The invention relates to an integrated ejection /
recovery device of a shipborne unmanned aerial vehicle, which comprises a base, a stability augmentation device, a base seat, an ejection device and a
recovery device. The base seat is mounted on the base through bearings so as to be rotatable in the circumferential direction, and a
cushioning device is mounted on the bottom of the base seat for reducing the
impact force. The ejection device and
recovery device of the unmanned aerial vehicle (UAV) are integrated into one body, which reduces the occupying space, improves the mobility of the device, and expands the application range of the UAV take-off and landing auxiliary device. Using the rotating base structure, the unmanned aerial vehicle (UAV) ejection take-off slideway is used as rockerarm, and the
impact load is converted into torque by the integral rotating motion of the slideway and the base seat and transmitted to the
cushion device in the base seat, which reduces the structuralstrength requirement of the collision net recovery
system for UAV, and reducing the self-weight of the UAV. Through the self-stabilizing device and the terminal guiding device, the recovery precisionof the unmanned aerial vehicle is improved, and the influence of the
operating environment on the recovery precision and the operating pressure of the unmanned aerial vehicle are reduced.