Actuator Faults Estimation for a Helicopter UAV in the Presence of Disturbances
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DOI: 10.1007/s40313-020-00621-9
Abstract: The aim of this paper is to develop robust three-stage extended Kalman filter for a model based on a fault detection and identification for nonlinear hover mode system of helicopter unmanned aerial vehicle. In addition,… read more here.
Keywords: presence; estimation helicopter; faults estimation; actuator faults ... See more keywords