A new aerodynamic decoupled frequential FDIR methodology for satellite actuator faults

DOI10.1002/acs.2379zbMath1327.93039OpenAlexW2117979882MaRDI QIDQ3458163

Nicola Mimmo, Silvio Simani, Pietro Baldi, Paolo Castaldi

Publication date: 8 December 2015

Published in: International Journal of Adaptive Control and Signal Processing (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/acs.2379

zbMATH Keywords

disturbance decouplingsatellite attitude controlactive fault tolerant controlfrequency signal analysisrobust fault detection and isolationnonlinear geometric approach

Mathematics Subject Classification ID

Related Items (2)

Actuator failure‐tolerant control of an all‐thruster satellite in coupled translational and rotational motion using neural networks ⋮ LEO satellite active FTC with aerodynamic disturbance decoupled fault diagnosis

Cites Work

• Unnamed Item
• Design and analysis of robust fault diagnosis schemes for a simulated aircraft model
• A geometric approach to nonlinear fault detection and isolation
• Fault detection and isolation for on‐board sensors of a general aviation aircraft

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