Pod launch and landing system for vertical take-off and landing (VTOL) unmanned aerial vehicles (UAVs)
An unmanned aerial vehicle (UAV) storage and launch system, including: a UAV pod having an interior; and a telescoping UAV landing surface disposed in the interior of the UAV pod; where the telescoping UAV landing surface may translate up toward a top opening of the UAV pod, translate down into an interior of the UAV pod, or rotate relative to the UAV pod.
1. An unmanned aerial vehicle (UAV) launch system, comprising:
a UAV landing surface; and
one or more regions disposed on a surface proximate to the UAV landing surface, wherein each of the one or more regions correspond to one or more landing points of the UAV, and wherein each of the one or more regions comprise at least one of: a power connection and a communication connection with a corresponding landing point of the one or more landing points of the UAV;
wherein the UAV landing surface is configured to rotate the UAV relative to the one or more regions, and wherein the UAV landing surface is configured to lower the UAV to make contact between the one or more landing points of the UAV and the one or more regions.
2. The UAV launch system of claim 1 , wherein the UAV landing surface is configured to elevate the UAV above the one or more regions.
3. The UAV launch system of claim 1 , wherein the UAV landing surface is a telescoping UAV landing surface.
4. The UAV launch system of claim 1 , wherein the one or more landing points of the UAV are electrically conductive.
5. The UAV launch system of claim 4 , wherein the one or more landing points of the UAV are connected to at least one of: a battery and a data connection within the UAV.
6. The UAV launch system of claim 1 , wherein at least one of the one or more landing points is positioned on an end of a motor pod of the UAV.
7. The UAV launch system of claim 1 , wherein at least one of the one or more landing points is a positive lead.
8. The UAV launch system of claim 7 , wherein at least one of the one or more landing points is a negative lead.
9. The UAV launch system of claim 1 , wherein at least one of the one or more landing points is positioned on a vertical stabilizer of the UAV.
10. The UAV launch system of claim 1 , wherein the UAV landing surface is rotatable to account for crosswind during a launch of the UAV seated in the UAV landing surface.
11. The UAV launch system of claim 1 , wherein the UAV landing surface is configured to rotate to align a wing of the UAV seated on the UAV landing surface subsequent to a landing of the UAV.
12. The UAV launch system of claim 1 , wherein the UAV landing surface is configured to rotate to a predetermined alignment with respect to a prevailing wind.
13. The UAV launch system of claim 1 , wherein the one or more landing points comprise four landing points, wherein the one or more regions comprise four regions, and wherein the four regions comprise two power connections and two communication connections.
14. A method comprising:
vertically landing an unmanned aerial vehicle (UAV) on a UAV landing surface;
seating the UAV on one or more regions disposed on a surface proximate to the UAV landing surface, wherein each of the one or more regions correspond to one or more landing points of the UAV, and wherein each of the one or more regions comprise at least one of: a power connection and a communication connection with a corresponding landing point of the one or more landing points of the UAV;
rotating the UAV on the UAV landing surface relative to the one or more regions; and
lowering the UAV on the UAV landing surface to make contact between the one or more landing points of the UAV and the one or more regions.
15. The method of vertically landing the UAV of claim 14 further comprising:
elevating the UAV landing surface above the one or more regions.
16. The method of vertically landing the UAV of claim 14 further comprising:
guiding, by one or more pairs of guide paddles, the wing of the UAV into a proper angular orientation relative to the UAV landing surface, wherein each pair of guide paddles forms a V-channel, and wherein the wing of the UAV is at least partially disposed within the V-channel when the UAV is landed.
17. The method of vertically landing the UAV of claim 14 further comprising:
rotating the UAV landing surface to a predetermined alignment with respect to a prevailing wind subsequent to the landing of the UAV.
18. The method of vertically landing the UAV of claim 14 further comprising:
rotating the UAV landing surface to a predetermined alignment with respect to a prevailing wind; and
launching the UAV from the UAV landing surface.
19. The method of vertically landing the UAV of claim 14 further comprising:
providing power to a battery of the UAV from the power connection of the one or more regions.
20. The method of vertically landing the UAV of claim 14 further comprising:
providing data to a data connection of the UAV from the communication connection of the one or more regions.