作者: Marco Tursini , Giuseppe Fabri , Emidio Della Loggia , Marco Villani
DOI: 10.1109/ESARS.2012.6387469
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摘要: This work describes the control technique of a Fault-Tolerant electromechanical system aimed to actuation flap panels aircraft. The application provides adoption couple permanent magnet synchronous motors designed match minimum load requirements even in case fault one or two phases. consolidated mechanical synchronization mutual is replaced by fully electronic solution. usual master-slave configuration actuators with speed and correction tracking error parallel position control. solution allows avoid complex management applies same philosophy adopted inside for single multiphase motor. developed tested on test-bed emulate real aerodynamic condition. achieved results show effectiveness proposed