METHOD AND DEVICE FOR ESTIMATING AT LEAST ONE WIND CHARACTERISTIC ON AN AIRCRAFT

• US 20100241294A1
• Filed: 03/08/2010
• Published: 09/23/2010
• Est. Priority Date: 03/17/2009
• Status: Active Grant

• Current Assignee: Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Original Assignee: Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Inventors: Virelizier, Pierre, Bochot, Thomas
• Granted Patent: US 8,255,101 B2
• Time in Patent Office: Days
• US Class Current: 701/14
• CPC Class Codes: G01P 13/025 indicating air data, i.e. flight variables of an aircraft, e.g. angle of attack, side slip, shear, yaw
• CPC Class Codes: G01P 5/00 Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft application of speed-measuring devices for measuring volume of fluid G01F
• CPC Class Codes: G01P 5/16 using Pitot tubes , e.g. Machmeter

Abstract

A method and a device for estimating on an aircraft at least one wind characteristic.

The device (1) comprises means (7) for determining a corrective term being representative of an apparent wind created upon a rotation of the aircraft and means (4) for determining the wind characteristic taking into account such a corrective term.

Claims

1. A method for automatically estimating aboard an aircraft (AC) at least one wind characteristic existing outside said aircraft (AC), such a method wherein, upon said aircraft (AC) flying, the following automated operations are performed:

a) a first piece of speed information is received relating to the speed of the aircraft (AC) in a terrestrial reference system, being expressed in a first point (G) of the aircraft (AC);

b) a second piece of speed information ({right arrow over (Vair)}) is received relating to the speed of the aircraft (AC) in the air, being expressed in a second point (A) of the aircraft; and

c) from at least said first and second speed information, said wind characteristic is determined in said terrestrial reference system, such a wind characteristic being determined taking into account a corrective term being representative of an apparent wind,

wherein said corrective term TC is calculated using the following expression;

TC={right arrow over (Ω

)}̂

{right arrow over (GA)}

wherein;

̂

represents the vector product;

{right arrow over (Ω

)} represents the rotation rate of the aircraft (AC) in an inertial reference system;

G represents a reference point of the aircraft (AC), corresponding to said first point; and

A represents the position on the aircraft (AC) of at least one anemometric probe, the measurements thereof being used for determining said second piece of speed information, such a position A corresponding to said second point.

2. A method according to claim 1,

wherein in step c), there is calculated, as a wind characteristic, a speed vector {right arrow over (Vv)} of said wind, using the following expression:

{right arrow over (Vv)}={right arrow over (Vgs)}−

{right arrow over (Vair)}+{right arrow over (Ω

)}̂

{right arrow over (GA)}

wherein;

{right arrow over (Vgs)} represents said first piece of speed information;

{right arrow over (Vair)} represents said second piece of speed information;

̂

represents the vector product;

{right arrow over (Ω

)} represents the rotation rate of the aircraft (AC) in an inertial reference system;

G represents a reference point of the aircraft (AC), corresponding to said first point; and

A represents the position on the aircraft (AC) of at least one anemometric probe, the measurements thereof being used for determining said second piece of speed information, such a position A corresponding to said second point.

3. A method for automatically generating aboard an aircraft (AC) at least one wind characteristic existing outside said aircraft (AC),

wherein, upon said aircraft (AC) flying, the following automated operations are performed:

a) a first piece of speed information is determined on the aircraft (AC);

b) a second piece of speed information is determined on the aircraft (AC); and

c) from said first and second speed information, said wind characteristic is determined, implementing the method according to claim 1.

4. A device for automatically estimating aboard an aircraft (AC) at least one wind characteristic existing outside said aircraft (AC), said device (1) being aboard the aircraft (AC) and comprising:

first means (2) for receiving a first piece of speed information relating to the speed of the aircraft (AC) in a terrestrial reference system, being expressed in a first point (G) of the aircraft (AC);

second means (3) for receiving a second piece of speed information ({right arrow over (Vair)}) relating to the speed of the aircraft (AC) in the air, being expressed in a second point (A) of the aircraft (AC);

auxiliary means (7) for calculating a corrective term being representative of an apparent wind; and

third means (4) for determining, at least from said first and second speed information, said wind characteristic in the terrestrial reference system, said third means (4) being formed so as to determine said wind characteristic taking into account said corrective term,

wherein said auxiliary means (7) comprise elements for calculating said corrective term TC using the following expression;

TC={right arrow over (Ω

)}̂

{right arrow over (GA)}

wherein;

̂

represents the vector product;

{right arrow over (Ω

)} represents the rotation rate of the aircraft (AC) in an inertial reference system;

G represents a reference point of the aircraft (AC), corresponding to said first point; and

A represents the position on the aircraft (AC) of at least one anemometric probe, the measurements thereof being used for determining said second piece of speed information, such a position A corresponding to said second point.

5. A system for automatically generating aboard an aircraft (AC) at least one wind characteristic existing outside said aircraft (AC),

wherein it is located aboard the aircraft (A) and comprises:

means (13) for generating a first piece of speed information;

means (11) for generating a second piece of speed information; and

a device (1) according to claim 4, for estimating said wind characteristic by means of said first and second speed information.

6. A system according to claim 5, it further comprising means (15) so as to show to a crew member of the aircraft (AC) the wind characteristic having been estimated by said device (1).

7. An aircraft, comprising a device (1) according to claim 4.

8. An aircraft, comprising a system (10) according to claim 5.