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:
Nov. 25, 2014

Filed:

Nov. 11, 2008
Applicants:

Hugues Meunier, Frouzins, FR;

Nicolas Marty, Saint Sauveur, FR;

Aurélie Sallier, Toulouse, FR;

Inventors:

Hugues Meunier, Frouzins, FR;

Nicolas Marty, Saint Sauveur, FR;

Aurélie Sallier, Toulouse, FR;

Assignee:

Thales, Neuilly-sur-Seine, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01C 5/00 (2006.01); G05D 1/00 (2006.01); G05D 3/00 (2006.01); G06F 7/00 (2006.01); G06F 17/00 (2006.01); G01S 13/94 (2006.01); G08G 5/00 (2006.01); G08G 5/02 (2006.01);
U.S. Cl.
CPC ...
G01S 13/94 (2013.01); G08G 5/0086 (2013.01); G08G 5/025 (2013.01); G08G 5/0065 (2013.01);
Abstract

Described is a method of protecting an aircraft in approach by signalling against risks of collision with a terrain in steep-sided environments in order to avoid unwanted warnings emanating from clearance sensors of the on-board TAWS (Terrain Awareness and Warning System) while protecting the aircraft when the aircraft fails to observe a published procedure which includes a landing procedure and a take-off procedure. The method, in some embodiments, includes modifying characteristics of at least one of the clearance sensors according to the position deviation of the aircraft relative to a published RNP (Required Navigation Performance) trajectory.


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