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:
Dec. 17, 2019

Filed:

May. 22, 2017
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Matthew T. Luszcz, Hamden, CT (US);

David L. Adams, Wallingford, CT (US);

Mark R. Alber, Milford, CT (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Int. Cl.
CPC ...
G05D 1/00 (2006.01); F41G 5/18 (2006.01); B64C 29/00 (2006.01); B64C 27/10 (2006.01); B64C 27/82 (2006.01); B64C 27/57 (2006.01);
U.S. Cl.
CPC ...
F41G 5/18 (2013.01); B64C 27/10 (2013.01); B64C 27/57 (2013.01); B64C 27/82 (2013.01); B64C 29/0033 (2013.01); G05D 1/0094 (2013.01); B64C 2027/8236 (2013.01);
Abstract

A flight control system for an aircraft includes a flight control computer operatively interconnected with a main rotor system and a translational thrust system of the aircraft. A selectively enabled integrated target and flight control system arranged in communication with the flight control computer. The integrated target flight and control system is configured to control pitch attitude and heading of the aircraft. When the integrated target and flight control system is enabled, at least partial operation of the aircraft is controlled in response to a pilot input via the flight control computer.


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