System and method for capturing and releasing fixed-wing aircraft
A capture-and-release aircraft for capturing and releasing fixed-wing aircraft is provided. The capture-and-release aircraft comprises a frame to which is secured a set of rotor units. Each rotor unit has a rotor with a rotation axis, the rotation axes of the rotors being generally parallel. A set of aircraft engagement members is also secured to the frame that can align with a set of anchors of a fixed-wing aircraft to releasably couple with the anchors.
1. A capture-and-release aircraft for capturing and releasing a fixed-wing aircraft, comprising:
a frame;
a set of at least three rotor units secured to the frame, each of the at least three rotor units being configured to generate vertical lift; and
a set of at least three aircraft engagement members secured to the frame, each of the at least three aircraft engagement members comprising:
an anchor-capture device configured to releasably couple to a corresponding one of a set of anchors of a fixed-wing aircraft, and
an articulating arm coupled to the anchor-capture device and controllable to move the anchor-capture device relative to the frame through at least two dimensions to align the anchor-capture device with the corresponding one of the set of anchors of the fixed-wing aircraft,
a first and a second of the at least three aircraft engagement members being spaced laterally to position the first of the at least three aircraft engagement members towards a first wing of the fixed-wing aircraft to engage the corresponding one of the set of anchors positioned on the first wing, and a second of the at least three aircraft engagement members towards a second wing of the fixed-wing aircraft on an opposite lateral side of the fixed-wing aircraft from the first wing to engage the corresponding one of the set of anchors positioned on the second wing.
2. The capture-and-release aircraft according to claim 1 , wherein the capture-release aircraft further comprises a refueling hose extendable towards a fuel receptacle of the fixed-wing aircraft.
3. The capture-and-release aircraft according to claim 1 , wherein a third of the at least three aircraft engagement members is spaced longitudinally in a fore or aft direction from at least one of the first and the second of the at least three aircraft engagement members to engage the corresponding one of the set of anchors that is spaced longitudinally in a fore or aft direction from at least one of the corresponding ones of the set of anchors to which the first and the second aircraft engagement members releasably couple.
4. The capture-and-release aircraft according to claim 3 , wherein each of the aircraft engagement members comprises a proximity sensor for detecting an engageable position of the corresponding one of the set of anchors of the fixed-wing aircraft.
5. The capture-and-release aircraft according to claim 3 , wherein the capture-and-release aircraft further comprises a cargo, battery, fuel cell, and/or passenger hold secured to the frame, and wherein each of the aircraft engagement members further comprises at least one motor that, when the anchor-capture devices are coupled to the anchors of the fixed-wing aircraft, can move the cargo, battery, fuel cell, and/or passenger hold between a first position in which the cargo, battery, fuel cell and/or passenger hold is spaced from the fixed-wing aircraft and a second position in which the cargo, battery, fuel cell, and/or passenger hold is adjacent or within the fixed-wing aircraft.
6. The capture-and-release aircraft according to claim 3 , wherein each of the anchor-capture devices comprises an anchor receptacle in which one of the anchors is received.
7. The capture-and-release aircraft according to claim 3 , wherein each of the aircraft engagement members further comprises at least one sensor for detecting an alignment of the anchor-capture device coupled to the articulating arm of the aircraft engagement member with the corresponding one of the set of anchors of the fixed-wing aircraft, and wherein the capture-and-release aircraft further comprises a guidance system coupled to the each of the articulating arm and the at least one sensor to align the anchor-capture device with the corresponding one of the set of anchors.
8. The capture-and-release aircraft according to claim 7 , wherein each of the anchor-capture devices comprises an anchor receptacle in which one of the anchors is received.
9. The capture-and-release aircraft according to claim 8 , wherein the at least one sensor comprises at least one optical sensor positioned on an inner surface of the anchor receptacle.
10. The capture-and-release aircraft according to claim 8 , wherein the at least one sensor comprises at least one optical sensor positioned on an outer surface of the anchor receptacle.
11. The capture-and-release aircraft according to claim 7 , wherein the at least one sensor comprises at least one optical sensor.
12. The capture-and-release aircraft according to claim 11 , wherein the at least one optical sensor is positioned on the anchor-capture device.
13. The capture-and-release aircraft according to claim 11 , wherein the guidance system processes data from the at least one sensor to detect an optical pattern one of on or adjacent to the corresponding one of the set of anchors to facilitate detection of the alignment of the anchor-capture devices with the anchors of the fixed-wing aircraft.
14. The capture-and-release aircraft according to claim 13 , wherein the optical pattern comprises a light-emitting beacon.
15. The capture-and-release aircraft according to claim 13 , wherein the optical pattern comprises a pattern of demarcations on a surface of the anchors of the fixed-wing aircraft.
16. The capture-and-release aircraft according to claim 13 , wherein the optical pattern comprises a pattern of demarcations on a surface of the fixed-wing aircraft adjacent the anchors of the fixed-wing aircraft.