Spacecraft actuator diagnosis with principal component analysis: application to the rendez-vous phase of the Mars sample return mission

DOI10.1155/2015/204918zbMath1326.93059OpenAlexW1582748774WikidataQ59112364 ScholiaQ59112364MaRDI QIDQ892579

Kamal Benothman, Philippe Dague, Othman Nasri, Imen Gueddi

Publication date: 19 November 2015

Published in: Journal of Control Science and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2015/204918

zbMATH Keywords

principal component analysis (PCA)fault detection and isolation (FDI)autonomous spacecraftMars sample return (MSR) missionrendezvous phase

Mathematics Subject Classification ID

Eigenvalue problems (93B60) Variable mass, rockets (70P05)

Related Items (3)

Application of residual-based EWMA control charts for detecting faults in variable-air-volume air handling unit system ⋮ A new interval diagnosis method: Application to the spacecraft rendezvous phase of the Mars sample return mission ⋮ A Bayesian approach to control loop performance diagnosis incorporating background knowledge of response information

Cites Work

• Fault detection, isolation and estimation for Takagi-Sugeno nonlinear systems
• Fault-Diagnosis Applications
• Fault Detection and Isolation with Robust Principal Component Analysis
• Fault detection and isolation for on‐board sensors of a general aviation aircraft
• Some Theorems on Quadratic Forms Applied in the Study of Analysis of Variance Problems, I. Effect of Inequality of Variance in the One-Way Classification

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