The invention provides an
aviation permanent magnet synchronous motor control architecture based on master-slave redundancy and
model prediction, belongs to the field of
aviation electric propulsion control systems, and aims to solve the problems of
extreme environment parameter drift, single-fault shutdown, multi-
target control conflict, fault diagnosis
lag and the like of an existing
system. The control architecture comprises a master-slave dual-redundancy
control unit, a wide-temperature-range adaptive
model prediction control unit, an
electromagnetic interference adaptive suppression unit and a multi-dimensional
fault tolerance unit. According to the invention, a DSP + FPGA heterogeneous redundant architecture is matched with two-out-of-three voting logic, so that fault non-
perception switching is realized; an
extended Kalman filter observer is embedded to update motor parameters on line, and take-off /
cruise / landing three
modes are preset; interference at the
frequency band of 100kHz-10MHz is controlled and suppressed through adaptive notch filtering and a sliding mode variable structure; a long short-
term memory network is fused to realize accurate diagnosis of early faults, and the
system is adaptive to
aviation scenes such as electric
general aviation aircrafts and unmanned aerial vehicles.