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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
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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
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Stable Model Predictive Strategy for Rendezvous Hovering Phases Allowing for Control Saturation

 Paulo Ricardo Arantes Gilz , Mioara Maria Joldes , Christophe Louembet , Frédéric Camps
Journal of Guidance, Control, and Dynamics, 2019, 42 (8), ⟨10.2514/1.G003558⟩
Article dans une revue hal-01678768v2
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Validated Semi-Analytical Transition Matrices for Linearized Relative Spacecraft Dynamics via Chebyshev Series Approximations

 Paulo Ricardo Arantes Gilz , Florent Bréhard , Clément Gazzino
SCITECH 2018 - AIAA Science and Technology Forum and Exposition, 28th Space Flight Mechanics Meeting, Jan 2018, Kissimmee, United States. pp.1-23, ⟨10.2514/6.2018-1960⟩
Communication dans un congrès hal-01540170v3
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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
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Embedded and validated control algorithms for the spacecraft rendezvous

 Paulo Ricardo Arantes Gilz
Embedded Systems. Université Paul Sabatier - Toulouse III, 2018. English. ⟨NNT : 2018TOU30155⟩
Thèse tel-01922288v2
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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
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A non-linear simulator written in C for orbital spacecraft rendezvous applications.

 Paulo Ricardo Arantes Gilz
2016
Pré-publication, Document de travail hal-01410075v1
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A Matlab®/Simulink® non-linear simulator for orbital spacecraft rendezvous applications.

 Paulo Ricardo Arantes Gilz
2016
Autre publication scientifique hal-01413328v1
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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
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