Multiple-input multiple-output imaging radar system

Patent metadata

Field	Value
Publication number	US-12204012-B2
Application number	US-202117525851-A
Country	US
Kind code	B2
Filing date	Nov 12, 2021
Priority date	Nov 12, 2020
Publication date	Jan 21, 2025
Grant date	Jan 21, 2025

Abstract

The invention relates to a MIMO imaging radar system. The system comprises transmission channels (Ve 1 , VeM), reception channels (Vr 1 , VrN), and co-located radiating elements (ER e1 , ER eM , ER r1 , ER rN ) forming a two-dimensional antenna array. Each radiating element (ER e1 , ER eM , ER r1 , ER rN ) has a predefined instantaneous field of coverage. Each radiating element is formed by a plurality of p radiating sub-elements (SeElt 1 , SsEltp) distributed in at least one of the two dimensions of the antenna array. The radar comprises a plurality of electronic steering modules (MD e1 , . . . , MD rN ). Each electronic steering module is connected to one radiating element. Each steering module is configured to apply a steering command (Cmd) between all the radiating sub-elements (SeElt 1 , SsEltp) of a given radiating element. The steering command (Cmd) is identical from one radiating element to the next, so as to move the field of coverage of each radiating element in the same direction.

First claim

The invention claimed is:

1. A multiple-input multiple-output imaging radar system, comprising:
a plurality of transmission channels, each transmission channel being configured to apply a phase coding in such a way that orthogonality is obtained between the transmission channels in a burst of transmitted pulses;
a plurality of reception channels;
a plurality of co-located radiating elements forming a two-dimensional antenna array, each radiating element being able to be fed by one of the transmission channels and/or being able to feed one of the reception channels, each radiating element having a predefined instantaneous field of coverage;
characterized in that each radiating element is formed by a plurality of p radiating sub-elements distributed in at least one of the two dimensions of the antenna array,
the radar comprising a plurality of electronic steering modules, each electronic steering module being connected between a radiating element and one among the transmission channels or reception channels, each steering module being configured to apply a steering command between all the radiating sub-elements of a given radiating element, the steering command being identical from one radiating element to the next, so as to move the field of coverage of each radiating element in the same direction,
wherein the steering command comprises a phase gradient applied between the various radiating sub-elements, said phase gradient being based on the number of sub-elements per radiating element.

2. The multiple-input multiple-output imaging radar system according to claim 1 , wherein each electronic steering module comprises:
a divider or a combiner, connected to the transmission channel or to the reception channel, respectively, and
a plurality of phase shifters, each phase shifter being connected to one of the radiating sub-elements of the radiating element.

3. The multiple-input multiple-output imaging radar system according to claim 1 , wherein each electronic steering module comprises a plurality of amplifying means, each amplifying means being connected to one radiating sub-element.

4. The multiple-input multiple-output imaging radar system according to claim 1 , wherein the phase gradient corresponds to a constant angular difference, selected from the following values: 0 ; ±π/4, ±π/2, ±π/4; ±π, wherein π is a mathematical constant which is the ratio of a circle's circumference to its diameter.

5. The multiple-input multiple-output imaging radar system according to claim 1 , wherein the radiating elements are placed on an antenna panel, the radiating elements occupying an area of at least 50% of the antenna panel.

6. The multiple-input multiple-output imaging radar system according to claim 1 , wherein the radiating sub-elements are placed in the azimuthal dimension and in the elevation dimension of the 2D array.

7. The multiple-input multiple-output imaging radar system according to claim 1 , wherein p equals 2 or 4.

8. The multiple-input multiple-output imaging radar system according to claim 1 , comprising a calibration table, configured to compensate, for each steering command, steering errors between the transmission channels and/or between the reception channels, produced by the electronic steering modules.

9. The multiple-input multiple-output imaging radar system according to claim 1 , configured to operate in millimeter band.

10. An aircraft, comprising the multiple-input multiple-output imaging radar system according to claim 1 , wherein the system comprises a computer configured to change the steering command depending on a difference between the heading and the route of the aircraft.

11. The aircraft according to claim 10 , wherein the steering command is recomputed at a rate comprised between 10 and 15 Hz.

12. Method for controlling a multiple-input multiple-output imaging radar system, the method comprising the following steps:
transmitting a radar signal over a plurality of transmission channels each transmission channel being configured to apply a phase coding in such a way that orthogonality is obtained between the transmission channels in a burst of transmitted pulses;
receiving the radar signal over a plurality of reception channels following reflection or backscatter from a target;
the transmission channels and reception channels feeding and/or being fed, respectively, by a co-located set of radiating elements forming a two-dimensional antenna array, so as to obtain a predefined instantaneous field of coverage for each of the radiating elements,
characterized in that each radiating element is formed by a plurality of p radiating sub-elements distributed in at least one of the two dimensions of the antenna array, the method further comprising the following step:
applying a steering command between all the radiating sub-elements of a given radiating element, the steering command being applied by an electronic steering module, said electronic steering module being connected between a radiating element and one among the transmission channels or reception channels, the steering command being identical from one radiating element to the next, so as to move the instantaneous field of coverage of each radiating element in the same direction,
wherein the steering command comprises a phase gradient applied between the various radiating sub-elements, said phase gradient being based on the number of sub-elements per radiating element.

13. The method according to claim 12 , comprising a calibrating step, in which the following sub-steps are implemented:
measuring phase and/or amplitude errors between the field of coverage of a radiating element for a given steering command, with respect to the centre of the theoretical shifted scanning field of each radiating element;
determining calibration coefficients depending on the measured phase and/or amplitude errors;
storing the calibration coefficients in a table called a calibration table specific to the steering command.

Assignees

• Thales Sa

Inventors

• Veyrac Yoan
• Cornic Pascal
• Le Gall Renan
• Bertin De La Hautiere Gonzague

Classifications

• H01Q3/36

  with variable phase-shifters · CPC title

• G01S2013/0263

  Passive array antenna · CPC title

• G01S13/913 Primary

  for landing purposes · CPC title

• G01S13/89 Primary

  for mapping or imaging · CPC title

• Y02A90/10

  Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation · CPC title