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. 13, 2021

Filed:

Dec. 21, 2018
Applicant:

United States of America As Represented BY the Administrator of the Nasa, Washington, DC (US);

Inventors:

Nhan Thanh Nguyen, Santa Clara, CA (US);

Kelley Elizabeth Hashemi, San Francisco, CA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/22 (2006.01); B64C 9/06 (2006.01); B64C 3/38 (2006.01); B64C 9/00 (2006.01); B64C 13/04 (2006.01); B64C 3/14 (2006.01);
U.S. Cl.
CPC ...
B64C 13/22 (2013.01); B64C 3/38 (2013.01); B64C 9/06 (2013.01); B64C 13/04 (2013.01); B64C 3/14 (2013.01); B64C 2003/147 (2013.01); B64C 2009/005 (2013.01);
Abstract

A flight control system for an aircraft having a multi-functional flight control surface. The aircraft has at least one multi-functional flight control surface formed by a sequence of flaps. The shape of each multi-functional flight control surface may be configured by a flight control to simultaneously adjust a trajectory of the aircraft in two or more of a pitch direction, a roll direction, and a yaw direction. The flight control for operating said the multi-functional flight control surface responds to both pilot commands and machine-generated commands. The machine-generated commands configure the shape of the surface of each multi-functional flight control surface in real-time based, at least in part, upon a set of flight objectives comprising: (a) minimizing drag of the aircraft, (b) aeroelastic modal suppression for the aircraft, and (c) maneuver load alleviation in the aircraft.


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