Systems and methods for establishing a flight pattern adjacent to a target for a vehicle to follow

Patent metadata

Field	Value
Publication number	US-10096251-B2
Application number	US-201615381342-A
Country	US
Kind code	B2
Filing date	Dec 16, 2016
Priority date	Dec 16, 2016
Publication date	Oct 9, 2018
Grant date	Oct 9, 2018

Abstract

An example method of establishing a flight pattern adjacent to a target for an aerial vehicle to follow includes determining a stand-off distance to the target. The stand-off distance indicates a distance from the target at a point along the flight pattern. The example method also includes generating the flight pattern in a form of a conchoidal transformation of a lemniscate based on the stand-off distance.

First claim

What is claimed is:

1. A method of establishing a flight pattern adjacent to a target for an aerial vehicle to follow, comprising:
determining a stand-off distance to the target, wherein the stand-off distance indicates a distance from the target at a point along the flight pattern; and
generating the flight pattern in a form of a conchoidal transformation of a lemniscate based on the stand-off distance.

2. The method of claim 1 , wherein the lemniscate comprises a lemniscate of Bernouilli or a lemniscate of Gerono.

3. The method of claim 1 , wherein generating the flight pattern in the form of the conchoidal transformation of the lemniscate based on the stand-off distance comprises:
generating the flight pattern to resemble a flattened figure-eight pattern.

4. The method of claim 1 , further comprising:
determining an angle of coverage for the flight pattern around the target; and
generating the flight pattern in the form of the conchoidal transformation of the lemniscate based also on the angle of coverage.

5. The method of claim 4 , wherein generating the flight pattern in the form of the conchoidal transformation of the lemniscate based also on the angle of coverage comprises:
determining a size of lobes of the lemniscate.

6. The method of claim 1 , further comprising:
determining an orientation of the flight pattern relative to the target; and
generating the flight pattern in the form of the conchoidal transformation of the lemniscate based also on the orientation.

7. The method of claim 6 , wherein determining the orientation of the flight pattern relative to the target comprises:
determining an up-sun position of the flight pattern relative to the target.

8. The method of claim 6 , wherein determining the orientation of the flight pattern relative to the target comprises:
determining an up-wind position of the flight pattern relative to the target.

9. The method of claim 6 , wherein determining the orientation of the flight pattern relative to the target comprises:
determining a down-wind position of the flight pattern relative to the target.

10. The method of claim 1 , further comprising:
designating an area proximate to the target as a no-fly zone; and
generating the flight pattern in the form of the conchoidal transformation of the lemniscate based also on avoiding entering the designated no-fly zone.

11. The method of claim 1 , further comprising:
sending, by a computing device, instructions to the aerial vehicle indicating to fly the generated flight pattern so as to follow a path enabling continuous coverage of the target from a nose mounted sensor on the aerial vehicle.

12. The method of claim 1 , further comprising:
receiving, at an input interface, a change to the stand-off distance; and
modifying the generated flight pattern in real time based on the change to the stand-off distance.

13. The method of claim 1 , further comprising:
predicting performance of the aerial vehicle along the generated flight pattern based on a kinematic model of the aerial vehicle and wind conditions; and
modifying the generated flight pattern based on the predicted performance of the aerial vehicle.

14. The method of claim 1 , further comprising:
predicting a noise output of the aerial vehicle while flying along the generated flight pattern; and
modifying the generated flight pattern based on the predicted noise output of the aerial vehicle.

15. The method of claim 1 , further comprising:
predicting performance of the aerial vehicle along the generated flight pattern based on a kinematic model of the aerial vehicle; and
modifying the generated flight pattern based on the predicted performance of the aerial vehicle to optimize performance of payload of the aerial vehicle.

16. The method of claim 1 , wherein the method is performed by a computing device having one or more processors, and the method further comprises:
virtually positioning the lemniscate relative to the target based on the stand-off distance; and
conchoidally transforming the lemniscate.

17. A non-transitory computer readable storage medium having stored therein instructions, that when executed by a system having one or more processors, causes the system to perform functions of establishing a flight pattern adjacent to a target for an aerial vehicle to follow, the functions comprising:
determining a stand-off distance to the target, wherein the stand-off distance indicates a distance from the target at a point along the flight pattern; and
generating the flight pattern in a form of a conchoidal transformation of a lemniscate based on the stand-off distance.

18. The non-transitory computer readable medium of claim 17 , wherein the functions further comprise:
determining an angle of coverage for the flight pattern around the target;
determining an orientation of the flight pattern relative to the target; and
generating the flight pattern in the form of the conchoidal transformation of the lemniscate based also on the angle of coverage and the orientation of the flight pattern relative to the target.

19. A computing device comprising:
a communication interface for receiving a stand-off distance to a target, wherein the stand-off distance indicates a distance from the target at a point along a flight pattern adjacent to the target for an aerial vehicle to follow; and
one or more processors for executing instructions stored on data storage to generate the flight pattern in a form of a conchoidal transformation of a lemniscate based on the stand-off distance.

20. The computing device of claim 19 , further comprising:
an output interface for sending instructions to the aerial vehicle indicating to fly the generated flight pattern so as to follow a path enabling continuous coverage of the target from a nose mounted sensor on the aerial vehicle.

Assignees

• Insitu Inc A Subsidiary Of The Boeing Company
• Insitu Inc

Inventors

• Rysdyk Rolf

Classifications

• B64U2201/20

  Remote controls · CPC title

• B64U2101/30

  for imaging, photography or videography · CPC title

• G05D1/0011

  associated with a remote control arrangement · CPC title

• G08G5/006

  Physics · mapped topic

• G05D1/101 Primary

  specially adapted for aircraft · CPC title