Supplementing energy storage of an in-flight solar-powered UAV by casting light from a secondary in-flight UAV

Patent metadata

Field	Value
Publication number	US-10476296-B1
Application number	US-201715637214-A
Country	US
Kind code	B1
Filing date	Jun 29, 2017
Priority date	Jun 29, 2017
Publication date	Nov 12, 2019
Grant date	Nov 12, 2019

Abstract

A secondary UAV flies over the solar-powered UAV at night and illuminates the solar-powered UAV's solar panels to help supplement the solar-powered UAV's battery charge mid-flight. The secondary UAV could be equipped with a directional light source for providing light of a color and intensity selected for optimal absorption by the solar cells of the solar-powered UAV. As the secondary UAV flies over the solar-powered UAV, the secondary UAV could thus direct its light source at the solar-powered UAV for absorption by the solar cells, to help supplement the solar-powered UAV's battery charge. Further, the secondary UAV could potentially recharge multiple solar-powered UAVs during a single nighttime mission.

First claim

We claim:

1. A method of charging an energy-storage device of a first unmanned aerial vehicle (UAV) while the first UAV is in flight, wherein the first UAV is equipped with solar cells that convert light into electricity for charging the energy-storage device, the method comprising:
flying a second UAV in proximity to the first UAV while the first UAV is in flight, wherein the second UAV is equipped with a directional light source; and
while the second UAV is flying in proximity to the first UAV in flight, using the directional light source to cast light onto the solar cells of the first UAV to help charge the energy-storage device of the first UAV.

2. The method of claim 1 , wherein the light is incoherent.

3. The method of claim 2 , wherein the energy-storage device comprises a battery.

4. The method of claim 2 , wherein the directional light source comprises a bank of multiple lamps.

5. The method of claim 2 , wherein the first UAV is a High Altitude Pseudo-Satellite (HAPS) platform.

6. The method of claim 2 , wherein the first UAV is selected from the group consisting of a balloon system and a drone.

7. The method of claim 2 , wherein flying the second UAV in proximity to the first UAV while the first UAV is in flight comprises flying the second UAV above the first UAV while the first UAV is in flight.

8. The method of claim 2 , wherein the directional light source is mounted to the second UAV with at least one controllable multi-axial mount, and wherein using the directional light source to cast light onto the solar cells of the first UAV comprises controlling the at least one controllable multi-axial mount to direct light from directional light source toward the solar cells of the first UAV.

9. The method of claim 2 ,
wherein flying the second UAV in proximity to the first UAV while the first UAV is in flight comprises using satellite-based positioning to determine a location of the first UAV and flying the second UAV in proximity to the determined location of the first UAV, and
wherein using the directional light source to cast light onto the solar cells of the first UAV while the first UAV is in flight comprises computing a beam direction from the second UAV to the first UAV and pointing the directional light source in the computed beam direction.

10. The method of claim 9 , further comprising, as the second UAV flies and the first UAV flies:
updating the beam direction from the second UAV to the first UAV; and
adjusting the directional light source to point in the updated beam direction.

11. The method of claim 2 , further comprising:
detecting when charge of the energy-storage device increases to a threshold level; and
responsive to the detecting, (i) flying the second UAV from being in proximity to the first UAV in flight to being in proximity to a third UAV in flight and (ii) while the second UAV is flying in proximity to the third UAV in flight, using the directional light source to cast light onto solar cells of the third UAV for conversion of the light by the solar cells of the third UAV into electricity for charging an energy-storage device of the third UAV.

12. The method of claim 11 , further comprising operating a ground-based control center in communication with at least the first UAV and the second UAV,
wherein the ground-based control center controls flying of the second UAV, and
wherein detecting when the charge of the energy-storage device increases to the threshold level comprises receiving by the ground-based control center from the first UAV a report indicating that charge of the energy-storage device has increased to the threshold level.

13. The method of claim 2 , carried out in the stratosphere at night.

14. A method of charging a battery of a first aircraft in flight at night, wherein the first aircraft is equipped with solar cells that convert light into electricity for charging the battery, the method comprising:
flying a second aircraft in proximity to the first aircraft when the first aircraft is in flight at night; and
while flying the second aircraft in proximity to the first aircraft when the first aircraft is in flight at night, (i) shining an incoherent light from the second aircraft onto the solar cells of the first aircraft for conversion of the incoherent light by the solar cells into electricity for charging the battery and (ii) tracking a position of the first aircraft in relation to a position of the second aircraft and, based on the tracking, dynamically adjusting direction of the incoherent light to continue to shine the incoherent light onto the solar cells of the first aircraft for conversion of the incoherent light by the solar cells into electricity for charging the battery.

15. A system for charging a battery of a first unmanned aerial vehicle (UAV) while the first UAV is in flight, wherein the first UAV is equipped with solar cells that convert light into electricity for charging the battery, the system comprising:
a second UAV equipped with a directional light source; and
a controller configured (i) to cause the second UAV to fly in proximity to the first UAV while the first UAV is in flight and (ii) while the second UAV is flying in proximity to the first UAV in flight, to cause the directional light source to cast incoherent light onto the first UAV for conversion of the light by the solar cells into electricity for charging the battery.

16. The system of claim 15 , wherein the controller comprises a ground-based control center in communication with the second UAV, and wherein the ground-based control center commands the second UAV to fly in a flight-pattern proximate to the first UAV and to cast the incoherent light onto the first UAV.

17. The system of claim 15 , wherein the directional light source comprises a bank of multiple lamps mounted to an underside of the second UAV by at least one controllable multi-axial mount.

18. The system of claim 15 , wherein the controller is configured to cause the second UAV to fly above the first UAV at a safe distance from the first UAV, the distance being short enough to allow the incoherent light from the second UAV to reach the solar cells of the first UAV for charging the battery.

19. The system of claim 15 , wherein the controller is configured to track a flight position of the first UAV in relation to a flight position of the second UAV and, based on the tracking, to dynamically redirect the directional light source to continue to cast incoherent light onto the first UAV in flight for conversion of the light by the solar cells into electricity for charging the battery.

20. The system of claim 15 , wherein the controller is configured to detect when charge of the battery increases to a threshold level and, in response to the detecting, to cause the directional light source to discontinue casting the incoherent light onto the first UAV.

Assignees

• Sprint Spectrum Lp

Inventors

• Rausch Walter F
• Ottendorfer Guenther

Classifications

• H02S20/30

  Supporting structures being movable or adjustable, e.g. for angle adjustment · CPC title

• B64U2201/102

  adapted for flying in formations · CPC title

• H02J50/30 Primary

  using light, e.g. lasers · CPC title

• H02J7/35

  with light sensitive cells · CPC title

• H02S40/38

  Energy storage means, e.g. batteries, structurally associated with PV modules · CPC title