Event-triggered Model predictive control for spacecraft rendezvous
Résumé
In the context of space rendezvous hovering phase, a event-triggered predictive controller has been designed in order to maintain the relative position of a chaser spacecraft relatively to a target for orbit servicing purposes. The main goal is to minimize the consumption and the computation burden of the controller with respect to previously developed controller.
Domaines
Automatique / Robotique
Origine : Fichiers produits par l'(les) auteur(s)
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