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:
Apr. 26, 2022

Filed:

May. 20, 2019
Applicant:

Textron Innovations Inc., Providence, RI (US);

Inventors:

Luke Dafydd Gillett, Grapevine, TX (US);

Sung Kyun Kim, Bedford, TX (US);

Robert Earl Worsham, II, Weatherford, TX (US);

Assignee:

TEXTRON INNOVATIONS INC., Providence, RI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/50 (2006.01); B64C 13/04 (2006.01); B64C 27/605 (2006.01); B64C 27/78 (2006.01); B64C 27/82 (2006.01); B64C 27/08 (2006.01); B64D 35/04 (2006.01); B64C 27/72 (2006.01); B64C 39/02 (2006.01);
U.S. Cl.
CPC ...
B64C 13/503 (2013.01); B64C 13/0421 (2018.01); B64C 27/08 (2013.01); B64C 27/605 (2013.01); B64C 27/78 (2013.01); B64C 27/82 (2013.01); B64D 35/04 (2013.01); B64C 39/024 (2013.01); B64C 2027/7255 (2013.01); B64C 2027/8263 (2013.01); B64C 2201/024 (2013.01);
Abstract

In an embodiment, a rotorcraft includes: a flight control computer configured to: receive a first sensor signal from a first aircraft sensor of the rotorcraft; receive a second sensor signal from a second aircraft sensor of the rotorcraft, the second aircraft sensor being different from the first aircraft sensor; combine the first sensor signal and the second sensor signal with a complementary filter to determine an estimated vertical speed of the rotorcraft; adjust flight control devices of the rotorcraft according to the estimated vertical speed of the rotorcraft, thereby changing flight characteristics of the rotorcraft; and reset the complementary filter in response to detecting the rotorcraft is grounded.


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