Method for calibrating an airborne goniometry apparatus for low frequencies

Patent metadata

Field	Value
Publication number	US-11994602-B2
Application number	US-202217862752-A
Country	US
Kind code	B2
Filing date	Jul 12, 2022
Priority date	Jul 13, 2021
Publication date	May 28, 2024
Grant date	May 28, 2024

Abstract

The invention includes a method for calibrating at low frequency and in-flight a goniometry apparatus including an antenna array, on board an air carrier. The method includes for an angular position of reception, calibrating the airborne goniometry apparatus at a given frequency, comprising transmitting, by means of a calibration transmitter, at the given frequency and in the direction of the goniometry apparatus, at least two calibration signals, with polarizations orthogonal to each other. The method also includes measuring a response of the antenna array for each of the signals. The invention also includes a system implementing such a method.

First claim

The invention claimed is:

1. A method for calibrating at low frequency and in-flight a goniometry apparatus comprising an antenna array, on board an air carrier, said method comprising, for an angular position of reception:
calibrating said goniometry apparatus at a given frequency, comprising
transmitting, by means of a calibration transmitter, at said given frequency and in a direction of said goniometry apparatus, at least two calibration signals, with polarizations orthogonal to each other, and
measuring a response of said antenna array for each of said at least two calibration signals.

2. The method according to claim 1 , wherein the at least two calibration signals are transmitted simultaneously and comprise a frequency shift therebetween that is negligible with respect to their frequency of 200 kHz.

3. The method according to claim 1 , further comprising, for the angular position of reception, several iterations of the calibrating said goniometry apparatus for different frequencies so as to perform a frequency scan over a given range of frequency.

4. The method according to claim 1 , further comprising several iterations of the calibrating said goniometry apparatus in different angular positions of reception, following a predetermined calibration path.

5. The method according to claim 4 , wherein the predetermined calibration path comprises any combination of at least one of the following paths:
at least one horizontal linear path,
at least one upward helical path, and
at least one downward helical path.

6. The method according to claim 1 , further comprising, for said angular position and a frequency, calculating by interpolation calibration data for at least one target polarization, which is different from orthogonal polarizations, based on calibration data measured at said frequency and at said angular position.

7. A system for calibrating an airborne goniometry apparatus comprising:
a goniometry apparatus comprising an antenna array, configured to be on board an aerial carrier, and
at least one calibration transmitter, intended configured to transmit at least two calibration signals with orthogonal polarizations in a direction of said goniometry apparatus;
configured to implement a method for calibrating at low frequency and in-flight said goniometry apparatus, wherein for an angular position of reception
calibrating said goniometry apparatus at a given frequency, comprising
transmitting, by means of said at least one calibration transmitter, at said given frequency and in said direction of said goniometry apparatus, said at least two calibration signals, with said orthogonal polarizations orthogonal to each other, and

measuring a response of said antenna array for each of said at least two calibration signals.

8. The system according to claim 7 , wherein the at least one calibration transmitter comprises a single dual orthogonal polarization transmission antenna with radiating parts at +45°/−45°.

9. The system according to claim 7 , further comprises a first positioner for modifying a look direction of the at least one calibration transmitter, in azimuth and/or in elevation.

10. The system according to claim 9 , further comprising a second positioner for modifying a look direction of the antenna array, in azimuth and/or in elevation.

11. The system according to claim 7 , further comprising a geolocation module on a side of the goniometry apparatus to locate a position of said goniometry apparatus.

12. The system according to claim 7 , further comprising a module, disposed on a side of the goniometry apparatus, to determine at least one tilt of said goniometry apparatus and/or of the aerial carrier.

13. The system according to claim 7 , further comprising at least one calculation unit configured to calculate, by interpolation, calibration data for at least one unmeasured polarization, or an unmeasured frequency or an unmeasured angular position.

14. The system according to claim 7 , wherein the goniometry apparatus and the at least one calibration transmitter are equipped with communication modules enabling them to communicate with each other.

Assignees

• Bull Sas

Inventors

• Teneze Bernard
• Charton Philippe

Classifications

• G01S3/023 Primary

  Monitoring or calibrating · CPC title

• G01S3/465

  the waves arriving at the aerials being frequency modulated and the frequency difference of signals therefrom being measured · CPC title

• G01S3/146

  by comparing linear polarisation components · CPC title

• G01S1/026

  of associated receivers · CPC title

• H01Q3/267

  Phased-array testing or checking devices · CPC title