Assessment of a Supervisory Fault-Hiding Scheme in a Classical Guidance, Navigation and Control Setup: the e.Deorbit mission

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dc.contributor.authorCieslak, Jérôme
dc.contributor.authorHenry, David
dc.contributor.authorColmenarejo, Pablo
dc.contributor.authorBranco, João
dc.contributor.authorSantos, Nuno
dc.contributor.authorSerra, Pedro
dc.contributor.authorTelaar, Jüergen
dc.contributor.authorStrauch, Hans
dc.contributor.authorGiordano, Alessandro
dc.contributor.authorStefano, Marco
dc.contributor.authorOtt, Christian
dc.contributor.authorReiner, Matthias
dc.contributor.authorJaworski, Jaroslaw
dc.contributor.authorPapadopoulos, Evangelos
dc.contributor.authorVisentin, Gianfranco
dc.contributor.authorAnkersen, Finn
dc.contributor.authorGil-Fernandez, Jesus
dc.date.accessioned2019-09-27T10:52:09Z
dc.date.available2019-09-27T10:52:09Z
dc.date.issued18/09/2019
dc.descriptionInternational Conference on Control and Fault-Tolerant Systems (SYSTOL)pt
dc.description.abstractThe design of a model-based Fault Tolerant Control (FTC) strategy based on Virtual Actuators (VA) in a built-in Guidance, Navigation and Control (GNC) setup is addressed for the e.Deorbit space mission. This mission, initiated by the European Space Agency (ESA), aims at removing a large defunct satellite from Earth orbit: ENVISAT. The goal of this paper is to promote academic solutions to add fault tolerance capacities against thruster faults without any change or new tuning of the already in-place GNC solution. The validation of the proposed FTC solution is assessed by a simulation campaign based on a high-fidelity nonlinear industrial simulator.en
dc.formatapplication/pdf
dc.identifier.urihttp://hdl.handle.net/10437/9797
dc.language.isoengpt
dc.publisher4th International Conference on Control and Fault-Tolerant Systems (SYSTOL)pt
dc.rightsopenAccess
dc.subjectASTRONAUTICSen
dc.subjectAERONAUTICSen
dc.subjectCONTROL SYSTEMSen
dc.subjectASTRONÁUTICApt
dc.subjectAERONÁUTICApt
dc.subjectSISTEMAS DE CONTROLO AUTOMÁTICOpt
dc.titleAssessment of a Supervisory Fault-Hiding Scheme in a Classical Guidance, Navigation and Control Setup: the e.Deorbit missionen
dc.typeconferenceObjecten

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