AUTONOMOUS AIRCRAFT GUIDING MOBILE UNIT

• US 20140249736A1
• Filed: 03/04/2013
• Published: 09/04/2014
• Est. Priority Date: 03/04/2013
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Beda, Tomas, Koukol, Ondrej, Marczi, Tomas
• Application Number:
  US13/783,611
• Publication Number:
  US 20140249736A1
• Time in Patent Office: Days
• US Class Current: 701/120
• CPC Class Codes: G05D 1/0083 to help an aircraft pilot in the rolling phase
• CPC Class Codes: G05D 1/0274 using mapping information stored in a memory device navigation using map-matching G01C21/30
• CPC Class Codes: G05D 1/0278 using satellite positioning signals, e.g. GPS
• CPC Class Codes: G05D 1/0297 by controlling means in a control room
• CPC Class Codes: G08G 5/065 Navigation or guidance aids, e.g. for taxiing or rolling

Abstract

Embodiments of the subject application provide methods and systems for an autonomous aircraft guiding mobile unit (GMU). The GMU includes one or more light modules, one or more processing units, and one or more data storage mediums. The one or more data storage mediums include instructions which, when executed by the one or more processing units, cause the one or more processing units to receive control messages from a traffic control ground station (TCGS), the control messages assigning the GMU to an aircraft and controlling movement of the GMU and its assigned aircraft, and to provide light commands to a pilot of the assigned aircraft with the one or more light modules, the light commands directing movement of the assigned aircraft during taxiing.

Claims

1. An autonomous aircraft guiding mobile unit (GMU) comprising:

one or more light modules;

one or more processing units; and

one or more data storage mediums, the one or more data storage mediums including instructions which, when executed by the one or more processing units, cause the one or more processing units to;

receive control messages from a traffic control ground station (TCGS), the control messages assigning the GMU to an aircraft and controlling movement of the GMU and its assigned aircraft; and

provide light commands to a pilot of the assigned aircraft with the one or more light modules, the light commands directing movement of the assigned aircraft during taxiing.

2. The GMU of claim 1, wherein the light commands provided to the pilot include commands of:

follow-me, stop, turn right, and turn left.

3. The GMU of claim 1, comprising:

an engine for moving the GMU about an airport; and

a heading control system to control a direction of motion for the GMU;

wherein the instructions cause the one or more processing units to control the engine and the heading control system based on the control messages from the TCGS to guide the assigned aircraft.

4. The GMU of claim 3, wherein the engine comprises one of an internal combustion engine or an electric motor.

5. The GMU of claim 1, comprising:

a location unit to determine a location of the GMU;

a heading unit to determine a heading of the GMU;

wherein the instructions cause the one or more processing units to obtain the location and heading of the GMU from the location unit and the heading unit and provide indications of the location and heading to the TCGS.

6. The GMU of claim 1, wherein communication between the TCGS and the GMU occurs over a ground control datalink.

7. The GMU of claim 1, wherein the TCGS determines a route on airport taxiways for the GMU, wherein the control messages direct the GMU assigned to an aircraft in accordance with the route;

and

wherein the GMU includes an airport database indicating a location of the airport taxiways, wherein the instructions cause the one or more processing units to control the engine and the heading control system to drive the GMU over the airport taxiways in accordance with the route.

8. The GMU of claim 1, comprising:

an aircraft distance measuring unit configured to measure a distance between the GMU and its assigned aircraft, wherein the instructions cause the one or more processing units to maintain the distance between the GMU and its assigned aircraft within a defined range.

9. The GMU of claim 8, wherein the instructions cause the one or more processing units to send an indication of a location of the assigned aircraft to the TCGS.

10. The GMU of claim 1, wherein the instructions cause the one or more processing units to verify whether an aircraft is the assigned aircraft by receiving a broadcast identification beacon from the aircraft and comparing identification information in the broadcast identification beacon with identification information of the assigned aircraft.

11. The GMU of claim 10, wherein the instructions cause the one or more processing units to, in response to verifying that the aircraft is the assigned aircraft, commence the providing light commands to the pilot.

12. The GMU of claim 1, comprising:

one or more infrared (IR) emitter modules, wherein the instructions cause the one or more processing units to provide IR commands to a pilot of the assigned aircraft with the one or more IR emitter modules, the IR commands providing the same directives as the light commands provided to the pilot, such that the pilot can receive the directives in low visibility conditions when the light commands are not easily visible.

13. A method for guiding an aircraft with an autonomous guiding mobile unit (GMU), the method comprising:

receiving control messages including information regarding assigned aircraft and aircraft pick-up location from a traffic control ground station (TCGS);

controlling, with one or more processing units, an engine and a heading control system of the GMU to driving to the aircraft pick-up location;

verifying, with the one or more processing units, whether an aircraft in proximity of the aircraft pick-up location is the assigned aircraft;

determining, with the one or more processing units, light commands to provide to the assigned aircraft based on the control messages from the TCGS; and

providing the light commands to the assigned aircraft to guide the assigned aircraft during taxiing.

14. The method of claim 13, comprising:

maintaining a distance between the GMU and the assigned aircraft during taxiing to within a defined range.

15. The method of claim 13, wherein verifying whether an aircraft in proximity of the aircraft pick-up location is the assigned aircraft includes receiving a broadcast identification beacon from the aircraft and comparing identification information in the broadcast identification beacon with identification information of the assigned aircraft.

16. The method of claim 13, wherein determining light commands includes determining when to provide a follow-me, stop, turn left, and turn right command.

17. The method of claim 13, comprising:

sending to the TCGS information regarding a location and heading of the GMU and a location of the assigned aircraft.

18. An airport follow-me guidance system comprising:

a traffic control ground station (TCGS) for directing aircraft during taxiing; and

a plurality of aircraft guiding mobile units (GMUs), each GMU configured to guide an aircraft during taxiing, wherein each GMU includes;

one or more light modules;

one or more processing units; and

one or more data storage mediums, the one or more data storage mediums including instructions which, when executed by the one or more processing units, cause the one or more processing units to;

receive control messages from the TCGS, the control messages assigning the GMU to an aircraft and controlling movement of the GMU and its assigned aircraft; and

provide light commands to a pilot of the assigned aircraft with the one or more light modules, the light commands directing movement of the assigned aircraft during taxiing.

19. The follow-me guidance system of claim 18, wherein the TCGS is configured to coordinate movement of all the GMUs to safely direct aircraft to an appropriate gate, runway entrance, or other location.

20. The follow-me guidance system of claim 18, wherein each GMU includes:

an engine for moving the GMU about an airport; and

a heading control system to control a direction of motion for the GMU;

wherein the instructions cause the one or more processing units to control the engine and the heading control system based on the control messages from the TCGS to guide the assigned aircraft.