eprintid: 2206
rev_number: 11
eprint_status: archive
userid: 6
dir: disk0/00/00/22/06
datestamp: 2014-06-16 12:58:57
lastmod: 2016-04-06 10:33:26
status_changed: 2014-06-16 12:58:57
type: book_section
metadata_visibility: show
creators_name: Saponara, M.
creators_name: Barrena, V.
creators_name: Bemporad, Alberto
creators_name: Hartley, E. N.
creators_name: Maciejowski, Jan M.
creators_name: Richards, A.
creators_name: Tramutola, A.
creators_name: Trodden, P.
creators_id: 
creators_id: 
creators_id: alberto.bemporad@imtlucca.it
creators_id: 
creators_id: 
creators_id: 
creators_id: 
creators_id: 
title: Model predictive control application to spacecraft rendezvous in mars sample return scenario
ispublished: pub
subjects: TL
divisions: CSA
full_text_status: public
abstract: Model Predictive Control (MPC) is an optimization-based control strategy that is considered extremely attractive in the autonomous space rendezvous scenarios. The Online Recon¦guration Control System and Avionics Architecture (ORCSAT) study addresses its applicability in Mars Sample Return (MSR) mission, including the implementation of the developed solution in a space representative avionic architecture system. With respect to a classical control solution High-integrity Autonomous RendezVous and Docking control system (HARVD), MPC allows a signi¦cant performance improvement both in trajectory and in propellant save. Furthermore, thanks to the online optimization, it allows to identify improvements in other areas (i. e., at mission de¦nition level) that could not be known a priori
date: 2013-12
date_type: published
volume: 6
publisher: EDP Sciences
pagerange: 137-158
id_number: 10.1051/eucass/201306137
refereed: TRUE
book_title: Progress in Flight Dynamics, Guidance, Navigation, Control, Fault Detection, and Avionics
official_url: http://dx.doi.org/10.1051/eucass/201306137
citation:   Saponara, M. and Barrena, V. and Bemporad, Alberto and Hartley, E. N. and Maciejowski, Jan M. and Richards, A. and Tramutola, A. and Trodden, P.  Model predictive control application to spacecraft rendezvous in mars sample return scenario.   In:  Progress in Flight Dynamics, Guidance, Navigation, Control, Fault Detection, and Avionics.   EDP Sciences, pp. 137-158.       (2013)  
document_url: http://eprints.imtlucca.it/2206/1/EUCASS.pdf