Title:
METHOD FOR DETERMINING A STATE OF CREDIBILITY OF MEASUREMENTS MADE BY SENSORS OF AN AIRCRAFT AND CORRESPONDING SYSTEM
Document Type and Number:
WIPO Patent Application WO/2013/144126
Kind Code:
A3
Abstract:
This method for determining a state of credibility of measurements made by static and total pressure sensors and incidence sensors of an aircraft comprises the following steps: - determining (31) a speed of the aircraft, from static and total pressure measurements, - determining (33) a lift coefficient of the aircraft from an incidence measurement (31) and from said speed, - determining (39) a mass of the aircraft, - determining (70) if an equation of lift of the aircraft is verified, - activating a state of optimal credibility (74), wherein the measurements made by said sensors are considered to be reliable if said equation of lift is verified, - activating (75, 83) a state of non-optimal credibility (76; 84), wherein the measurements of at least one sensor are considered to be unreliable if said equation of lift is not verified.
Inventors:
DUPONT DE DINECHIN SEBASTIEN (FR)
Application Number:
PCT/EP2013/056368
Publication Date:
November 14, 2013
Filing Date:
March 26, 2013
Export Citation:
Assignee:
DASSAULT AVIAT (FR)
International Classes:
B64D43/02; G01C23/00; G01P13/02; G01P21/00
Domestic Patent References:
WO2007104851A1 | 2007-09-20 |
Foreign References:
EP0863451A1 | 1998-09-09 | |||
EP1498737A1 | 2005-01-19 | |||
US20100100260A1 | 2010-04-22 |
Attorney, Agent or Firm:
BLOT, Philippe et al. (2 place d'Estienne d'Orves, Paris, FR)
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