Systems and methods for in-flight recovery of a target aircraft by a host aircraft during forward flight
In-flight recovery of an unmanned aerial vehicle (UAV). A towline may be deployed by a host aircraft in-flight in order to recover a target UAV that is also in-flight. A reel on the host aircraft may pay out the towline having a fitting thereon. A catch on the target UAV may engage with the fitting on the towline, and the reel may then retract the towline to thereby pull in the target UAV to the host aircraft. The target UAV may then securely attach with the host aircraft.
1. A system for in-flight recovery of a target aircraft by a host aircraft during forward flight, the system comprising:
a reel configured to attach with the host aircraft;
a towline comprising an aft section and a fitting attached to the aft section, wherein the reel is configured to pay out the towline from the reel to extend the fitting away from the host aircraft during forward flight;
a catch system comprising at least one moveable arm configured to attach with the target aircraft and to transition from a first configuration to a second configuration, wherein in the first configuration, the catch system is configured to vertically receive a section of the towline located forward of the fitting, and in the second configuration, the at least one movable arm of the catch system is configured to prevent the towline from vertically separating from the catch system as the catch system and the towline move horizontally relative to each other;
wherein the catch system is further configured to couple with the fitting after a horizontal separation between the catch system and the fitting aft of the catch system is decreased such that the fitting and the catch system are brought into contact with one another, and wherein the reel is further configured to retract the towline with the catch system coupled with the fitting to direct the target aircraft towards the host aircraft.
2. The system of claim 1 , wherein the aft section of the towline includes a drogue configured to increase drag on the aft section of the towline to thereby cause the aft section to be oriented in a substantially horizontal orientation.
3. The system of claim 2 , wherein the drogue comprises the fitting.
4. The system of claim 2 , wherein the fitting is located along the towline forward of the drogue.
5. The system of claim 1 , wherein the catch system comprises two moveable arms configured to deploy, to guide the towline, and to stow.
6. The system of claim 5 , wherein the two moveable arms comprises a first arm and a second arm, wherein the first arm is configured to cross the second arm to prevent vertical separation of the towline from the catch system.
7. The system of claim 6 , wherein the two moveable arms are further configured to transition between a stowed configuration, the first configuration, and the second configuration, wherein in the stowed configuration the two moveable arms extend along opposite sides of target aircraft, wherein in the first configuration, the two moveable arms extend to receive the towline and define a capture envelope of the towline, and wherein in the second configuration the two moveable arms rotate downward towards each other and cross to create a closed section between the two moveable arms to capture the towline, wherein the two moveable arms guide the towline to a latch configured to engage with the fitting.
8. The system of claim 5 , wherein the two moveable arms comprise elongated members or hooks.
9. The system of claim 1 , wherein the catch system further comprises a latch configured to engage with the fitting.
10. The system of claim 1 , wherein the towline further comprises a weighted section and a forward section, wherein the forward section is separated from the aft section by the weighted section.
11. The system of claim 10 , wherein the aft section of the towline includes a drogue, and wherein the weighted section of the towline and the drogue are configured to cause the aft section of the towline to extend rearward from the weighted section at an angle of less than 180° (degrees) relative to the forward section.
12. A method for in-flight recovery of a target aircraft by a host aircraft during forward flight, the method comprising:
deploying a towline away from the host aircraft having a fitting coupled with the towline;
vertically receiving the towline with a catch system on the target aircraft forward of the fitting;
causing relative horizontal movement between the catch system and the towline to couple the fitting with the catch system; and
retracting the towline toward the host aircraft to direct the target aircraft toward the host aircraft after the catch system has engaged the fitting.
13. The method of claim 12 , further comprising orienting an aft section of the towline in a substantially horizontal orientation.
14. The method of claim 12 , further comprising detecting a position of the towline using an imaging system on the target aircraft and/or host aircraft, the imaging system comprising optical cameras.
15. The method of claim 12 , further comprising changing a configuration of the target aircraft to a tow configuration.
16. The method of claim 12 , wherein vertically receiving the towline with the catch system on the target aircraft includes deploying one or more arms of the catch system to receive the towline.
17. The method of claim 12 , further comprising horizontally receiving the fitting within a latch of the catch system on the target aircraft.
18. The method of claim 17 , further comprising deploying the latch from a stowed configuration to an open configuration, receiving the towline within the latch, and actuating the latch to a closed configuration with the towline secured therein.
19. The method of claim 12 , further comprising securing the target aircraft with the host aircraft.
20. A system for in-flight recovery of a target aircraft by a host aircraft during forward flight, the system comprising:
a reel configured to attach with the host aircraft;
a towline comprising an aft section and a fitting attached to the aft section, wherein the reel is configured to pay out the towline away from the host aircraft during forward flight such that the aft section extends substantially horizontally; and
a catch system coupled to the target aircraft and configured to vertically receive a section of the towline forward of the fitting, the catch system further configured to engage the fitting after relative motion between the catch system and fitting decreases a horizontal separation aft of the catch system,
wherein the reel is further configured to retract the towline with the catch system engaging the fitting to direct the target aircraft towards the host aircraft.
21. The system of claim 20 , wherein:
the system further comprises a decoupling mechanism mounted on the reel; and
the towline further comprises a weighted section located between a forward section and an aft section of the towline, the weighted section comprising a plurality of discrete weights; and
the discrete weights are configured to allow the towline to be released between the discrete weights of the weighted section by the decoupling mechanism.
22. The system of claim 21 , wherein the decoupling mechanism comprises a blade to sever a target portion of the towline between the discrete weights.
23. The system of claim 21 , wherein the decoupling mechanism comprises a releasable clamp to release a portion of the weighted section.
24. The system of claim 20 , wherein the catch system is further configured to transition from a first configuration to a second configuration, wherein in the first configuration the catch system is configured to vertically receive a part of the towline located forward of the fitting, and in the second configuration the catch system is configured to prevent vertical separation of the towline from the catch system as the catch system and the towline move horizontally relative to each other.
25. The system of claim 20 , wherein the towline further comprises a weighted section and a forward section, wherein the forward section is separated from the aft section by the weighted section.
26. The system of claim 25 , further comprising a drogue attached with the aft section, and wherein the weighted section of the towline and the drogue are configured to cause the aft section of the towline to extend rearward from the weighted section at an angle of less than 180° (degrees) relative to the forward section.
27. The system of claim 26 , wherein the drogue is one of a chute, a streamer, and a solid-body object.
28. The system of claim 26 , wherein the fitting is located forward of the drogue.
29. The system of claim 20 , wherein the catch system comprises one or more catch arms configured to deploy, to guide the towline, and to stow.
30. The system of claim 29 , wherein the one or more arms comprises a first arm and a second arm, wherein the first arm is configured to cross the second arm to prevent vertical separation of the towline from the catch system.
31. The system of claim 29 , wherein the one or more catch arms are further configured to transition between a stowed configuration, an open configuration, and a closed configuration, wherein in the stowed configuration the one or more catch arms extend along opposite sides of target aircraft, wherein in the open configuration, the one or more catch arms extend to receive the towline and define a capture envelope of the towline, and wherein in the closed configuration the one or more catch arms rotate downward towards each other and cross to create a closed section between the one or more catch arms to capture the towline, wherein the one or more catch arms guide the towline to a latch configured to engage with the fitting.