verified
Journal Article
Closed access
SASofiane Ahmed Ali
Sofiane Ahmed Ali
MGMohammed Guermouche
Mohammed Guermouche
Nicolas LangloisNicolas Langlois
Nicolas Langlois

1 January 2009
Verified
Conference Paper
Closed access
MDMarcelin Dabo
Marcelin Dabo
Nicolas LangloisNicolas Langlois
Nicolas Langlois
HCHOUCINE CHAFOUK
HOUCINE CHAFOUK
In this paper we apply dynamic feedback linearization to the tracking problem for a turbocharged diesel engine (TDE) equipped with exhaust gas recirculation (EGR) valve and variable geometry turbocharger (VGT). The model used here is the third-order mean-value model, a reduction of the eighth-order mean-value one, see, for sake of simplicity. Our goal is to track desired values of suitably chosen outputs. In fact, we first plan to control the input manifold pressure and the compressor mass flow rate instead of the air fuel ratio (AFR) and the EGR fraction. Unfortunately, the former lead to a non-minimum phase system while the latter are not accessible for measurements in a vehicle, see. We thus replace the problem of tracking of desired values of the original output y (input manifold pressure and compressor mass flow rate) by that of tracking a suitably constructed modified output for which the values to be tracked are specifically chosen: namely, when the modified output y tilde approaches them, the original output converges to the desired values. Simulation results are presented.