System and method for aiding airdrop computations

• US 20080078881A1
• Filed: 08/14/2006
• Published: 04/03/2008
• Est. Priority Date: 08/14/2006
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Parras, Gerald
• Granted Patent: US 8,271,179 B2
• Time in Patent Office: Days
• US Class Current: 244/137.1
• CPC Class Codes: G05D 1/105 specially adapted for unpowered flight, e.g. glider, parachuting, forced landing parachutes per se B64D17/00

Abstract

A system and method for aiding airdrop computations is described. The system includes a ground system, a data link, and an airborne system. The ground system accumulates substantially real time drop zone GPS and meteorological data, which is transferred to the airborne system via the data link. The airborne system makes adjustments to a release point of the airdrop based on the data received from the ground system. Additionally, the airborne system provides airdrop status to the ground system via the data link.

Claims

1. A system for aiding airdrop computations, comprising in combination:

a ground system that includes a first computer that receives data from a plurality of sensors; and

an airborne system that includes a second computer that calculates a release point for an airdrop maneuver;

wherein the ground system and the airborne system communicate via a data link to allow the sensor data received by the first computer to be communicated to the second computer, and wherein the second computer calculates the release point based on the sensor data.

2. The system of claim 1, wherein the second computer communicates status of the airdrop maneuver to the first computer via the data link.

3. The system of claim 1, wherein the plurality of sensors provides position and meteorological data.

4. The system of claim 1, wherein the plurality of sensors includes a Global Positioning System.

5. The system of claim 1, wherein the plurality of sensors includes air data sensors selected from the group consisting of a pilot balloon, a clinometer, an anemometer, a thermometer, and a barometer.

6. The system of claim 1, wherein at least one of the sensors automatically transmits data to the first computer.

7. The system of claim 1, wherein data from at least one of the sensors is manually entered into the first computer.

8. The system of claim 1, wherein the first computer includes a wind calculator algorithm.

9. The system of claim 1, wherein the data link is a Link 16 data link.

10. The system of claim 1, further comprising a first data link unit for communicating data between the first computer and the data link, and a second data link unit for communicating data between the second computer and the data link.

11. The system of claim 10, wherein the first data link unit and the second data link unit are tactical data link units.

12. The system of claim 1, wherein the second computer computes a lateral track for the airborne system to follow during the airdrop maneuver.

13. A method for aiding airdrop computations, comprising in combination:

receiving substantially real time sensor data from a drop zone via a data link;

calculating a release point for an airdrop maneuver based on the received sensor data; and

adjusting a flight plan based on the calculated release point.

14. The method of claim 13, further comprising obtaining the sensor data from the drop zone.

15. The method of claim 13, further comprising notifying flight crew of the adjusted flight plan.

16. The method of claim 13, further comprising providing ground crew a status of the airdrop maneuver via the data link.

17. A method for receiving status of an airdrop maneuver, comprising in combination:

providing an initial flight plan for an airdrop maneuver to a computer accessible by ground crew; and

providing an updated flight plan for the airdrop maneuver to the computer via a data link as the airdrop maneuver progresses, wherein the updated flight plan includes an adjustment to a release point.

18. The method of claim 17, wherein the computer displays an aircraft symbol overlaying a lateral track that represents the updated flight plan.

19. The method of claim 18, wherein the release point is depicted on the lateral track.

20. The method of claim 17, wherein the adjustment to the release point is based on substantially real time sensor data communicated to an aircraft via the data link.