METHOD AND APPARATUS FOR AUTOMATICALLY CONTROLLING AIRBORNE VEHICLE LIGHTING SYSTEMS

• US 20120133283A1
• Filed: 02/28/2011
• Published: 05/31/2012
• Est. Priority Date: 03/02/2010
• Status: Active Grant

• Current Assignee: Evolved Aircraft Systems, LLC
• Original Assignee: Evolved Aircraft Systems, LLC
• Inventors: Everett, Michael Louis, Everett, Louis Jackson, Ruiz, Mario Jr.
• Granted Patent: US 8,970,111 B2
• Time in Patent Office: Days
• US Class Current: 315/77
• CPC Class Codes: B64D 47/02 Arrangements or adaptations of signal or lighting devices
• CPC Class Codes: H05B 31/50 specially adapted for ac
• CPC Class Codes: H05B 47/105 in response to determined parameters
• CPC Class Codes: H05B 47/11 by determining the brightness or colour temperature of ambient light
• CPC Class Codes: H05B 47/115 by determining the presence or movement of objects or living beings
• CPC Class Codes: Y02B 20/40 Control techniques providing energy savings, e.g. smart controller or presence detection

Abstract

An airborne vehicle lighting control apparatus and method for automatically controlling activation and deactivation of an airborne vehicle lighting system. A processor for automatically controlling the lighting system can be employed and having one or more sensors operatively connected to the processor for sensing the current flight operating mode and geographical position of an airborne vehicle. The processor can activate or deactivate lighting based on the current flight operating mode and position.

Claims

1. An apparatus for automatically controlling airborne vehicle lighting, comprising:

a vehicle lighting system for a vehicle;

a processor for automatically controlling activation and deactivation of said vehicle lighting system based on an operating mode of said vehicle, wherein said processor communicates with said vehicle lighting system; and

at least one sensor operatively connected to said processor for sensing said operating mode of said vehicle.

2. The apparatus of claim 1, wherein said operating mode is determined by said processor based on a three-dimensional geographical position of said vehicle.

3. The apparatus of claim 2, further comprising:

a GPS sensor operatively connected to said processor to determine said three-dimensional geographical position wherein said three-dimensional geographical position includes both an altitude above ground and a geographical position.

4. The apparatus of claim 3, further comprising:

a database comprising data indicative of a plurality of three-dimensional airspace coordinates, wherein said operating mode of said vehicle is determinate upon said three-dimensional geographical position located within said three-dimensional geographical airspace coordinates.

5. The apparatus of claim 1 wherein said database is stored in a memory that communicates with said processor.

6. The apparatus of claim 1, wherein said at least one sensor comprises a vehicle speed sensor operatively connected to said processor to determine said operating mode.

7. The apparatus of claim 1, wherein said at least one sensor comprises at least one ambient light sensor operatively connected to said processor to determine vehicle lighting system requirements.

8. The apparatus of claim 1, wherein said vehicle comprises an airborne vehicle.

9. The apparatus of claim 8, wherein said operating mode of said airborne vehicle is determinate on a three-dimensional geographical position of said vehicle located within or without a three-dimensional geographical airspace, an altitude above ground of said vehicle, and airspeed of said vehicle.

10. An apparatus for automatically controlling airborne vehicle lighting, comprising:

a vehicle lighting system for a vehicle;

a processor for automatically controlling activation and deactivation of said vehicle lighting system based on an operating mode of said vehicle;

wherein said processor communicates with said vehicle lighting system; and

at least one sensor operatively connected to said processor for sensing said operating mode of said vehicle, wherein said operating mode is determined by said processor based on a three-dimensional geographical position of said vehicle.

11. The apparatus of claim 10, further comprising:

a GPS sensor operatively connected to said processor to determine said three-dimensional geographical position wherein said three-dimensional geographical position includes both an altitude above ground and a geographical position; and

a database comprising data indicative of a plurality of three-dimensional airspace coordinates, wherein said operating mode of said vehicle is determinate upon said three-dimensional geographical position located within said three-dimensional geographical airspace coordinates.

12. The apparatus of claim 10, wherein said vehicle comprises an airborne vehicle.

13. An method for automatically controlling airborne vehicle lighting, comprising:

providing a vehicle lighting system for a vehicle;

automatically controlling, via a processor, activation and deactivation of said vehicle lighting system based on an operating mode of said vehicle, wherein said processor communicates with said vehicle lighting system; and

sensing said operating mode of said vehicle utilizing at least one sensor operatively connected to said processor.

14. The method of claim 13, further comprising:

determining said operating mode based on a three-dimensional geographical position of said vehicle.

17. The method of claim 13, further comprising:

storing said database in a memory that communicates with said processor.

18. The apparatus of claim 13, further comprising:

configuring said at least one sensor to comprise a vehicle speed sensor operatively connected to said processor to determine said operating mode.

19. The method of claim 13, further comprising:

configuring said at least one sensor to comprise at least one ambient light sensor operatively connected to said processor to determine vehicle lighting system requirements.

20. The method of claim 13, wherein said vehicle comprises an airborne vehicle and wherein said operating mode of said airborne vehicle is determinate on a three-dimensional geographical position of said vehicle located within or without a three-dimensional geographical airspace, an altitude above ground of said vehicle, and airspeed of said vehicle.

15. The method of 14, further comprising:

determining via a GPS sensor, said three-dimensional geographical position, wherein said three-dimensional geographical position includes both an altitude above ground and a geographical position.

16. The method of claim 15, further comprising:

configuring a database to comprise data indicative of a plurality of three-dimensional airspace coordinates, wherein said operating mode of said vehicle is determinate upon said three-dimensional geographical position located within said three-dimensional geographical airspace coordinates.