The invention provides a unified
electric control method and device for turning and shimmy damping of a front wheel of an
airplane, and solves the technical problems of
high complexity and poor adaptability. The device comprises a
voltage sensor used for collecting a
bus voltage value of a DC power supply loop of an
inverter; the power switch device is used for controlling the switch-in and switch-out of the
energy consumption resistor R1 in the power supply loop; the
relay is used for controlling the on-off of a power supply loop between the direct-current power supply and the
inverter; and the
logic control module is used for responding to a control requirement, outputting a PWM
signal according to a preset control strategy of the corresponding
control mode and performing power supply
loop control. A turning / shimmy damping unified
electric control framework based on
electric control is formed to be matched with a unified electric control strategy, a hydraulic shimmy damping device is simplified, and meanwhile the weight and cost of an undercarriage are reduced. Through
control mode switching, a PWM technology is adopted to drive the front wheel to actively steer in a control state, and shimmy damping is provided in a non-control state.