Assessment of a Supervisory Fault-Hiding Scheme in a Classical Guidance, Navigation and Control Setup: the e.Deorbit mission
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Data
2019-09-18
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4th International Conference on Control and Fault-Tolerant Systems (SYSTOL)
Resumo
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.
Descrição
International Conference on Control and Fault-Tolerant Systems (SYSTOL)
Palavras-chave
ASTRONÁUTICA, AERONÁUTICA, SISTEMAS DE CONTROLO AUTOMÁTICO, AERONAUTICS, CONTROL SYSTEMS, ASTRONAUTICS
Citação
Cieslak, 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.