| 摘要 |
An aerial delivery assembly such as a glider 10 for autonomously delivering a load to a target location comprises an airframe including a main body 10 and at least one deployable lift providing structure such as wings 30. The lift providing structure is moveable between a stowed position and a deployed position. The assembly includes at least one deployable and adjustable control structure for controlling the flight of the assembly and moveable between a stowed position and a deployed position. The adjustable control structure may include a tail 16 with vertical and horizontal stabilisers 34, 36. The main body comprises a compartment for receiving a load to be delivered. The assembly further comprises a control unit comprising an actuation module for receiving position information and for use in adjusting the control structure. The control unit is releaseably connected to the airframe such that it is reusable in an aerial delivery assembly having a different airframe. |
