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	Pour les 39 documents Envoyer sur ORCID RSS ATOM Exporter BibTeX XML-TEI CSV RTF EndNote PDF HTML Export avancé	Page : Page précédente 1 2 Page suivante	triés par Pertinence Auteur A→Z Auteur Z→A Titre A→Z Titre Z→A Date de publication croissante Date de publication décroissante Date de dépôt croissante Date de dépôt décroissante

		Design of Algorithms for Satellite Slew Manoeuver by Flatness and Collocation Christophe Louembet , Franck Cazaurang , Ali Zolghadri American Control Conference, Jul 2007, New York, United States. pp.3168 - 3173, ⟨10.1109/ACC.2007.4282459⟩ Communication dans un congrès hal-00180798v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Path planning for satellite slew maneuvers: A combined Flatness and Collocation based Approach Christophe Louembet , Franck Cazaurang , Ali Zolghadri IET Control Theory and Applications, 2009, 3 (4), pp.481-491. ⟨10.1049/iet-cta.2008.0054⟩ Article dans une revue hal-00324646v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Predictive control algorithm for spacecraft rendezvous hovering phases Paulo Ricardo Arantes Gilz , Christophe Louembet European Control Conference, Jul 2015, Linz, Austria Communication dans un congrès hal-01078506v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Embedding a SDP-based control algorithm for the orbital rendezvous hovering phases Frédéric Camps , Paulo Ricardo Arantes Gilz , Mioara Joldes , Christophe Louembet International Conference on Integrated Navigation Systems (ICINS 2018), May 2018, Saint Petersburg, Russia. 10p Communication dans un congrès hal-01729956v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		V-bar and R-bar Glideslope Guidance Algorithms for Fixed-Time Rendezvous: A Linear Programming Approach Yassine Ariba , Denis Arzelier , Laura Sofia Urbina , Christophe Louembet 20th IFAC Symposium on Automatic Control in Aerospace, Aug 2016, Sherbrooke, Canada Communication dans un congrès hal-01358188v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		A Flatness-Based Predictive Controller for Six-Degrees of Freedom Spacecraft Rendezvous Julio C Sanchez , Francisco Gavilan , Rafael Vazquez , Christophe Louembet Acta Astronautica, 2020, 167, pp.391-403. ⟨10.1016/j.actaastro.2019.11.026⟩ Article dans une revue hal-02155012v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Motion planning for flat systems using positive B-splines: An LMI approach Christophe Louembet , Franck Cazaurang , Ali Zolghadri Automatica, 2010, 46 (8), pp.Pages 1305-1309. ⟨10.1016/j.automatica.2010.05.001⟩ Article dans une revue hal-00636595v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		A two-impulse method for stabilizing the spacecraft relative motion with respect to a periodic trajectory Georgia Deaconu , Christophe Louembet , Alain Théron 51st Annual Conference on Decision and Control (CDC 2012), Dec 2012, Maui, United States. ⟨10.1109/CDC.2012.6426542⟩ Communication dans un congrès hal-01872905v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Linearized Impulsive Fixed-Time Fuel-Optimal Space rendezvous: A New Numerical Approach Denis Arzelier , Florent Bréhard , Norbert Deak , Mioara Joldes , Christophe Louembet , et al. 20th IFAC Symposium on Automatic Control in Aerospace, Aug 2016, Sherbrooke, Canada. ⟨10.1016/j.ifacol.2016.09.064⟩ Communication dans un congrès hal-01275427v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Minimizing the Effects of Navigation Uncertainties on the Spacecraft Rendezvous Precision Georgia Deaconu , Christophe Louembet , Alain Théron Journal of Guidance, Control, and Dynamics, 2014, 37 (2), pp.695-700. ⟨10.2514/1.62219⟩ Article dans une revue hal-01078527v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Robust Rendezvous Planning Under Maneuver Execution Errors Christophe Louembet , Denis Arzelier , Georgia Deaconu Journal of Guidance, Control, and Dynamics, 2015, 38 (1), pp.76-93. ⟨10.2514/1.G000391⟩ Article dans une revue hal-01078508v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Constrained periodic spacecraft relative motion using non-negative polynomials Georgia Deaconu , Christophe Louembet , Alain Théron American Control Conference (ACC 2012), Jun 2012, Montreal, Canada. pp.6715-6720 Communication dans un congrès hal-00639905v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		A New Mixed Iterative Algorithm to Solve the Fuel-Optimal Linear Impulsive Rendezvous Problem Denis Arzelier , Christophe Louembet , Aude Rondepierre , Mounir Kara-Zaitri Journal of Optimization Theory and Applications, 2013, 159 (1), pp. 210-230 Article dans une revue hal-00687499v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Model predictive control for rendezvous hovering phases based on a novel description of constrained trajectories Paulo Ricardo Arantes Gilz , Mioara Joldes , Christophe Louembet , Frédéric Camps IFAC World Congress, Jul 2017, Toulouse, France. pp.7490-7495 Communication dans un congrès hal-01484764v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		A Flatness-Based Predictive Controller for Six-Degrees of Freedom Spacecraft Rendezvous Julio C Sanchez , Francisco Gavilan , Rafael Vazquez , Christophe Louembet IFAC Workshop on Networked & Autonomous Air & Space Systems, Jun 2018, Santa Fe, Nouveau Mexique, United States Communication dans un congrès hal-02071291v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Contributions au guidage pour le rendez-vous spatial par résolution du problème de commande optimale impulsionnelle Christophe Louembet Automatique / Robotique. Université Toulouse 3 Paul Sabatier (UT3 Paul Sabatier), 2017 HDR tel-01960763v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Impulsive zone model predictive control for rendezvous hovering phases Christophe Louembet , Alejandro Hernan Gonzalez , Paulo Ricardo Arantes Gilz Conference on Decision and Control, Dec 2019, Nice, France Communication dans un congrès hal-02154952v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		A Three-step Decomposition Method for Solving the Minimum-Fuel Geostationary Station Keeping of Satellites Equipped with Electric Propulsion Clément Gazzino , Denis Arzelier , Luca Cerri , Damiana Losa , Christophe Louembet , et al. Acta Astronautica, 2019, 158, pp.12-22. ⟨10.1016/j.actaastro.2018.08.015⟩ Article dans une revue hal-01696455v2	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Flatness and collocation based methodology for satellite trajectory planning Christophe Louembet , Franck Cazaurang , Ali Zolghadri IEEE International Symposium on Control, Communications, and Signal Processing, Mar 2006, Marrakech, Morocco. pp.NC Communication dans un congrès hal-00243129v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Convex inner approximations of nonconvex semialgebraic sets applied to fixed-order controller design Didier Henrion , Christophe Louembet International Journal of Control, 2012, 85 (8), pp. 1083-1092 Article dans une revue hal-00585633v2	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Designing Continuously Constrained Spacecraft Relative Trajectories for Proximity Operations Georgia Deaconu , Christophe Louembet , Alain Théron Journal of Guidance, Control, and Dynamics, 2015, 38 (7), pp.1208-1217. ⟨10.2514/1.G000283⟩ Article dans une revue hal-01078528v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Integer Programming for Optimal Control of Geostationary Station Keeping of Low-Thrust Satellites Clément Gazzino , Christophe Louembet , Denis Arzelier , Nicolas Jozefowiez , Damiana Losa , et al. IFAC World Congress, Jul 2017, Toulouse, France. pp.8499-8504 Communication dans un congrès hal-01416694v4	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		A Minimum-Fuel Fixed-Time Low-Thrust Rendezvous Solved with the Switching Systems Theory Clément Gazzino , Denis Arzelier , Luca Cerri , Damiana Losa , Christophe Louembet , et al. Transactions of the Japan Society for Aeronautical and Space Sciences, 2018, ISTS Special Issue, 16 (7), pp.628-634. ⟨10.2322/tastj.16.628⟩ Article dans une revue hal-01609252v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Solving the Minimum-Fuel Low-Thrust Geostationary Station Keeping Problem via the Switching Systems Theory Clément Gazzino , Denis Arzelier , Luca Cerri , Damiana Losa , Christophe Louembet , et al. 7th European Conference for Aeronautics and Space Sciences (EUCASS 2017), Jul 2017, Milano, Italy. 14p Communication dans un congrès hal-01562696v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Génération de trajectoire pour satellite AGILE par platitude et collocation Franck Cazaurang , Christophe Louembet , Ali Zolghadri Conférence Internationale Francophone d'Automatique CIFA 2006, Jun 2006, Bordeaux, France. pp.N.C Communication dans un congrès hal-00180809v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Collision avoidance in low thrust rendezvous guidance using flatness and positive B-splines Christophe Louembet , Georgia Deaconu American Control Conference 2011 (ACC 2011), Jun 2011, San Francisco, United States. 6p Communication dans un congrès hal-00526269v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Sécurisation passive du rendez-vous orbital par des polynômes non négatifs Georgia Deaconu , Christophe Louembet , Alain Théron Conférence Internationale Francophone d'Automatique (CIFA2012), Jul 2012, Grenoble, France. pp. 811-816 Communication dans un congrès hal-00639908v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Computing impulsive equilibrium sets with respect to target zone for linear impulsive systems Christophe Louembet , Alejandro Hernan Gonzalez , Ignacio Sanchez 21st IFAC World Congress, Jul 2020, Berlin, Germany Communication dans un congrès hal-02403599v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		Event-triggered Model predictive control for spacecraft rendezvous Christophe Louembet , Paulo Ricardo Arantes Gilz 6th IFAC Conference on Nonlinear Model Predictive Control (NMPC 2018), Aug 2018, Madison, United States. 2p Communication dans un congrès hal-01844002v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More
		A hybrid control framework for impulsive control of satellite rendezvous Mirko Brentari , Laura Sofia Urbina , Denis Arzelier , Christophe Louembet , Luca Zaccarian IEEE Transactions on Control Systems Technology, 2019, 27 (4), pp.1537-1551. ⟨10.1109/TCST.2018.2812197⟩ Article dans une revue hal-01741201v1	Envoyer sur ORCID Exporter BibTeX XML-TEI Dublin Core DC Terms EndNote DataCite Export avancé Partager Gmail Facebook X LinkedIn More

Filtrer vos résultats

Design of Algorithms for Satellite Slew Manoeuver by Flatness and Collocation

Path planning for satellite slew maneuvers: A combined Flatness and Collocation based Approach

Predictive control algorithm for spacecraft rendezvous hovering phases

Embedding a SDP-based control algorithm for the orbital rendezvous hovering phases

V-bar and R-bar Glideslope Guidance Algorithms for Fixed-Time Rendezvous: A Linear Programming Approach

A Flatness-Based Predictive Controller for Six-Degrees of Freedom Spacecraft Rendezvous

Motion planning for flat systems using positive B-splines: An LMI approach

A two-impulse method for stabilizing the spacecraft relative motion with respect to a periodic trajectory

Linearized Impulsive Fixed-Time Fuel-Optimal Space rendezvous: A New Numerical Approach

Minimizing the Effects of Navigation Uncertainties on the Spacecraft Rendezvous Precision

Robust Rendezvous Planning Under Maneuver Execution Errors

Constrained periodic spacecraft relative motion using non-negative polynomials

A New Mixed Iterative Algorithm to Solve the Fuel-Optimal Linear Impulsive Rendezvous Problem

Model predictive control for rendezvous hovering phases based on a novel description of constrained trajectories

A Flatness-Based Predictive Controller for Six-Degrees of Freedom Spacecraft Rendezvous

Contributions au guidage pour le rendez-vous spatial par résolution du problème de commande optimale impulsionnelle

Impulsive zone model predictive control for rendezvous hovering phases

A Three-step Decomposition Method for Solving the Minimum-Fuel Geostationary Station Keeping of Satellites Equipped with Electric Propulsion

Flatness and collocation based methodology for satellite trajectory planning

Convex inner approximations of nonconvex semialgebraic sets applied to fixed-order controller design

Designing Continuously Constrained Spacecraft Relative Trajectories for Proximity Operations

Integer Programming for Optimal Control of Geostationary Station Keeping of Low-Thrust Satellites

A Minimum-Fuel Fixed-Time Low-Thrust Rendezvous Solved with the Switching Systems Theory

Solving the Minimum-Fuel Low-Thrust Geostationary Station Keeping Problem via the Switching Systems Theory

Génération de trajectoire pour satellite AGILE par platitude et collocation

Collision avoidance in low thrust rendezvous guidance using flatness and positive B-splines

Sécurisation passive du rendez-vous orbital par des polynômes non négatifs

Computing impulsive equilibrium sets with respect to target zone for linear impulsive systems

Event-triggered Model predictive control for spacecraft rendezvous

A hybrid control framework for impulsive control of satellite rendezvous