SYSTEM AND METHOD FOR DETERMINING A LENGTH OF AN EXTERNAL LOAD SLING

• US 20160048131A1
• Filed: 08/11/2015
• Published: 02/18/2016
• Est. Priority Date: 08/12/2014
• Status: Active Grant

• Current Assignee: Sikorsky Aircraft Corporation (Martin Marietta Corporation)
• Original Assignee: Sikorsky Aircraft Corporation (Martin Marietta Corporation)
• Inventors: Lesperance, Jesse J., Zygmant, Thomas
• Granted Patent: US 9,718,547 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B64D 1/22 Taking-up articles from earth's surface
• CPC Class Codes: G05D 1/102 specially adapted for vertical take-off of aircraft

Abstract

A system and method for determining length of load sling assembly in an aircraft, includes receiving, with a processor, information via one or more sensors regarding a load length during a delivery and descent state, the load length comprising length of a load sling assembly and a load height; controlling, with the processor, a minimum altitude of operation of the aircraft that ensures that the load does not touch the ground or obstacles during one or more of a flight plan, during decent, or during delivery; determining, with the processor, when a load has touched a ground in response to the receiving of the load length information; and releasing, with the processor, the load from the load sling assembly when the processor determines that the load has touched the ground.

Claims

1. A method for determining length of load sling assembly in an aircraft, comprising:

receiving, with a processor, information via one or more sensors regarding a load length during a delivery and descent state, the load length comprising length of a load sling assembly and a load height;

controlling, with the processor, a minimum altitude of operation of the aircraft that ensures that the load does not touch the ground or obstacles during one or more of a flight plan, during decent, or during delivery;

determining, with the processor, when a load has touched a ground in response to the receiving of the load length information; and

releasing, with the processor, the load from the load sling assembly when the processor determines that the load has touched the ground.

2. The method of claim 1, further comprising determining the load height during an initial descent state.

3. The method of claim 1, wherein the determining of the load height during the initial descent state further comprises determining the load height from one or more of a distance of the aircraft to each of the load, a pendant, a bucket height factor, and the ground.

4. The method of claim 1, wherein the receiving of the information regarding the load length further comprises receiving information regarding the load height during a lift state.

5. The method of claim 1, wherein the receiving of the load height information during the lift state further comprises determining the load height as a function of a distance of the aircraft to the load and a distance of the aircraft to the ground.

6. The method of claim 5, wherein the receiving of the load height information during the lift state further comprises determining the load length through successive iterations of the difference between the distance between the aircraft to each of the load and the pendant.

7. The method of claim 1, further comprising navigating the load to a landing site in response to receiving the load length information during the delivery and descent state.

8. A system for determining length of load sling assembly in an aircraft, comprising:

one or more sensors coupled to the aircraft;

the load sling assembly including a sling coupled to an attachment device and a load; and

memory having instructions stored thereon that, when executed by the processor, cause the system to;

receive information regarding a load length during a delivery and descent state, the load length comprising a length of the load sling assembly and a load height;

control a minimum altitude of operation of the aircraft that ensures that the load does not touch the ground or obstacles during one or more of a flight plan, during decent, or during delivery;

determine when a load has touched a ground in response to the receiving of the load length information; and

release the load from the load sling assembly when the processor determines that the load has touched the ground.

9. The system of claim 8, wherein the processor is configured to determine the load height during an initial descent state.

10. The system of claim 8, wherein the processor is configured to determine the load height from one or more of a distance of the aircraft to each of the load, a pendant, a bucket height factor, and the ground.

11. The system of claim 8, wherein the processor is configured to receive information regarding the load height during a lift state.

12. The system of claim 8, wherein the processor is configured to determine the load height as a function of a distance of the aircraft to the load and a distance of the aircraft to the ground.

13. The system of claim 12, wherein the processor is configured to determine the load length through successive iterations of the difference between the distance between the aircraft to each of the load and the pendant.

14. The system of claim 8, wherein the processor is configured to navigate the load to a landing site in response to receiving the load length information during the delivery and descent state.