The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jan. 17, 2017

Filed:

May. 23, 2013
Applicant:

Honeywell International Inc., Morristown, NJ (US);

Inventors:

Michael Ray Elgersma, Plymouth, MN (US);

Xiaohong Linda Li, Plymouth, MN (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Morris Plains, NJ (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G06F 19/00 (2011.01); G06G 7/70 (2006.01); G08G 5/02 (2006.01); G05D 1/06 (2006.01); G05D 1/12 (2006.01); B64F 1/00 (2006.01); G05D 1/00 (2006.01); B64C 13/16 (2006.01);
U.S. Cl.
CPC ...
G08G 5/025 (2013.01); G05D 1/0684 (2013.01); B64C 13/16 (2013.01); B64F 1/00 (2013.01); G05D 1/00 (2013.01); G06F 19/00 (2013.01); G06G 7/70 (2013.01); G08G 5/02 (2013.01);
Abstract

A system and method of generating a landing trajectory for use in landing an aircraft onto a deck of a waterborne ship includes sensing motion of the ship, and sensing wind speed and wind direction. The sensed motion of the ship is processed to generate estimates of ship attitude and vertical speed, and the sensed wind speed and wind direction are processed to generate estimates of air-wake disturbances ahead of the aircraft. The landing trajectory is generated based on the estimates of ship attitude and vertical speed and the estimates of air-wake disturbances. The system and method implement model predictive control to calculate the control maneuvers multiple steps ahead, which provides the capability to smoothly control the timing of the aircraft touchdown phase.


Find Patent Forward Citations

Elgersma, Michael. (2017). Aircraft precision approach and shipboard landing control system and method (U.S. Patent No. 9547991). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9547991

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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