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:
Feb. 07, 2017

Filed:

Jul. 18, 2012
Applicants:

Itzhak Yogev, Tel-Mond, IL;

Michael Shepshelovich, Ganei Tikva, IL;

Danny Abramov, Rehovot, IL;

Inventors:

Itzhak Yogev, Tel-Mond, IL;

Michael Shepshelovich, Ganei Tikva, IL;

Danny Abramov, Rehovot, IL;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 9/12 (2006.01); B64C 9/32 (2006.01); B64C 15/02 (2006.01);
U.S. Cl.
CPC ...
B64C 9/12 (2013.01); B64C 9/323 (2013.01); B64C 9/326 (2013.01); B64C 15/02 (2013.01); Y02T 50/32 (2013.01);
Abstract

A method for providing a controllable side force to an air vehicle having a vertical stabilizer arrangement includes (a) selectively causing the vertical stabilizer arrangement to generate a first side force in a first side direction to provide the controllable side force, the first side force inducing a corresponding first yaw moment in a first yaw direction; and (b) selectively providing to the air vehicle a second yaw moment in a second yaw direction, the second yaw moment being induced by a force component of an auxiliary force applied to the air vehicle, the force component being in a force direction that is non-parallel with respect to the first side direction and the force component being spaced from a center of gravity of the air vehicle; wherein the second yaw direction is opposed to the first yaw direction. Also disclosed is a corresponding auxiliary yaw generating system.


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