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:
May. 29, 2018

Filed:

May. 24, 2016
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Richard Pire, Istres, FR;

Marianne Gillet, Vitrolles, FR;

Nicolas Certain, Aix en Provence, FR;

Assignee:

AIRBUS HELICOPTERS, Marignane, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G08G 5/04 (2006.01); B64D 45/08 (2006.01); G08G 5/00 (2006.01); G01C 23/00 (2006.01);
U.S. Cl.
CPC ...
G08G 5/045 (2013.01); B64D 45/08 (2013.01); G01C 23/005 (2013.01); G08G 5/0021 (2013.01); G08G 5/0052 (2013.01); G08G 5/0086 (2013.01);
Abstract

A piloting assistance method for avoiding an obstacle with a rotorcraft flying along a current speed vector (Vect). An alert is generated by using a speed vector of the rotorcraft referred to as a 'calculation' speed vector (Vect) in order to determine whether the rotorcraft might impact an obstacle. During a correction stage and at each calculation iteration, the calculation speed vector (Vect) is determined using a horizontal component and a vertical component, the vertical component being a function of a current vertical speed of the rotorcraft relative to the ground corrected with a corrective term, the corrective term being a function of a product of a current path speed of the rotorcraft multiplied by the derivative of the path speed.


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