Method and device for aiding the piloting of an aircraft

• US 8,086,362 B2
• Filed: 08/20/2008
• Issued: 12/27/2011
• Est. Priority Date: 08/22/2007
• Status: Active Grant

• Current Assignee: Airbus Operations SAS (Airbus SE)
• Original Assignee: Airbus, Airbus Operations SAS (Airbus SE)
• Inventors: Ferret, Nicolas, Foucault, Philippe, Dupre, Alain
• Primary Examiner(s): EL CHANTI, HUSSEIN A
• Application Number:
  US12/194,776
• Publication Number:
  US 20090055037A1
• Time in Patent Office: 1,224 Days
• Field of Search: 701/4, 701/5, 701/7, 701/8, 701/11, 701/14
• US Class Current: 701/14
• CPC Class Codes: G01C 23/005 Flight directors indicating arrangements specially adapted for rotary gyroscopes G01C19/32
• CPC Class Codes: G05D 1/0202 specially adapted to aircraft

Abstract

Method and device for assisting the piloting of an aircraft.

• • The device (1) comprises means (4) for determining, using a roll instruction and measured current values of external characteristics and of flight characteristics of the aircraft, a predicted path which is a flight path having a constant roll angel, taking account of the effect of the wind.

Claims

1. Method for assisting the piloting of an aircraft, the method comprising:

a) generating a roll instruction for the aircraft;

b) measuring current values of flight characteristics of the aircraft and current values of wind characteristics existing outside of the aircraft;

c) calculating a predicted path according to the generated roll instruction and the measured current values of wind characteristics by;

c1) calculating a first path which exhibits a constant roll angle corresponding to the generated roll instruction but which does not take account of the current values of the wind characteristics; and

c2) integrating the current values of the wind characteristics into the first path to obtain a predicted path which is at a constant roll angle; and

d) following calculating the predicted path, carrying out the following operations α and

β

repetitively;

α

) determining a new roll instruction based on the predicted path to obtain a new predicted path which approaches a particular point (P0); and

β

) repeating calculation of the new predicted path based on a new roll instruction until the new predicted path joins the particular point.

2. Method according to claim 1, wherein the predicted path is displayed on a navigation screen of the aircraft.

3. Method according to claim 1, wherein the predicted path is transmitted to an autopilot device of the aircraft, which then automatically pilots the said aircraft according to the said predicted path, wherein the aircraft is piloted with a roll angle equal to the said roll instruction.

4. Method according to claim 1, wherein the first path is determined as a circular path of constant radius R and the said radius R is calculated using the following expression:

R=(Vtas²/g)/tan φ

wherein;

Vtas is the measured speed of the aircraft;

g is the acceleration of gravity;

tan is the tangent; and

φ

is the said roll instruction.

5. Method according to claim 1, wherein the said predicted path is generated in the form of a series of points which are connected to each other by straight segments.

6. Method according to claim 5, wherein the predicted path Tp comprises a number n of points P1 to Pn, and each of the points Pp of the predicted path, with 1≦

p≦

n, has the following coordinates Xp and Yp in an aircraft reference system;

Xp=R.[1−

cos(π

.p/n)]+R(π

.p/n).(Wsp/Vtas).cos(Wdir-Hdg)

Yp=R.sin(π

.p/n)+R(π

.p/n)(Wsp/Vtas)sin(Wdir-Hdg)

in which expressions;

R is the radius of the said first path;

Wsp is the measured force of the wind;

Vtas is the measured speed of the aircraft;

Wdir is the direction of the wind, measured and projected into the aircraft reference system; and

Hdg is the measured heading of the aircraft.

7. Method according to claim 1, wherein step c2) takes into account an effect due to a turn of the aircraft following the said roll instruction, in order to determine the said predicted path.

8. Method according to claim 1, wherein b), c) and d) are carried out automatically and repetitively.

9. Method according to claim 1 , wherein the particular point corresponds to the end of a segment of path which the aircraft is required to join tangentially.

10. Device for assisting the piloting of an aircraft, the said device comprising:

roll instruction generator that generates a roll instruction for the aircraft;

aircraft information source that measures current values of flight characteristics of the aircraft and current values of wind characteristics existing outside of the aircraft; and

predicted path calculator that calculates, according to the generated roll instruction and the said measured current values, a predicted path which is a flight path with a constant roll angle, the predicted path calculator comprising;

a first element that calculates a first path which exhibits a constant roll angle corresponding to the generated roll instruction, but which does not take account of the current values of the wind characteristics; and

a second element that integrates the current values of the wind characteristics into the first path to obtain the said predicted path;

wherein

the predicted path calculator comprises a first unit that determines a new roll instruction based on the predicted path to obtain a new predicted path which approaches a particular point and a second unit that repeatedly calculates the new predicted path taking account of the new roll instruction until the new predicted path joins the particular point.

11. A method for assisting the piloting of an aircraft, the method comprising:

a) generating a roll instruction for the aircraft;

b) measuring current values of flight characteristics of the aircraft and current values of wind characteristics existing outside of the aircraft;

c) calculating a predicted path according to the generated roll instruction and the measured current values of wind characteristics by;

c1) calculating a first path which exhibits a constant roll angle corresponding to the generated roll instruction but which does not take account of the current values the wind characteristics, wherein the first path is determined as a circular path of constant radius R and the said radius R is calculated using the following expression;

R=(Vtas²/g)/tan φ

wherein;

Vtas is the measured speed of the aircraft;

g is the acceleration of gravity;

tan is the tangent; and

φ

is the said roll instruction; and

c2) integrating the current values of the wind characteristics into the first path to obtain a predicted path (Tp) which is at a constant roll angle; and

d) following calculating the predicted path, carrying out the following operations α and

β

repetitively;

α

) determining a new roll instruction based on the predicted path to obtain a new predicted path which approaches a particular point; and

β

) repeating calculation of the new predicted path based on a new roll instruction until the new joins the particular point.

12. A method for assisting the piloting of an aircraft, the method comprising:

a) generating a roll instruction for the aircraft;

b) measuring current values of flight characteristics of the aircraft and current values of wind characteristics existing outside of the aircraft;

c) calculating a predicted path according to the generated roll instruction and the measured current values of wind characteristics by;

c1) calculating a first path which exhibits a constant roll angle corresponding to the generated roll instruction but which does not take account of the current values the wind characteristics; and

c2) integrating the current values of the wind characteristics into the first path to obtain a predicted path which is at a constant roll angle,

wherein

the predicted path Tp comprises a number n of points P1 to Pn, and each of the points Pp of the predicted path, with 1≦

p≦

n, has the following coordinates Xp and Yp in an aircraft reference system;

Xp=R.[1−

cos(π

.p/n)]+R(π

.p/n).(Wsp/Vtas).cos(Wdir-Hdg)

Yp=R. sin(π

.p/n)+R(π

.p/n)(Wsp/Vtas)sin(Wdir-Hdg)

in which expressions;

R is the radius of the said first path;

Wsp is the measured force of the wind;

Vtas is the measured speed of the aircraft;

Wdir is the direction of the wind, measured and projected into the aircraft reference system; and

Hdg is the measured heading of the aircraft; and

d) following calculating the predicted path, carrying out the following operations α and

β

repetitively;

α

) determining a new roll instruction based on the predicted path to obtain a new predicted path which approaches a particular point; and

β

) repeating calculation of the new predicted path based on a new roll instruction until the new joins the particular point.