Method for recovering a UAV

1. A method for recovering an unmanned aerial vehicle (UAV) after a flight comprising:

setting up a UAV recovery system at a recovery site, the UAV recovery system comprising a capture net support assembly, and a pneumatic capture net, the pneumatic net comprising a set of inflatable, flexible, compliant tubes;

the setting up step comprising:

erecting the pneumatic capture net on a support surface at a recovery site, the pneumatic capture net erecting step comprising:

supporting the pneumatic net adjacent to support surface using the capture net support assembly; and

inflating the set of tubes of the pneumatic net to place the tubes in an inflated, use state extending upwardly away from the base;

directing the UAV into the pneumatic net along a final flight path, the UAV having wings with forward edges;

creating a drag force on the UAV by engagement of at least the forward edges of the wings with at least some of the tubes as the UAV moves along a terminal segment of a final flight path;

the drag force creating step comprising resisting movement of the pneumatic net using decelerators operably connecting the pneumatic net to the support surface by restraint straps;

temporarily preventing at least one of the decelerators from releasing restraint strap from the decelerator; and

sensing when the UAV engages the pneumatic net and then permitting said at least one decelerator to release restraint strap from the decelerator.

2. The method according to claim 1 , wherein the drag force creating step comprises resisting movement of the pneumatic net using decelerators operably connected to the pneumatic net.

3. The method according to claim 1 , wherein sensing and then permitting step is carried out using a trigger net at the pneumatic net coupled to the at least one decelerator by a trigger line, and further comprising:

placing the at least one decelerator in an unlocked, use condition when the UAV engages the trigger net causing the trigger line to change the decelerator from a locked condition, during which restraint strap is prevented from being pulled from the decelerator, to the unlocked, use condition, during which restraint strap can be pulled from the decelerator.

4. The method according to claim 1 , wherein:

the setting up step is carried out with the set of tubes having a width and a height defining an impact area when the tubes are in the inflated, use state; and

the directing step comprises directing the UAV into the impact area.

5. The method according to claim 1 , wherein:

the setting up step is carried out with the UAV recovery system comprising a ground tarp; and

the setting up step further comprising positioning the ground tarp between the support surface and the base.

6. The method according to claim 1 , wherein the setting up step is carried out with the UAV recovery system comprising a generally vertically-extending row of inflatable, compliant, flexible tubes, and the drag force creating step further comprises folding at least some of said engaged tubes over the wings causing the tubes to exert decelerating forces on the UAV.

7. The method according to claim 1 , wherein the UAV recovery system comprises a base and the setting up step comprises placing the base on the support surface.

8. A method for recovering an unmannered aerial vehicle (UAV) after a flight comprising:

setting up a UAV recovery system at a recovery site, the UAV recovery system comprising a capture net support assembly, and a pneumatic capture net, the pneumatic net comprising a set of inflatable, flexible, compliant tubes;

the setting up step is carried out with the pneumatic capture net comprising a row of tubes, the tubes having first and second ends, the first ends of the tubes being physically and fluidly connected to one another by a lower connector and the second ends of the tubes being physically and fluidly connected to one another by an upper connector;

the setting up step comprising

erecting the pneumatic capture net on a support surface at a recovery site, the pneumatic capture net erecting step comprising:

supporting the pneumatic net adjacent to the support surface using the capture net support assembly;

inflating the set of tubes of the pneumatic net to place the tubes in an inflated, use state extending upwardly away from the base; and

positioning the first ends of the tubes adjacent to the support surface;

directing the UAV into the pneumatic net along a final flight path the UAV having wings with forward edges; and

creating a drag force on the UAV by engagement of at least the forward edges of the wings with at least some of the tubes as the UAV moves along a terminal segment of a final flight path.

9. The method according to claim 8 , wherein the drag force creating step comprises resisting movement of the pneumatic net using decelerators operably connected to the pneumatic net.

10. The method according to claim 9 , wherein:

the setting up step is carried out with the set of tubes having a width and a height defining an impact area when the tubes are in the inflated, use state; and

the directing step comprises directing the UAV into the impact area.

11. The method according to claim 9 , wherein:

the setting up step is carried out with the UAV recovery system comprising a ground tarp; and

the setting up step further comprising positioning the ground tarp between the support surface and the base.

12. The method according to claim 9 , wherein the setting up step is carried out with the UAV recovery system comprising a generally vertically-extending row of inflatable, compliant, flexible tubes, and the drag force creating step further comprises folding at least some of said engaged tubes over the wings causing the tubes to exert decelerating forces on the UAV.

13. The method according to claim 9 , wherein the UAV recovery system comprises a base and the setting up step comprises placing the base on the support surface.