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

Abstract

Abstract—In this paper, the problem of fault detection and isolation in the attitude control subsystem of spacecraft formation flying is considered. In order to design the fault detection method, an extended Kalman filter is utilized which is a nonlinear stochastic state estimation method. Three fault detection architectures, namely, centralized… (More)
DOI: 10.1080/00207179.2015.1039591

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