METHOD FOR DETERMINING THE POSITION, NOTABLY IN TERMS OF ELEVATION, OF A TARGET FLYING AT VERY LOW ALTITUDE

• US 20090315755A1
• Filed: 05/09/2007
• Published: 12/24/2009
• Est. Priority Date: 05/16/2006
• Status: Active Grant

• Current Assignee: Thales SA
• Original Assignee: Thales SA
• Inventors: Cornic, Pascal, Barraux, Eric, Garrec, Patrick
• Granted Patent: US 7,994,964 B2
• Time in Patent Office: Days
• US Class Current: 342/38
• CPC Class Codes: G01S 13/68 for angle tracking only
• CPC Class Codes: G01S 13/913 for landing purposes
• CPC Class Codes: G01S 3/14 Systems for determining direction or deviation from predetermined direction aerial arrangements for changing or varying the orientation or the shape of the directional pattern H01Q3/00; combinations of different interacting aerial units for giving a desired directional characteristic H01Q21/29; aerials or aerial systems providing at least two radiation patterns H01Q25/00
• CPC Class Codes: G01S 3/48 the waves arriving at the antennas being continuous or intermittent and the phase difference of signals derived therefrom being measured

Abstract

The present invention relates to a method for determining the position notably the elevation of a target flying at very low altitude. An electromagnetic detection system extracts the measurement of the elevation on the basis of the amplitude of the interference signal produced by a signal emitted directly by the target and by a signal emitted by the target towards the ground then reflected by the ground towards the radar. Embodiments of the invention can notably be used within the framework of the guidance of drones in the final landing phase.

Claims

1. Method for determining by an electromagnetic detection system an elevation of a target close to a ground, comprising the steps of:

receiving, by a reception antenna, a first signal emitted directly by a target;

receiving, by the reception antenna, a second signal emitted by the target towards the ground then reflected by the ground toward the electromagnetic detection system; and

determining the of the target from an amplitude of an interference signal produced by the first signal and by the second signal.

2. The method of claim 1, further comprising the steps of:

emitting a detection signal towards the target, wherein the signal re-emitted directly by the target is the first signal, and the signal re-emitted by the target towards the ground then reflected by the ground is the second signal.

3. The method of claim 1, wherein the reception antenna comprises a plurality of sub-arrays of radiating elements, the method further comprising the steps of:

sampling the interference signal at the level of the sub-arrays, to produce a sampled interference signal; and

determining the elevation based on the amplitude of the sampled interference signal.

4. The method of claim 3, wherein the sub-arrays comprise a line of radiating elements disposed in a substantially horizontal, parallel and uniform manner over the reception antenna as a whole.

5. The method of claim 3, wherein the sub-arrays are situated in a substantially vertical plane.

6. Method according to claim 3, wherein a frequency f of the sampled signal is a value which minimizes the following a function:

$J<br><br>\left(U\right)=\underset{i,k}{\sum <br><br>}<br><br><br><br>r_{i+k}+r_{i-k}-2<br><br>r_i<br><br>\cos <br><br>\left(2<br><br>\mathrm{\pi <br><br>}<br><br><br><br>\mathrm{Uk}<br><br><br><br>\mathrm{\Delta <br><br>}\right)<br><br>$

wherein

r_i+k is a subtraction between a value of a signal received at sub-array i+k and the value of the signal received at sub-array of order i+k+1,

r<sub>i−

k</sub> is a subtraction between the value of the signal received at sub-array i−

k and the value of the signal received at sub-array i−

k−

1, and

Δ

is a distance between the phase centers of two consecutive sub-arrays.

7. The method of claim 1, further comprising the following step:

calculating a ratio between an elevation height h₂ of the target relative to the ground and a distance d projected on the ground between the electromagnetic detection system and the target according to the relationship;

h₂/d=λ

f/2 where λ

is a wavelength of the first signal and f is a frequency of the interference signal.

8. The method of claim 7, further comprising the following step:

obtaining the coordinates (x_R, z_R) of a reflection point R and an angle α

_R between the tangent plane to the ground at the point R and the horizontal on the basis of a cost function;

$<br><br>C<br><br>\left(r\right)<br><br>=<br><br>\frac{h_2-z_R+x_R\times <br><br>{\mathrm{\alpha <br><br>}}_R}{x_R}-\frac{h_2}{d-x_R}<br><br>$

wherein;

h₁ represents the height relative to the ground of the antenna,

h₂ represents the estimation of the elevation height calculated in the case of plane and horizontal ground, and

the values (x_R, z_R, α

_R) minimizing the cost function are the coordinates of the reflection point R.

9. The method of claim 8, further comprising the following steps:

correcting the height of the target relative to the tangent plane to a value H₂, using the value of the angle α

_R between the tangent plane at R to the terrain and the horizontal, as;

H₂=h₂+z_R+(d−

x_R)×

α

_R

wherein;

h₂ is the calculated height of the target relative to the ground in the case of plane and horizontal ground, and

d is the distance projected on the ground of the target from the antenna.

10. The method of claim 1, further comprising the followings step:

correlating an amplitude and a phase of the signal received with a predefined replica.

11. The method of claim 1, wherein the antenna used includes a sparse antenna.

12. The method of claim 1, wherein the target comprises an active emitter.

13. The method of claim 1, wherein the target includes a passive reflector.

14. The method of claim 1, wherein the target includes a drone in the landing phase.

15. The method of claim 1, further comprising the step of determining a height h₂ of the target by a monopulse-type process if the value of the amplitude of the reflection coefficient is less than a predetermined threshold.

16. The method of claim 7, further comprising the following step:

determining the elevation height h₂ for a non-plane and non-horizontal ground on the basis of a point of reflection R of a signal re-emitted by the target towards the ground on non-horizontal ground, or of an elevation height determined for plane and horizontal ground.