The application discloses an electromagnetic force direct driving type
dragonfly imitating
flapping wing aircraft platform and a flight control method thereof, and relates to the technical fields of bionic aircraft and electromagnetic driving control. The aircraft platform comprises a body, front and rear
flapping wing groups, a wing-body connecting rod, an electromagnetic driving device and a main controller. The electromagnetic driving device is composed of a driving shell, a permanent
magnet and a transmission connecting rod. The main controller adjusts the amplitude, direction and frequency of the
driving current of the conductive coil, generates electromagnetic force to drive the
flapping wing to reciprocally flap, and realizes the
controllability of the amplitude, direction and frequency. The method establishes a target speed and equivalent frequency mapping in a manual mode, calculates a frequency error based on the feedback of an inductive device, and adjusts the
driving current parameters through a PID
closed loop. In a target navigation task, path planning,
image acquisition, obstacle detection, straight flight or
obstacle avoidance branches and heading correction cycles are executed. The scheme has fast response and compact structure, and can realize stable hovering, sensitive steering and autonomous navigation.