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:
Aug. 01, 2023

Filed:

Mar. 25, 2019
Applicant:

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

Inventor:

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

Assignee:

Other;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
A63H 33/18 (2006.01); G05D 1/10 (2006.01); G05D 1/00 (2006.01); F42B 10/62 (2006.01); A63H 27/00 (2006.01); A63H 30/04 (2006.01); F42B 10/02 (2006.01);
U.S. Cl.
CPC ...
A63H 33/18 (2013.01); F42B 10/62 (2013.01); G05D 1/0022 (2013.01); G05D 1/105 (2013.01); A63B 2225/01 (2013.01); A63B 2225/20 (2013.01); A63B 2225/50 (2013.01); A63H 27/00 (2013.01); A63H 30/04 (2013.01); F42B 10/025 (2013.01);
Abstract

A method of controlling a gyroscopically-stabilized projectile, comprising a control system producing a control signal, a rotating aerodynamic shell, and a reaction mass system responsive to the control signal, the method comprising: imparting rotational and translational kinetic energy to induce gyroscopic stabilization of the projectile about a gyroscopic axis and a movement of the projectile along a flight path; interacting the shell with surrounding air while moving, to induce aerodynamic forces; generating the control signal from the control system; and altering a state of the reaction wheel system selectively in dependence on the control signal, to alter the flight path.


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