Patent Application
20230417893
The invention relates to the field of active antenna radar systems, and more particularly radar systems designed to cover a given solid angle with a high angular discrimination. The invention is notably applicable for Doppler radar systems on moving platforms, for example radar systems allowing the visualization of runways on a commercial aircraft, performing a function of EVS (acronym for Enhanced Vision System) or else automobile radar systems for anti-collision or imaging functions designed for autonomous vehicles.
One problem to be addressed is to display a virtually instantaneous image with high angular resolution of the scene present in the whole of the field of view of a radar, while at the same time limiting the digital processing requirements to enable this function and while reducing the complexity and the cost of such a radar. This capacity is particularly advantageous on a carrier which is moving at a high speed with respect to the scene to be observed, or when the scene is itself rapidly changing, or even when these two conditions occur simultaneously.
In such cases, the refreshment time must be reduced which requires the number of orientation directions of the antenna to be reduced in order to cover the whole of the angular field. In practice, the angular field to be processed is often very wide, typically several tens of degrees, whereas the focusing requirement imposes a narrow elementary beam, typically with a width of less than one degree, which increases the difficulty of defining a solution that is both simple and effective.
In the prior art, in order to achieve the desired result, the conventional solutions of the mechanical scanning type implementing a narrow beam for scanning the field of observation are not suitable because of the cycle time needed in order to refresh the information. Moreover, this type of solution often presents a lack of reliability over time, in particular when the scanning speed needs to be high.
A second very common type of radar is based on antennas using electronic scanning, in one or two dimensions. These antennas require a large number of phase-controlled radiating elements in order to produce both a good resolution and a wide angular coverage. Unfortunately, these solutions are often very expensive and maladapted for applications requiring moderate costs.
The solutions based on beam formation by computation, implementing a transmission by a single wide-field antenna and a multichannel array antenna in reception, allow an instantaneous observation of the angular field but suffer from a low discrimination, due to the lack of selectivity of the transmission antenna, and are likely to need a high power emitter in view of the low antenna gain at the transmission.
Other solutions, of the type “with multiple inputs and outputs” referred to as MIMO (acronym for Multiple Input Multiple Output), associating several transmission channels and several reception channels, are possible. In this case, there are N transmission channels and M reception channels, and the elementary transmission power can remain modest. However, the radar processing must be applied to all of these N×M channels, which may entail an extremely high processing load, in particular for a real-time application. This processing load is all the higher the larger the number of orientation directions of the beam. This may be out of reach for reasons of cost, of integration and of power consumption.
The patent application FR1910613 discloses a solution based on a radar with active antenna in which a focusing of the transmission antenna is carried out in a different direction from transmission pulse to pulse with a formation of at least one reception beam in the direction of focusing of the transmission for each pulse emitted. This solution allows, at the same time, a virtually instantaneous image of the scene of observation to be produced, the angular discrimination objective to be achieved and the processing load to be very significantly reduced with respect to a solution based on MIMO processing. It is applicable to an antenna with a conventional AESA (acronym for Active Electronically Scanned Array) architecture or MIMO. It may be implemented using a low power technology at the transmission and standard electronic components.
The patent application FR2004262, which is based on the same principles, provides an alternative which allows, as a complement, the speed of the targets to be determined when the radar is ambiguous in Doppler mode.
In order to reduce the cost and the complexity, these solutions according to the prior art are preferably implemented by means of thinned antenna arrays exhibiting ambiguities. This may decrease the observable angular field or may necessitate complex processing operations in order to remove these ambiguities. Furthermore, the refreshment time of the data and the processing load may be significant owing to the large number of different angular orientations needed for the transmission to cover the whole of the angular field with a low-divergence focused beam.
One aim of the invention is notably to overcome these drawbacks of the prior art and to solve the aforementioned technical problem. For this purpose, the subject of the invention is a radar with ambiguous electronic scanning allowing a given angular field to be covered. The electronic scanning radar comprises an active antenna comprising an array of elementary transmission antennas and an array of elementary reception antennas with the same angular opening, said transmission and reception arrays having the same radiation plane, in which:
This configuration allows the coverage of said given angular field by said radar to be obtained in the following manner:
Advantageously, the radar is configured for covering the given angular field:
In other words, the angular coverage of the given angular field by the radar is obtained:
In one particular embodiment:
Advantageously, the coverage of said given angular field is obtained:
Advantageously, the radar is configured for covering the angular field in the manner described in the preceding paragraph.
Advantageously, residual ambiguity lobes are rejected by Doppler filtering.
Advantageously, residual ambiguity lobes are rejected by selectivity in distance.
In one embodiment, said active antenna is of the type active array with electronic scanning.
In another embodiment, said active antenna is of the type with multiple inputs and outputs.
The invention also relates to a method of electronic scanning of a given angular field using a radar with ambiguous electronic scanning according to the invention. In the method according to the invention, the given angular field is covered:
Advantageously, the radar used has the following features:
In the method, the given angular field is advantageously covered:
Advantageously, residual ambiguity lobes are rejected by Doppler filtering.
Advantageously, residual ambiguity lobes are rejected by selectivity in distance.
Other features and advantages of the invention will become apparent with the aid of the description that follows, presented with regard to the appended drawings which show:
A radar system according to the invention is based on an active antenna architecture, which may be an antenna with conventional electronic scanning of the AESA (Active Electronically Scanned Array) type or an antenna of the MIMO type.
In the AESA structure illustrated in
In the MIMO structure illustrated in
A radar according to the invention comprises hardware and processing features.
As regards the hardware, a radar according to the invention is based on an active antenna using an ambiguous array, whose angular coverage is provided within a field Δθ by electronic scanning or MIMO processing notably exhibiting the following features:
As regards the processing, the coverage of the angular field is subsequently obtained within the angular field Δθ:
Advantageously, the radar is configured for this purpose. Advantageously, the electronic scanning method using the radar according to the invention implements the steps previously described implemented so as to cover the angular field.
Finally, the residues of angular ambiguities linked to the product of the ambiguous transmission and reception radiating patterns are eliminated by a Doppler processing allowing the directions of arrival of the echoes coming from the targets or from the fixed radar clutter to be separated.
The radar is advantageously configured for this purpose and the scanning method advantageously comprises this step.
The array thus formed allows a given angular field ΔΘ to be covered with a reduced number of antenna orientation control states at the transmission. Thus, for a given angular resolution ΔΘr, corresponding to the length of the antenna array L, such that ΔΘr=(λ/NTX).LTX, with a conventional angular scanning, a minimum number of antenna orientations would be needed at the transmission Np=ΔΘ/ΔΘr in order to cover the whole of the field ΔΘ.
According to the invention, this number is reduced by a factor NambTX, corresponding to the number of ambiguous beams at the transmission contained in the opening ΔΘ of the elementary antenna.
Furthermore, at least two angular directions are observable simultaneously at reception for the same transmission orientation command. In the case of an electronic scanning, this allows the refreshment time to be decreased, which is able to compensate for a part of the losses of the antenna array due to the fact that it is a thinned array. In the case of MIMO processing, this allows the processing load to be reduced.
These hardware aspects and these processing operations according to the invention are now described, first of all with regard to a linear array (
Thus formed, when the transmission and reception orientations are aligned in the direction orthogonal to the antenna plane, taken as reference at θ=0°, the arrays TX and RX each form focused and ambiguous radiating patterns, according to
The angular opening 44 of an elementary antenna at 3 dB surrounding the reference 0° is also shown, here included between −5.7° and +5.7°. Within this antenna angular opening, there are:
The product of the transmission radiating pattern 42 and of the reception radiating pattern 43, in this configuration, exhibits an unambiguous single lobe, in the direction 0°, according to the representation in
It is recalled here that, for the transmission, the beam is oriented in a direction given according to a phase law, in a known manner, whereas for the reception a digital processing operation is carried out. The digital processing in reception is also well known and corresponds to a complex weighting of phases where a numerical sum of the received signals is carried out, each received signal being assigned a phase. The weighting determines the orientation of the beam in reception, 0° for example in the case of
The radiating pattern resulting from the product of the transmission and reception radiating patterns exhibits a main lobe corresponding to the coincidence of the transmission radiating pattern and of the reception radiating pattern, whose respective orientations are obtained as described hereinabove. The product illustrated in
In both cases, by the product of the transmission and reception radiating patterns, a radiating pattern is obtained comprising a main lobe 61, 62 in the direction of coincidence of the transmission and reception array functions respectively at −5.6° and +5.6° and a residual secondary lobe 63, 64 in the opposite direction, with a lower level. The main lobes 61, 62 are limited by the square of the antenna radiating pattern 60.
Thus, for the same orientation direction in transmission, it is possible to simultaneously form reception beams 51, 61, 62 in three different directions, potentially with residual ambiguous lobes 63, 64. These beams may be formed simultaneously because, as has previously been recalled, the beams in reception are formed by computation and, for the same orientation direction of the transmission beam, may be calculated in parallel (hence simultaneously). In the exemplary application in
Other orientation solutions for transmission and for reception TX/RX are illustrated in
Each configuration of transmission orientation TX intermediate between the direction 0° and the direction corresponding to the limit of the field of ambiguity TX, in the same way, allows three main beams to be generated by multiplication of the array radiating patterns TX and RX, with residual lobes that are larger or smaller depending on the combination of orientation TX with respect to RX. In the present example, three beams are generated starting from the three ambiguous transmission beams; a different number of beams may of course be generated depending on the number NambTX of ambiguous beams comprised within the antenna opening.
These principles may be applied to a two-dimensional array antenna, comprising several transmission lines and several reception lines.
In particular, in one application of the EVS type, ambiguous antenna arrays may be used once in azimuth and in elevation, and the same methods applied in the two planes, which decreases even more the number of beams to be formed at the transmission.
In order to reduce the residual ambiguity lobes obtained by transmission beam TX formation and by reception beam RX formation, the radar according to the invention uses Doppler processing, for example by integrating the received signals from recurrence to recurrence by numerical Fourier transform according to the methods known to those skilled in the art.
Indeed, on a carrier moving at the speed Vp, the Doppler frequencies Fd corresponding to the fixed echoes are different depending on the directions of arrival with respect to the path of the carrier, according to the relationship
where Θ is the angle between the direction of movement of the carrier and the direction of arrival of the fixed echoes.
The variation of the Doppler frequency as a function of the angle Θ is given by:
for small angles, where Θ is expressed in radians.
According to the invention, this property is exploited in order to reduce the residual ambiguous lobes by virtue of Doppler filtering. In particular, for a radar operating in the millimeter wave range, the Doppler frequencies are high and the angular separation by the Doppler technique is possible, even for low angles.
For example, considering a carrier moving at a speed Vp equal to 60 m/s and a wavelength λ of 3 cm, we obtain:
An angular variation of 1°, i.e. 17 mrd, then produces a variation in Doppler frequency at small angles of the order of 70 Hz.
Thus, in a typical configuration where the Doppler integration time is of the order of Ti=50 ms, the Doppler resolution of the radar is: ΔFd=1/Ti=20 Hz, and two echoes angularly separated by 1° are separable.
The elimination of the ambiguity lobe residues is obtained by selecting as useful signal the output of the Doppler filter corresponding to the direction of the main beam resulting from the product of the radiating patterns for transmission TX and for reception RX. This requires the knowledge of the speed Vp of the carrier and of the boresight direction of the antenna. The speed Vp of the carrier may be estimated by an inertial navigation system or by the radar itself, for example according to the principles described in the patent application FR2004262. The boresight direction of the antenna is furthermore known, the radar being rigidly attached to the carrier. The field of the signals retained as useful may be extended as needed to a few filters around the direction of the main beam, depending on the uncertainties in the estimations.
Lastly, in the case of an airborne radar providing the EVS function using an ambiguous array in elevation, the rejection of the residues of the ambiguity lobes in elevation may be further reinforced by virtue of the selectivity in distance of the radar, the glide slope of the aircraft α, typically 3°, the altitude H and the tilt of the antenna being known. The tilt of the antenna being the orientation of the antenna beam with respect to the horizontal, in this context it is accordingly deduced at which distance the beam will reach the ground, the undesirable distances corresponding to undesirable angles. These angles, and hence the corresponding directions, may then be filtered.
The altitude of the carrier may be estimated for example by the onboard altimeter, or by the radar itself using the return of the ground echoes according to the methods known to those skilled in the art. The distance from a point on the ground corresponds to an angle of elevation Θel with respect to the horizontal, where Θel=arctan(D/H), D being the distance estimated by the radar. It is possible to establish an estimation of Θel by the estimation of the distance of the point targeted and of the altitude of the aircraft. Depending on the distance slot processed by the radar, only the detections whose elevation angular measurements are close to the primary estimation of Θel, are validated.
The preceding examples show that, by advantageously exploiting the ambiguities of an antenna array, a radar system according to the invention can cover a given angular field ΔΘ with a reduced number of antenna orientation control states at the transmission. Thus, for a given angular resolution ΔΘr, corresponding to the length of the antenna array L, such that ΔΘr=(λ/NTX).LTX, with a conventional angular scanning, a minimum number of antenna orientations at the transmission Np=ΔΘ/ΔΘr would be required in order to cover the whole of the field ΔΘ.
For a radar system according to the invention, this number is reduced by a factor NambTX, corresponding to the number of ambiguous beams at the transmission contained within the opening ΔΘ of the elementary antenna. Referring to the example in
Furthermore, at least two angular directions are observable simultaneously in reception for the same transmission orientation control, as is illustrated for example in
| Number | Date | Country | Kind |
|---|---|---|---|
| 2010279 | Oct 2020 | FR | national |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/EP2021/075204 | 9/14/2021 | WO |
