Mutually exclusive three dimensional flying spaces

Patent metadata

Field	Value
Publication number	US-12340705-B2
Application number	US-202318314017-A
Country	US
Kind code	B2
Filing date	May 8, 2023
Priority date	Aug 23, 2018
Publication date	Jun 24, 2025
Grant date	Jun 24, 2025

Abstract

Boundary information for a three-dimensional (3D) flying space is obtained. An input associated with steering a vehicle is received from an input device and location information associated with the vehicle is received from a location sensor. A control signal for the vehicle is generated based at least in part on the boundary information, the input, and the location information. In the event the input would cause the vehicle to cross the boundary of the 3D flying space if obeyed, the control signal for the vehicle is generated so that the vehicle is prevented from crossing the boundary of the 3D flying space. In response to receiving an indication associated with the vehicle landing, the boundary information is modified so that the 3D flying space includes a landing pathway.

First claim

What is claimed is:

1. A system, comprising:
a memory;
an input device;
a location sensor; and
a flight computer which is configured to:
obtain boundary information associated with a three-dimensional (3D) flying space from the memory, comprising to:
send a request to a 3D flying space assignor;
receive, from the 3D flying space assignor, an assignment which includes a selection from a plurality of predefined 3D flying spaces with predefined boundary information which are already stored on the aircraft; and
store information from the assignment, including by storing the selection;

receive an input associated with flying an aircraft from the input device;
receive location information associated with the aircraft from the location sensor; and
generate a control signal for the aircraft based at least in part on the boundary information, the input, and the location information, wherein the control signal is responsive to the input in a manner that would not cause the aircraft to cross a boundary associated with the 3D flying space, wherein the generating of the control signal for the aircraft comprises to:
receive a first indication prior to a switch from a landed state of the aircraft to an airborne state of the aircraft;
in response to receiving the first indication, temporarily modify the boundary information associated with the 3D flying space in order to produce modified boundary information associated with a modified 3D flying space, wherein the modified 3D flying space includes a range of permitted altitudes excluded from the 3D flying space and the aircraft switches between the landed state and the airborne state including by passing through the range of permitted altitudes;

receive a second indication after the switch from the landed state of the aircraft to the airborne state of the aircraft; and
in response to receiving the second indication, return the modified boundary information to the boundary information such that the modified 3D flying space returns to the 3D flying space.

2. The system recited in claim 1 , wherein the 3D flying space has one or more of the following cross sections: a circular cross section, an elliptical cross section, or a rectangular cross section.

3. The system recited in claim 1 , wherein:
the 3D flying space includes an entrance and an exit; and
a length of the 3D flying space, measured from the entrance to the exit, is larger than a height or a width of a cross-sectional area associated with the 3D flying space.

4. The system recited in claim 1 , wherein the boundary information associated with the 3D flying space includes a range of permitted altitudes and a perimeter.

5. The system recited in claim 1 , wherein obtaining the boundary information associated with the 3D flying space includes:
receiving, from the 3D flying space assignor, the assignment which includes the boundary information associated with the 3D flying space; and
storing information from the assignment, including by storing the boundary information associated with the 3D flying space.

6. The system recited in claim 1 , wherein obtaining the boundary information associated with the 3D flying space includes:
listening on a wireless channel to receive zero or more communications from zero or more other aircraft;
determining any already-claimed 3D flying spaces using any received communications; and
claiming the 3D flying space, including by transmitting on the wireless channel.

7. The system recited in claim 1 , wherein obtaining the boundary information associated with the 3D flying space includes:
listening on a wireless channel to receive zero or more communications from zero or more other aircraft;
determining any already-claimed 3D flying spaces using any received communications, wherein there is a plurality of predefined 3D flying spaces with predefined boundary information which are already stored on the aircraft and any received communications include an identification of any already-claimed predefined 3D flying spaces; and
claiming the 3D flying space, including by transmitting on the wireless channel, wherein the transmission on the wireless channel includes an identification of the claimed 3D flying space.

8. The system recited in claim 1 , wherein obtaining the boundary information associated with the 3D flying space includes:
listening on a wireless channel to receive zero or more communications from zero or more other aircraft;
determining any already-claimed 3D flying spaces using any received communications, including by querying any other aircraft from which any communication is received; and
claiming the 3D flying space, including by transmitting on the wireless channel, wherein the transmission on the wireless channel includes an identification of the aircraft.

9. The system recited in claim 1 , wherein the boundary information associated with the 3D flying space is modified in response to identification of a potential collision between a moving object and the aircraft using publically-available location information associated with the moving object.

10. The system recited in claim 1 , wherein:
the boundary information associated with the 3D flying space is modified in response to identification of a potential collision between a moving object and the aircraft using publically-available location information associated with the moving object;
the moving object includes a ship; and
the publically-available location information associated with the moving object is associated with Automatic Identification System (AIS) information.

11. A method, comprising:
obtaining boundary information associated with a three-dimensional (3D) flying space, comprising:
sending a request to a 3D flying space assignor;
receiving, from the 3D flying space assignor, an assignment which includes a selection from a plurality of predefined 3D flying spaces with predefined boundary information which are already stored on the aircraft; and
storing information from the assignment, including by storing the selection;

receiving an input associated with flying an aircraft from an input device;
receiving location information associated with the aircraft from a location sensor; and
generating a control signal for the aircraft based at least in part on the boundary information, the input, and the location information, wherein the control signal is responsive to the input in a manner that would not cause the aircraft to cross a boundary associated with the 3D flying space, wherein the generating of the control signal for the aircraft comprises:
receiving a first indication prior to a switch from a landed state of the aircraft to an airborne state of the aircraft;
in response to receiving the first indication, temporarily modifying the boundary information associated with the 3D flying space in order to produce modified boundary information associated with a modified 3D flying space, wherein the modified 3D flying space includes a range of permitted altitudes excluded from the 3D flying space and the aircraft switches between the landed state and the airborne state including by passing through the range of permitted altitudes;
receiving a second indication after the switch from the landed state of the aircraft to the airborne state of the aircraft; and
in response to receiving the second indication, returning the modified boundary information to the boundary information such that the modified 3D flying space returns to the 3D flying space.

12. The method recited in claim 11 , wherein obtaining the boundary information associated with the 3D flying space includes:
listening on a wireless channel to receive zero or more communicatio

Assignees

• Kitty Hawk Corp

Inventors

• Robertson Cameron
• Roetter Alex

Classifications

• G05D1/2245

  providing the operator with a purely computer-generated representation of the environment of the vehicle, e.g. virtual reality · CPC title

• G08G5/80

  Anti-collision systems · CPC title

• G08G5/59

  in accordance with predefined flight zones, e.g. to avoid prohibited zones · CPC title

• G06Q40/06

  Asset management; Financial planning or analysis · CPC title

• G06F16/248

  Presentation of query results · CPC title