Enhanced Accuracy for Tracking Tethered Airborne Vehicles

Patent metadata

Field	Value
Publication number	US-2016005159-A1
Application number	US-201414325187-A
Country	US
Kind code	A1
Filing date	Jul 7, 2014
Priority date	Jul 7, 2014
Publication date	Jan 7, 2016
Grant date	—

Abstract

Wind energy systems, such as an Airborne Wind Turbine (“AWT”), may be used to facilitate conversion of kinetic energy to electrical energy. An AWT may include an aerial vehicle that flies in a path to convert kinetic wind energy to electrical energy. The aerial vehicle may be tethered to a ground station with a tether that terminates at a tether termination mount system. In one aspect, the tether termination mount system may include a tether termination unit configured in one or more gimbals that allow for the tether termination unit to rotate about one or more axes while tracking the aerial vehicle in flight. In a further aspect, the tether termination mount system may include an imaging device configured for imaging the aerial vehicle during flight in order to enhance tracking accuracy over that which is performed by angular motion of the tether termination unit.

First claim

We claim:

1 . An apparatus comprising:
a tether termination mount system comprising a tether termination unit configured for rotation about a first axis of rotation and a second axis of rotation, the first and second axes of rotation being oriented at an angle to one another; a tether configured for coupling an aerial vehicle to the tether termination mount system, the tether having a proximal end emanating from the tether termination unit along a pointing axis of the tether termination unit and distal end attached to the aerial vehicle, wherein the pointing axis is configured for tracking angular motion of the proximal end of the tether induced by flight motion of the aerial vehicle; an imaging device attached to the tether termination unit and having an image plane oriented at a fixed angle with respect to the pointing axis, and a reference point in the image plane corresponding to the pointing axis direction in a field-of-view (FOV) of the image plane; and a vehicle tracking subsystem configured for tracking a location of the aerial vehicle with respect to the tether termination mount system during tethered flight of the aerial vehicle by (i) determining the pointing axis direction as a function of measured rotation angles of the tether termination unit about the first and second axes of rotation, (ii) determining an angular offset between an image of the aerial vehicle in the image plane and the reference point in the image plane, and (iii) applying the determined angular offset as a correction to the determined pointing axis direction.

2 . The apparatus of claim 1 , wherein the fixed angle is a right angle, whereby the image plane is oriented perpendicularly to the pointing axis.

3 . The apparatus of claim 1 , wherein the imaging device comprises a device selected from one of a digital camera and a line-scan camera synchronized to a pattern of blinking lights on the aerial vehicle.

4 . The apparatus of claim 1 , wherein the image of the aerial vehicle in the image plane is at least one of an optical image of a physical form of the aerial vehicle, an optical image of a pattern painted on the aerial vehicle, an optical image of a pattern of lights emitted from the aerial vehicle, or a signal reflected from a surface pattern on the aerial vehicle.

5 . The apparatus of claim 1 , wherein the vehicle tracking subsystem is further configured for tracking the location of the aerial vehicle with respect to the tether termination mount system during tethered flight of the aerial vehicle by measuring the line-of-sight distance to the aerial vehicle during tethered flight of the aerial vehicle.

6 . The apparatus of claim 1 , further comprising a distance ranging device configured for measuring a line-of-sight distance to the aerial vehicle,
and wherein the vehicle tracking subsystem is further configured for tracking the location of the aerial vehicle with respect to the tether termination mount system during tethered flight of the aerial vehicle by measuring the line-of-sight distance to the aerial vehicle during tethered flight of the aerial vehicle with the distance ranging device.

7 . The apparatus of claim 6 , wherein the distance ranging device is one of a LIDAR device or a RADAR device.

8 . The apparatus of claim 6 , wherein the imaging device and the distance ranging device are configured as integral components of a single distance-imaging device.

9 . The apparatus of claim 1 , wherein the first axis of rotation is incorporated in a first gimbal device, and the second axis of rotation is incorporated in a second gimbal device,
wherein the first gimbal device comprises a first encoder configured for measuring a rotation angle of the tether termination unit about the first axis of rotation, and wherein the second gimbal device comprises a second encoder configured for measuring a rotation angle of the tether termination unit about the second axis of rotation.

10 . The apparatus of claim 1 , wherein the first axis of rotation is orthogonal to the second axis of rotation.

11 . The apparatus of claim 1 , wherein the pointing axis is configured for tracking angular motion of the proximal end of the tether due to rotation of the tether termination unit about the first and second axes of rotation.

12 . The apparatus of claim 1 , wherein the tether termination unit comprises a spindle through which the tether is physically routed between the tether termination mount system and the aerial vehicle.

13 . The apparatus of claim 1 , wherein the reference point is at the center of the image plane, and further corresponds to the center of the FOV.

14 . The apparatus of claim 1 , wherein tracking the angular motion of the proximal end of the tether induced by flight motion of the aerial vehicle comprises tracking the aerial vehicle during flight with sufficient accuracy to locate the aerial vehicle within the FOV of the image plane.

15 . The apparatus of claim 1 , wherein the image plane is configured for rotation about the pointing axis direction in response to a twisting motion of the proximal end of the tether about the pointing axis.

16 . A method comprising:
determining a pointing direction of a pointing axis of a tether termination unit as a function of measured rotation angles of the tether termination unit about a first axis of rotation and a second axis of rotation, wherein the tether termination unit is configured for terminating a proximal end of a tether that is coupled at a distal end with an aerial vehicle, and wherein the pointing axis is configured for tracking angular motion of the proximal end of the tether induced by flight motion of the aerial vehicle; determining an angular offset between an image of the aerial vehicle in flight in an image plane of an imaging device attached to the tether termination unit and a reference point in the image plane, wherein the image plane is configured at a fixed angle with respect to the pointing axis, and the reference point corresponds to the pointing axis direction in a field-of-view (FOV) of the image plane; and determining a location of the aerial vehicle in flight with respect to the tether termination unit by applying the determined angular offset as a correction to the determined pointing axis direction.

17 . The method of claim 16 , wherein the fixed angle is a right angle, whereby the image plane is oriented perpendicularly to the pointing axis.

18 . The method of claim 16 , wherein the image of the aerial vehicle in the image plane is at least one of an optical image of a physical form of the aerial vehicle, an optical image of a pattern painted on the aerial vehicle, an optical image of a pattern of lights emitted from the aerial vehicle, or a signal reflected from a surface pattern on the aerial vehicle.

19 . The method of claim 16 , further comprising measuring a line-of-sight distance to the aerial vehicle during tethered flight of the aerial vehicle.

20 . The method of claim 19 , wherein the tether termination unit is a component of an apparatus that further comprises a distance ranging device select from one of a LIDAR device and a RADAR device,
and wherein measuring the line-of-sight distance to the aerial vehicle during tethered flight of the aerial vehicle comprises measuring the line-of-sight distance to the aerial vehicle during tethered flight of the aerial vehicle with the distance ranging device.

21 . The method of claim 16 , wherein the first axis of rotation is incorporated in a first gimbal

Assignees

• Google Inc

Inventors

• Hallamask Kurt
• Hachtmann Brian
• Nelson Rob
• Hardham Corwin
• Jensen Kenny
• Patten Elias Wolfgang

Classifications

• B64F1/02

  for arresting aircraft, e.g. nets or cables · CPC title

• G06T7/004 Primary

  Physics · mapped topic

• B64U2101/10

  for generating power to be supplied to a remote station, e.g. UAVs with solar panels · CPC title

• B64U2201/202

  using tethers for connecting to ground station · CPC title

• B64U10/60

  Tethered aircraft · CPC title