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:
Jan. 25, 2022

Filed:

Mar. 20, 2020
Applicant:

Steven M. Hoffberg, West Harrison, NY (US);

Inventor:

Steven M. Hoffberg, West Harrison, NY (US);

Assignee:

Other;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 39/00 (2006.01); B64C 23/00 (2006.01); B64C 21/00 (2006.01); B64C 23/08 (2006.01); B64C 17/02 (2006.01); F42B 10/02 (2006.01); F42B 10/62 (2006.01);
U.S. Cl.
CPC ...
B64C 39/001 (2013.01); B64C 17/02 (2013.01); B64C 21/00 (2013.01); B64C 23/005 (2013.01); B64C 23/08 (2013.01); B64C 2230/02 (2013.01); F42B 10/02 (2013.01); F42B 10/025 (2013.01); F42B 10/62 (2013.01);
Abstract

A method for controlling a flying projectile which rotates during flight, comprising: determining an angle of rotation of an inertial mass spinning about an axis during flight; and controlling at least one actuator for altering at least a portion of an aerodynamic structure, selectively in dependence on the determined angle of rotation and a control input, to control aerodynamic forces during flight. An aerodynamic surface may rotate and interact with surrounding air during flight, to produce aerodynamic forces. A sensor determines an angular rotation of the spin during flight. A control system, responsive to the sensor, produces a control signal in dependence on the determined angular rotation. An actuator selectively alters an aerodynamic characteristic of the aerodynamic surface in response to the control signal.


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