A two-stage extended Kalman filter method for fault estimation of satellite attitude control systems
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Publication:509360
DOI10.1016/J.JFRANKLIN.2016.06.034zbMath1355.93183OpenAlexW2498033163MaRDI QIDQ509360
Publication date: 9 February 2017
Published in: Journal of the Franklin Institute (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.jfranklin.2016.06.034
Filtering in stochastic control theory (93E11) Nonlinear systems in control theory (93C10) Estimation and detection in stochastic control theory (93E10) Variable mass, rockets (70P05)
Related Items (3)
Fault diagnosis for a class of nonlinear uncertain systems using deterministic learning approach ⋮ Robust state and sensor fault estimation for switched nonlinear systems based on asynchronous switched fuzzy observers ⋮ Two-stage exogenous Kalman filter for time-varying fault estimation of satellite attitude control system
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