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:
Oct. 16, 2018

Filed:

Apr. 02, 2014
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Erez Eller, Oakville, CT (US);

Aaron L. Greenfield, Shelton, CT (US);

Ole Wulff, Ansonia, CT (US);

Matthew A. White, Milford, CT (US);

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

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/50 (2006.01); B64C 27/08 (2006.01); B64C 13/18 (2006.01); B64C 27/82 (2006.01);
U.S. Cl.
CPC ...
B64C 13/503 (2013.01); B64C 13/18 (2013.01); B64C 27/08 (2013.01); B64C 27/82 (2013.01); B64C 2027/8236 (2013.01); B64C 2027/8272 (2013.01); B64C 2027/8281 (2013.01); Y02T 50/44 (2013.01);
Abstract

One aspect is a flight control system for a rotary wing aircraft including a main rotor system and an elevator control system. A flight control computer of the flight control system includes processing circuitry configured to execute control logic. The control logic includes an inverse plant model that produces a main rotor feed forward command based on a pitch rate command, and a load alleviation control filter configured to reduce loads on a main rotor system and produce an elevator command for an elevator control system. A transformed elevator command filter produces a main rotor pitch adjustment command based on the elevator command, and a main rotor command generator generates an augmented main rotor feed forward command for the main rotor system based on the main rotor feed forward command and the main rotor pitch adjustment command.


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