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:
Nov. 24, 2020

Filed:

Feb. 06, 2017
Applicant:

Brunswick Corporation, Lake Forest, IL (US);

Inventors:

Jason S. Arbuckle, Horicon, WI (US);

Thomas S. Kirchhoff, Fond Du Lac, WI (US);

Steven J. Andrasko, Oshkosh, WI (US);

Assignee:

Brunswick Corporation, Mettawa, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/02 (2020.01); B63H 25/42 (2006.01); B62D 6/00 (2006.01); B63H 25/02 (2006.01); B63H 21/21 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0206 (2013.01); B62D 6/005 (2013.01); B63H 25/02 (2013.01); B63H 25/42 (2013.01); B63H 2021/216 (2013.01); B63H 2025/022 (2013.01);
Abstract

A method for maintaining a marine vessel propelled by a marine propulsion device in a selected position includes determining a current global position of the marine vessel and receiving a signal command to maintain the current global position. The current global position is stored as a target global position in response to receiving the signal command. A subsequent global position of the marine vessel is determined and a position error difference between the subsequent global position and the target global position is determined. The method includes determining marine vessel movements required to minimize the position error difference, and causing the marine propulsion device to produce a thrust having a magnitude, a direction, and an angle calculated to result in achievement of the required marine vessel movements. At least one of timing and frequency of discontinuity of thrust production is controlled while the position error difference is minimized.


Find Patent Forward Citations

Loading…