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:
Apr. 21, 2015
Filed:
Jan. 20, 2011
Applicant:
Aviv Tzidon, Tel Aviv, IL;
Inventor:
Aviv Tzidon, Tel Aviv, IL;
Assignee:
Elbit Systems Ltd., Haifa, IL;
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
H04L 12/26 (2006.01); H04J 3/16 (2006.01); G01S 19/23 (2010.01); G01S 19/42 (2010.01); G01S 19/52 (2010.01); H04B 7/26 (2006.01); H04W 4/06 (2009.01); H04W 84/06 (2009.01);
U.S. Cl.
CPC ...
H04J 3/1682 (2013.01); G01S 19/23 (2013.01); G01S 19/42 (2013.01); G01S 19/52 (2013.01); H04B 7/2643 (2013.01); H04W 4/06 (2013.01); H04W 84/06 (2013.01);
Abstract
A method for estimating engine thrust values of an aircraft is disclosed, the method comprising calculating estimated thrust value of an engine based on an equation of longitudinal motion, aircraft data measured during flight and calibrated drag/lift models, and a method for determining the thrust of an aircraft engine, based on information available from tracking the aircraft air-speed, acceleration, and position, the method comprising calculating the thrust, using the following equation: Thrust=mg{dot over (H)}/V+m{dot over (V)}+Drag.