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.
Patent No.:
Date of Patent:
Aug. 15, 2017
Filed:
Jan. 10, 2013
Applicant:
Israel Aerospace Industries Ltd., Lod, IL;
Inventors:
Guy Dekel, Kazir, IL;
Lior Zivan, Hadera, IL;
Yoav Efraty, Tel Aviv, IL;
Amit Wolff, Zur Moshe, IL;
Avner Volovick, Petach Tikva, IL;
Assignee:
ISRAEL AEROSPACE INDUSTRIES LTD., Lod, IL;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/26 (2006.01); B64C 29/00 (2006.01); B64C 39/02 (2006.01); B64C 19/00 (2006.01); G05D 1/06 (2006.01); G05D 1/08 (2006.01);
U.S. Cl.
CPC ...
B64C 27/26 (2013.01); B64C 19/00 (2013.01); B64C 29/00 (2013.01); B64C 29/0033 (2013.01); B64C 39/024 (2013.01); G05D 1/0676 (2013.01); G05D 1/0858 (2013.01); B64C 2201/021 (2013.01); B64C 2201/042 (2013.01); B64C 2201/086 (2013.01); B64C 2201/104 (2013.01); B64C 2201/162 (2013.01); B64C 2201/165 (2013.01); B64C 2201/187 (2013.01);
Abstract
A control system configured to control a deceleration process of an air vehicle which comprises at least one tiltable propulsion unit, each of the at least one tiltable propulsion units is tiltable to provide a thrust whose direction is variable at least between a general vertical thrust vector direction and a general longitudinal thrust vector direction with respect to the air vehicle.