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:
Jul. 16, 2019

Filed:

Mar. 04, 2016
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Steven E. Spoldi, Shelton, CT (US);

Alex Faynberg, Cheshire, CT (US);

Stephen Kubik, Shelton, CT (US);

Donald T. Ream, Jupiter, FL (US);

John Rucci, Jupiter, FL (US);

Stephen C. McCulley, Palm City, FL (US);

Christiaan Corry, Jupiter, FL (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/00 (2006.01); B64C 13/18 (2006.01); B64C 13/22 (2006.01); B64C 13/50 (2006.01); G05D 1/00 (2006.01); G05D 1/08 (2006.01);
U.S. Cl.
CPC ...
B64C 13/18 (2013.01); B64C 13/22 (2013.01); B64C 13/503 (2013.01); G05D 1/0061 (2013.01); G05D 1/0808 (2013.01); G05D 1/0858 (2013.01);
Abstract

A method for position hold override control of an aircraft includes determining, by a processor, that a position hold mode is enabled to hold the aircraft at a substantially fixed position with respect to a target. The processor receives a control input indicative of a commanded change in acceleration of the aircraft as an override of the position hold mode. The processor determines an acceleration command based on the commanded change in acceleration. The acceleration command is adjusted as an adjusted acceleration command responsive to a non-linear scheduled translational rate command based on feedback of a commanded velocity of the aircraft. An update to the commanded velocity of the aircraft is generated based on the adjusted acceleration command.


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