Fault detection and isolation of the attitude control subsystem of spacecraft formation flying using extended Kalman filters

DOI10.1080/00207179.2015.1039591zbMath1334.93160OpenAlexW2060424125MaRDI QIDQ2799253

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Publication date: 8 April 2016

Published in: International Journal of Control (Search for Journal in Brave)

Full work available at URL: https://spectrum.library.concordia.ca/977399/1/Ghasemi_MSc_F2013.pdf

zbMATH Keywords

extended Kalman filterfault detection and isolationactuator faultsformation flight of satellites

Mathematics Subject Classification ID

Filtering in stochastic control theory (93E11) Estimation and detection in stochastic control theory (93E10) Decentralized systems (93A14) Stochastic systems in control theory (general) (93E03)

Related Items (5)

Attitude coordinated output feedback control based on event triggering for multiple spacecrafts ⋮ A nonlinear observer-based approach to fault detection, isolation and estimation for satellite formation flight application ⋮ Adaptive finite‐time actuator fault‐tolerant coordinated attitude control of multispacecraft with input saturation ⋮ Fault-tolerant cooperative output regulation for multi-vehicle systems with sensor faults ⋮ Distributed finite-time tracking control for multiple uncertain Euler-Lagrange systems with error constraints

Cites Work

• Hybrid fault diagnosis of nonlinear systems using neural parameter estimators
• Distributed fault detection for interconnected second-order systems
• A survey of design methods for failure detection in dynamic systems

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