Cieslak, JérômeHenry, DavidColmenarejo, PabloBranco, JoãoSantos, NunoSerra, PedroTelaar, JüergenStrauch, HansGiordano, AlessandroStefano, MarcoOtt, ChristianReiner, MatthiasJaworski, JaroslawPapadopoulos, EvangelosVisentin, GianfrancoAnkersen, FinnGil-Fernandez, Jesus2019-09-18Cieslak, J, Henry, D, Colmenarejo, P, Branco, J, Santos, N, Serra, P, Telaar, J, Strauch, H, Giordano, A, Stefano, M, Ott, C, Reiner, M, Jaworski, J, Papadopoulos, E, Visentin, G, Ankersen, F & Gil-Fernandez, J 2019, 'Assessment of a supervisory fault-hiding scheme in a classical guidance, Navigation and Control Setup : the e.Deorbit mission', Paper presented at 4th International Conference on Control and Fault-Tolerant Systems (SYSTOL), 18/09/19. https://doi.org/10.1109/SYSTOL.2019.8864753International Conference on Control and Fault-Tolerant Systems (SYSTOL)The 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.application/pdfengopenAccessASTRONÁUTICAAERONÁUTICASISTEMAS DE CONTROLO AUTOMÁTICOAERONAUTICSCONTROL SYSTEMSASTRONAUTICSAssessment of a supervisory fault-hiding scheme in a classical guidance, Navigation and Control Setup : the e.Deorbit missionconferenceObjecthttps://doi.org/10.1109/SYSTOL.2019.8864753