System and method for indicating a landing zone to an inbound helicopter

Patent metadata

Field	Value
Publication number	US-8933820-B1
Application number	US-201213564546-A
Country	US
Kind code	B1
Filing date	Aug 1, 2012
Priority date	Aug 1, 2012
Publication date	Jan 13, 2015
Grant date	Jan 13, 2015

Abstract

A method of designating and communicating a desired LZ to an aircraft includes outputting a coded laser signal at or near a desired landing zone to indicate a location of the desired landing zone. The coded laser signal is received by an aircraft that desires to land at the desired landing zone. The location of the desired landing zone and an ingress path from a current location of the aircraft to the desired landing zone are determined by a processor provided with the aircraft.

First claim

What is claimed is:

1. A landing zone designation system, comprising:
a laser transmitter provided at or near a desired landing zone for an aircraft and that outputs a coded laser signal to indicate a location of the desired landing zone;
a laser receiver provided on the aircraft for picking up the coded laser signal and for determining a location of where the coded laser signal is being transmitted; and
a processor that receives information of the coded laser signal received by the laser receiver and that determines an ingress path from a current location of the aircraft to the location where the coded laser signal is being transmitted.

2. The landing zone designation system according to claim 1 , wherein the aircraft comprises a helicopter.

3. The landing zone designation system according to claim 2 , wherein the laser receiver comprises an electro-optic/infrared turret provided on the helicopter.

4. The landing zone designation system according to claim 1 , wherein the laser transmitter is provided on a rifle.

5. The landing zone designation system according to claim 4 , wherein the laser transmitter provided on the rifle corresponds to a target sighting device.

6. The landing zone designation system according to claim 1 , further comprising:
a portable voice communications unit that is configured to provide secure voice communications with the aircraft by a person not located within or near the aircraft,
wherein the secure voice communications is used to authenticate the desired landing zone.

7. A method of designating a landing zone for an aircraft, comprising:
outputting, at a desired landing zone, a coded laser signal to indicate a location of the desired landing zone;
receiving, by the aircraft, the coded laser signal; and
determining, by a processor on the aircraft, the location of the desired landing zone and an ingress path from a current location of the aircraft to the desired landing zone.

8. The method according to claim 7 , wherein the aircraft comprises a helicopter.

9. The method according to claim 8 , wherein the receiving is accomplished by an electro-optic/infrared turret provided on the helicopter.

10. The method according to claim 7 , wherein the coded laser signal is output by a laser transmitter that is provided on a rifle.

11. The method according to claim 10 , wherein the laser transmitter corresponds to a target sighting device.

12. The method according to claim 7 , further comprising:
establishing secure voice communications with the aircraft by a person not located within or near the aircraft,
wherein the secure voice communications is used to authenticate the desired landing zone.

13. A non-transitory computer readable medium storing computer program product that, when executed by at least one computer, performs the functions of:
receiving, by the aircraft, data associated with a coded laser signal that indicates a location of a desired landing zone for the aircraft; and
determining, by the aircraft, the location of the desired landing zone and an ingress path from a current location of the aircraft to the desired landing zone.

14. The non-transitory computer readable medium according to claim 13 , wherein the aircraft comprises a helicopter.

15. The non-transitory computer readable medium according to claim 14 , wherein the receiving is accomplished by an electro-optic/infrared turret provided on the helicopter.

16. The non-transitory computer readable medium according to claim 13 , wherein the coded laser signal is output by a laser transmitter that is provided on a rifle.

17. The non-transitory computer readable medium according to claim 16 , wherein the laser transmitter corresponds to a target sighting device.

18. The non-transitory computer readable medium according to claim 13 , further comprising:
establishing secure voice communications with the aircraft by a person not located within or near the aircraft; and
authenticating the desired landing zone using the secure voice communications.

19. The non-transitory computer readable medium according to claim 18 , wherein the authenticating using the secure voice communications is performed by confirming an appropriate code-of-the-day uttered by the person at the desired landing zone.

20. The non-transitory computer readable medium according to claim 13 , wherein the coded laser signal is output by a lightweight laser designator rangefinder (LLDR).

Assignees

• Tyson Stephen E
• Vogl Thomas L
• Rockwell Collins Inc

Inventors

• Tyson Stephen E
• Vogl Thomas L

Classifications

• B64F1/007 Primary

  Helicopter portable landing pads · CPC title

• B64F1/18

  Visual or acoustic landing aids · CPC title