Abstract: The invention provides a pan-tilt-zoom (PTZ) camera, including a pan-tilt unit and a camera unit. The pan-tilt unit includes a first vibration damper plate, a second vibration damper plate, and a shock absorber ball; the camera unit is fixedly disposed on the first vibration damper plate, the shock absorber ball is sandwiched between the first vibration damper plate and the second vibration damper plate, and the shock absorber ball is fixedly connected to the second vibration damper plate; the shock absorber ball is elastic, and when the camera unit is horizontally laid, the first vibration damper plate is out of touch with the shock absorber ball; when the camera unit is subjected to extra load other than gravity, the first vibration damper plate compresses the shock absorber ball. The pan-tilt unit of the invention is simple in structure and safe in use.

Abstract: The invention provides a method for recording a flight path and controlling automatic flight of an unmanned aerial vehicle. The method includes: controlling, by a remote control or a smart mobile terminal device, the unmanned aerial vehicle to fly following a certain flight path according to user's requirement, triggering the unmanned aerial vehicle to record the flight path, storing tracking data, and selecting a learning track to fly automatically, where a flight mode comprises at least GPS learning mode, GPS automatic mode, and manual mode. The unmanned aerial vehicle having the control mode can be triggered to fly automatically following the tracking data stored in the flight control device according to different application scenarios, thus increasing the user experience and entertainment.

Abstract: Described herein is a vertical take-off and landing aircraft comprising: an upper enclosure comprising a first upper arm and a second upper arm; a lower enclosure comprising a first lower arm and a second lower arm; wherein the first upper arm and the first lower arm comprise a first upper buckle and a first lower buckle, respectively; wherein the second upper arm and the second lower arm comprise a second upper buckle and a second lower buckle, respectively; wherein the first upper buckle engages the first lower buckle and the second upper buckle engages the second lower buckle, thereby securing the upper enclosure to the lower enclosure.

Abstract: Described herein is a vertical take-off and landing aircraft comprising: an upper enclosure comprising a first upper arm and a second upper arm; a lower enclosure comprising a first lower arm and a second lower arm; wherein the first upper arm and the first lower arm comprise a first upper buckle and a first lower buckle, respectively; wherein the second upper arm and the second lower arm comprise a second upper buckle and a second lower buckle, respectively; wherein the first upper buckle engages the first lower buckle and the second upper buckle engages the second lower buckle, thereby securing the upper enclosure to the lower enclosure.