Maintaining a stable phase difference between multiple tethered vehicles lifting a payload

Patent metadata

Field	Value
Publication number	US-2020387178-A1
Application number	US-202017001411-A
Country	US
Kind code	A1
Filing date	Aug 24, 2020
Priority date	Jul 27, 2016
Publication date	Dec 10, 2020
Grant date	—

Abstract

A system to maintain a phase difference is disclosed. Two or more aircraft fly in a continuous periodic trajectory. The system maintains a phase difference between the two or more aircraft. Telemetry information for a reference aircraft moving in a first periodic trajectory is received. A phase difference between a primary aircraft and the reference aircraft with respect to the first periodic trajectory is determined. A variance in the phase difference between the primary aircraft and the reference aircraft from the target phase difference is determined. A new trajectory for the primary aircraft that decreases the variance in the phase difference with respect to the new periodic trajectory is determined, and the primary aircraft is maneuvered to follow the new trajectory.

First claim

What is claimed is:

1 . A system, comprising:
an interface configured to receive telemetry information for a reference aircraft moving in a first periodic trajectory; and a processor configured to:
determine a phase difference between a primary aircraft and the reference aircraft with respect to the first periodic trajectory, wherein the primary aircraft and the reference aircraft are tethered to a common payload;
determine a load adjustment based at least in part on lift associated with the primary aircraft;
determine a new trajectory for the primary aircraft that implements the load adjustment; and
cause at least one of the primary aircraft or the reference aircraft to move in the new trajectory.

2 . The system of claim 1 , wherein the lift associated with the primary aircraft is the lift experienced by the primary aircraft.

3 . The system of claim 1 , wherein the processor is further configured to determine the lift associated with the primary aircraft.

4 . The system of claim 1 , wherein determining the load adjustment includes:
comparing the lift associated with the primary aircraft with a lift associated with the reference aircraft; and determining a non-zero load adjustment in response to the lift associated with the primary aircraft being equal to the lift associated with the reference aircraft.

5 . The system of claim 1 , wherein determining the load adjustment includes:
comparing the lift associated with the primary aircraft with a lift associated with the reference aircraft; increasing a load value associated with the primary aircraft in response to the lift associated with the primary aircraft being greater than the lift associated with the reference aircraft; and determining the load adjustment based on the increased load value.

6 . The system of claim 1 , wherein the load adjustment improves lift capacity of the primary aircraft and the reference aircraft

7 . The system of claim 1 , wherein the primary aircraft is upwind of the reference aircraft, and the processor is further configured to increase the load on the upwind aircraft to increase a proportion of load experienced by the upwind aircraft.

8 . The system of claim 1 , wherein the lift associated with the primary aircraft is due at least in part to wind effects.

9 . The system of claim 8 , wherein the wind effects are determined from received wind information including by determining whether the primary aircraft is upwind or downwind of the reference aircraft based on the wind information.

10 . The system of claim 1 , wherein the processor is configured to determine the primary aircraft to be ahead of or behind a target position based on a variance in phase difference.

11 . The system of claim 10 , wherein in the event that the primary aircraft is determined to be behind a target position based on the variance in phase difference, the processor is configured to compute the new trajectory such that the primary aircraft moves towards a center of the first periodic trajectory.

12 . The system of claim 10 , wherein in the event that the primary aircraft is determined to be ahead of a target position based on the variance in phase difference, the processor is configured to compute the new trajectory such that the primary aircraft moves away from a center of the first periodic trajectory.

13 . The system of claim 1 , wherein the phase difference is determined based at least in part on one or more of the following: a sensor data, a visual data, and a location data.

14 . The system of claim 1 , wherein the primary aircraft comprises one or more of the following: a global positioning system, a ground reference sensor, a line angle sensor, and a camera.

15 . The system of claim 1 , wherein the new trajectory is a translation of the first periodic trajectory.

16 . The system of claim 1 , wherein the reference aircraft is upwind of the primary aircraft, and the processor is further configured to instruct the reference aircraft to fly closer to a vertical of a payload to bear a greater load compared with the primary aircraft to cause a battery of the primary aircraft to be preserved.

17 . The system of claim 1 , wherein the interface and the processor are provided in the primary aircraft, and the interface and the processor are in communication with the reference aircraft.

18 . The system of claim 1 , wherein the primary aircraft and the reference aircraft are configured to lift a payload via at least one tether.

19 . A method, comprising:
receiving telemetry information for a reference aircraft moving in a first periodic trajectory; determining a phase difference between a primary aircraft and the reference aircraft with respect to the first periodic trajectory, wherein the primary aircraft and the reference aircraft are tethered to a common payload; determining a load adjustment based at least in part on lift associated with the primary aircraft; determining a new trajectory for the primary aircraft that implements the load adjustment; and causing at least one of the primary aircraft or the reference aircraft to move in the new trajectory.

20 . A computer program product for maintaining a target phase difference, the computer program product being embodied in a non-transitory computer readable storage medium and comprising computer instructions for:
receiving telemetry information for a reference aircraft moving in a first periodic trajectory; determining a phase difference between a primary aircraft and the reference aircraft with respect to the first periodic trajectory, wherein the primary aircraft and the reference aircraft are tethered to a common payload; determining a load adjustment based at least in part on lift associated with the primary aircraft; determining a new trajectory for the primary aircraft that implements the load adjustment; and causing at least one of the primary aircraft or the reference aircraft to move in the new trajectory.

Assignees

• Kitty Hawk Corp

Inventors

• Vander Lind Damon
• Horn Gregory Mainland

Classifications

• B64U2201/20

  Remote controls · CPC title

• B64U2201/102

  adapted for flying in formations · CPC title

• B64U2201/104

  using satellite radio beacon positioning systems, e.g. GPS · CPC title

• B64U2101/30

  for imaging, photography or videography · CPC title

• B64U10/60

  Tethered aircraft · CPC title