法国专利FR3052870A1 SECONDARY RADAR WITH OPTIMIZED SPATIO-TEMPORAL MANAGEMENT

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专利摘要:
Since the secondary radar is equipped with an active or semi-active electronic scanning antenna covering the 360 ° azimuth space, the radar: - is mechanically independent of the primary radar; - applies the principles of separation ○ of emission and reception diagram; ○ assignment of tasks specific to it to separate bodies; - includes a first IFF interrogator (91) dedicated to both SSR surveillance and the collection of new Mode S targets; - furthermore includes one or more other selective monitoring IFF interrogators (92, 93) dedicated to Mode S monitoring and directed IFF identification queries; - simultaneously receiving responses to said interrogators (91, 92, 93) in different azimuths, said simultaneous reception being allowed when the azimuthal spacing of the beams formed in reception provides a decoupled level of at least 10 dB of interference between the expected responses by the respective sidelobes of the three beams formed in reception; control of the interrogators to ensure between them the temporal separation of the reception periods when the spacing of the beams in azimuth is insufficient to guarantee the detection.
公开号:FR3052870A1
申请号:FR1600982
申请日:2016-06-21
公开日:2017-12-22
发明作者:Philippe Billaud
申请人:Thales SA；
IPC主号:

专利说明:

Secondary Radar
OPTIMIZED SPATIAL-TEMPORAL MANAGEMENT
The present invention relates to a secondary radar with optimized spatio-temporal management, the radar being equipped with an active or semi-active electronic scanning antenna.
A mechanical rotating antenna secondary radar must in particular meet the following simultaneous requirements: - Ensure a high refresh rate of the target position leading to decrease the rotation period; - Perform many tasks with the cooperating targets according to the different protocols (surveillance task in SSR mode and Mode S or identification in Mode 4/5) at each antenna revolution, which leads to an increase of the lighting time on each target, therefore to increase the required illumination time per target and thus to an increase in the rotation period of the antenna.
These two simultaneous requirements are contradictory. In practice, the management in space and time of the radiation of a secondary antenna (spatio-temporal management) is a compromise giving preference to a task, (surveillance or identification in particular), according to the primary mission of the radar.
Conventionally, the antennas of a secondary radar are mechanically secured to the primary antenna.
The sequencing of the radar is divided into two parts: - SSR monitoring periods comprising sub-periods called "Ail Call" (AC) where it takes at least three to five sub-periods in the same mode to extract the codes. These same periods also serve as collection periods for new planes interrogated in Mode S. - Mode S periods comprising at least three to five sub-periods called "Roll Call" (RC) for transactions with Mode S targets.
During the AC periods, the radar transmits an SSR interrogation and a general call mode S interrogation at the beginning of the period and then waits for the rest of the period for the possible responses of the SSR targets and the new Mode S targets on the azimuth of the antenna. The listening period necessarily corresponds to the instrumented distance of the radar below which a new target can appear.
During the RC periods, the radar issues selective interrogations for each of the known Mode S targets (already detected and put on track) that are present at this azimuth. The targets being pre-localized in azimuth and distance by the tracking of the radar, the selective interrogations are positioned so that neither the interrogations nor the answers overlap. Unlike listening periods in AC, listening periods in CR are much shorter since they are limited to the duration of the expected Mode S response plus the uncertainty in the target distance prediction (see figure 1).
In practice, while the standby phase that constitutes the AC period is necessary, for the collection of new targets and for the surveillance of the SSR targets, according to the density of Mode S targets in the beam, the RC periods, according to the density of Mode S targets in the beam at a given azimuth, may be unused or otherwise insufficient in duration. Spatio-temporal management of the antenna beam is therefore not optimal.
This non-optimality can be explained in a very simple way: up to now, the so-called secondary radar function has been considered as an accessory of the so-called primary radar which has to adapt a posteriori to the aerial of the primary radar. This hierarchical and successive top-down approach required the principle of mechanical scanning with a single, focused diagram: the architecture thus deduced the limitations that go with it. The invention assumes that another design vision is possible where the secondary radar is first specifically designed (bottom up approach on the best way to perform the required functions) then comes the adaptation to the primary radar. Of course, the so-called primary radar and the so-called secondary radar form a system, to be conceived globally and simultaneously, which will ultimately lead to combining the two approaches to arrive at a compromise. Also the purpose of the invention is not only to improve the spatio temporal management of the secondary radar, but to introduce a concept as autonomous as possible of the functions called secondary.
The search for autonomy in the design of the so-called secondary radar functions will go through the satisfaction of fundamental independence requirements vis-à-vis the subsystem constituted by the so-called primary radar. Thus, the first element of independence will be to overcome the enslavement to the mechanical rotation of the antenna subsystem constituted by the so-called primary radar. It will then be sought additional degrees of freedom that will be obtained by separating the transmission function of the reception function.
Then, the application of these principles of autonomy will lead to different physical architectures of antennas associated with different emission regimes and different principles of beam formation on reception.
These elements of approach system will constitute the base of autonomy from where, consequently, a system architecture will be able to be built which will naturally sublimate the compromise undergone by the spatio-temporal management in the classic case by affecting quite naturally the different tasks, previously contradictory, with multiple elements as well for the interrogations as for the receptions.
Once the principles of conceptions are established and unfolded, it is then possible to envisage realizations of application in physical classes, as described in the paragraph below.
The antennas are: - Either by fixed antennas with electronic scanning: they can be cylindrical or consist of several fixed panels (the orientation of the market goes to a number of 4 to 6 fixed panels); - Or by rotating antennas with a panel.
At the microwave level, the electronic scanning antennas can be classified according to three main types: - Either passive emission: the transmission and the reception are centralized outside the antenna itself (conventionally as it is the case of rotating antennas); - Either semi-active type transmission: the emission is centralized outside the antenna and reception is distributed in the antenna itself: - Either active type transmission: the transmission and reception are distributed in the antenna.
An electronic scanning and passive transmitting antenna forms the beam and directs the energy in transmission and reception in a direction of space from or to an IFF interrogator. Once the IFF tasks are done in this direction, the beam is switched in another direction. By construction, a passive emitting electronic scanning antenna remains single beam. As a result, it can only transmit and receive at a given moment in one direction.
As a result, the passive emitting electronic scanning antennas are confronted with the same compromise as the antennas with mechanical rotation between refresh rate and the illumination time per target.
In the case of an electron-beam antenna with an active type emission, a transmission and reception function is associated with each radiating element to make it possible to transmit IFF interrogations simultaneously, for example in two different directions. When the receiving antenna has a beamforming by the calculation (FFC), it is then possible to simultaneously receive in all directions the responses of the targets to the interrogations previously issued, by forming the analog reception beam (FFA) or by calculation (FFC).
It is therefore understood that, in order to overcome the complete compromise between refresh rate and target illumination time faced by the mechanical rotation antennas and, in a more general manner, the emission-patterned electronic scanning antennas. and of identical reception, it is therefore necessary to have a distributed emission part with radiating emission elements and secondly, radiating reception elements with beam forming on reception. Thanks to this double condition, spatio-temporal management can be freed from the azimuthal pointing constraint of the beam and focus on the only temporal dimension.
It then becomes possible to improve the spatio-temporal management (GST), allowing in particular to distinguish: - The monitoring tasks on non-manageable targets in distance, such as the new targets SSR or Mode S; - Mode S surveillance and identification tasks pre-located in distance and azimuth.
These different tasks are assigned to different interrogators. For this purpose, the subject of the invention is a secondary radar equipped with an electronic scanning antenna with an active or semi-active emission regime, covering the 360 ° azimuth space, characterized in that said radar: is mechanically independent of the primary radar; - applies separation principles O of transmission and reception diagram; O assignment of tasks specific to it to separate bodies; - includes a first IFF interrogator dedicated to both SSR surveillance and the collection of new Mode S targets; - furthermore includes one or more other selective monitoring IFF interrogators dedicated to Mode S monitoring and directed IFF identification queries; - simultaneously receiving responses to said interrogators in different azimuths, said simultaneous reception being allowed when the azimuthal spacing of the beams formed in reception ensures a decoupled level of at least 10 dB of interference between the responses expected by the respective side lobes the three beams formed in reception; control of the interrogators to ensure between them the temporal separation of the reception periods when the spacing of the beams in azimuth is insufficient to guarantee the detection.
In a particular embodiment, the first interrogator dedicated to both the SSR monitoring and the collection of new Mode S targets, informs said interrogators, dedicated to mode S monitoring and directed interrogations, of the detection of a new target. said new target being then managed by said interrogators, at least one of said interrogators controlling the pointing of its transmission beam and of its reception beam in the direction of said target since the aforementioned simultaneous reception authorization is acquired. For example, the operator defines for each target the refresh rate he wants for the IFF monitoring / identification regardless of the azimuth of the detected target and decorrelated from the previous day.
To accelerate SSR monitoring, said radar may comprise at least one other SSR monitoring IFF interrogator, independent of said first interrogator (91), having an associated beam pointing in another direction than that of the beam associated with said first interrogator (opposite for another IFF interrogator, in quadrature for three other IFF interrogators).
When the transmission regime is of the active type, a supervisory device is for example provided to allow simultaneous interrogations in sufficiently distinct azimuths, taking into account the beam formed, to avoid the blocking of the transponders and in that, when the If the transmission is of the semi-active type, the common transmission resource can be allocated in priority to the IFF interrogator n ° 1, then to the other interrogators.
Said antenna is for example cylindrical.
Said antenna is for example constituted by panels each of which is associated with at least one IFF interrogator.
It can be fixed or rotating. Other characteristics and advantages of the invention will become apparent with the aid of the following description made with reference to the appended drawings which represent: FIG. 1, SSR monitoring sequences and selective interrogations in a radar with mechanical rotation ; FIG. 2 is a perspective view of an example of a cylindrical secondary antenna with electronic scanning; FIG. 3, an illustration of the operation of a cylindrical passive scanning electron antenna; FIG. 4, a representation of antenna gains for three successive pointing directions; FIG. 5, an illustration of the operation of a cylindrical antenna with active electronic scanning; FIG. 6, an illustration of the spatio-temporal management principle of the antenna beams in a semi-active electronic antenna radar according to the invention; FIG. 7, SSR monitoring sequences and selective interrogations in a radar according to the invention comprising two IFF interrogators; FIG. 8, an illustration of the operation of the antenna beams in a radar according to the invention comprising three IFF interrogators; FIG. 9, SSR monitoring sequences and selective interrogations in a radar according to the invention comprising three IFF interrogators; FIG. 10, an example of implementation of space-time management in a semi-active emission electron antenna radar according to the invention. FIG. 11, an example of implementation of spatio-temporal management in a radar with active emission electronic antenna with 4 fixed panels; FIG. 12, an example of implementation of spatio-temporal management in an active electron antenna radar with 1 rotating panel;
Although the figures take the semi-active emission electronic scanning antenna as an example, the principles of the invention are even more applicable to the active emission electron scanning antenna since it also allows simultaneous transmissions,
Figure 1 shows the conventional sequencing of an IFF interrogator associated with mechanical rotation. The GST is followed by time periods AC 11 and RC 12 at the azimuth at which the antenna points. The GST selectively interrogates in the RC period the Mode S targets that it thinks are present at this azimuth in the antenna beam.
Therefore, when, in its progressive progression in azimuth, the beam no longer illuminates the Mode S target it will have to wait for an antenna revolution to continue the Mode S transactions.
FIG. 2 presents, in perspective view, an example of a cylindrical electronic scanning antenna antenna 1 fitted to a radar 10. The invention could also be applied to an electronic antenna composed of flat panels, for example four in number, covering the 360 ° azimuth space.
FIG. 3 illustrates the operation of a passive type electronic antenna. In this case, a centralized single power amplifier prepares the interrogation. A switching matrix 25, for example a centralized Butler matrix, makes it possible to control the position of the transmission power on the periphery of the antenna by means of a phase law applied to the input of the matrix. Receiving control is also centralized via the Butler matrix. The latter is interfaced with an IFF interrogator 24 producing the SSR and Mode S interrogations and decoding the return responses.
The basic operation of a cylindrical fixed-scan passive electronic scanning antenna is to simulate a mechanical antenna rotation to evenly distribute the illumination time over the entire coverage. At a given moment, the cylindrical antenna uses P radiating elements 21 to form the beam in a given azimuth θη. Once the SSR or Mode S monitoring tasks have been carried out, the antenna pointer is shifted by N radiating elements and the antenna beam is reformed in another azimuth θη + ι from another set 22 of P elements shifted relative to the first set 21. And so on with another set 23 of P elements to form a beam in another direction θη + 2 ·
FIG. 4 shows the antenna gains 31, 32, 33 as a function of time for three successive azimuth positions θη, θη + ι, θη + 2. Thus, in each beam position, the GST performs a sequencing of the following type: Figure 1. Two types of beam management are possible: - either the beam advances at constant azimuthal speed, as for a mechanical rotation antenna, thus guaranteeing an identical refresh rate in all the azimuths but not guaranteeing the execution of all mode S transactions due to lack of time; - or the beam is maintained at a given azimuth the time required to set the number of periods AC and RC required to provide SSR and Mode S monitoring or for an identification IFF Mode 4 or Mode 5 but then the refresh rate is not more constant and it completely depends on the number of aircraft and associated transactions.
The sequencing of the passive type electronic antenna is thus the same as that of a mechanical antenna. Indeed, the switching of the antenna beam from one azimuthal position to another requires the switching of power elements. At each switching the RF transmission is interrupted. It is therefore more efficient to do all RF transactions at a given azimuth before changing the beam positioning.
With such an antenna, the radar remains a compromise between: - The simulated antenna rotation speed (refresh rate); The range of the radar, guaranteed by the gain of the antenna at the level of the gain taps 34 (speed of displacement of the beam in azimuth); - The maximum number of aircraft per sector manageable in Mode S; - The number of mode S transaction by aircraft.
FIG. 5 illustrates the principle of an active type emission electron scanning antenna in the case of a cylindrical antenna which associates with each radiating element 40: a transmission function 401 adjustable in power level and in phase; - A reception function 402.
This type of active type transmit antenna thus makes it possible simultaneously: in transmission 44, to transmit interrogations via a transmission bus 41, in sufficiently different directions, so that the first interrogation is not perceived by the target to which it is not intended to avoid its blocking, that is to say, sufficiently spaced in azimuth depending on the secondary lobes of the beam thus formed using P radiating elements 43, the emission beam being formed by forming beam by calculation 44 (FFC); - In reception 45, receive responses, via a receive bus 42, simultaneously on several other azimuths, following previously transmitted interrogations, exploiting by beam formation all the radiating elements of the fixed cylindrical antenna.
An active-type electronic scanning antenna thus makes it possible to fully exploit the characteristics of the S mode in the sense that the selectivity of the interrogations as responses makes it possible to select one of several targets at a given azimuth.
Another type of electronic scanning antenna is the semi-active type transmitting antenna, which represents a simplified version of an active type transmit antenna. In particular: - It comprises a centralized emission function performing a formation of the beam and switching to P radiating elements; - A reception function is associated with each radiating element.
A semi-active type emitter electron scanning antenna thus simultaneously makes it possible to: - transmit a single interrogation in a single azimuthal direction; - Receive responses, via the receive bus 42, simultaneously on several other azimuths, following previously transmitted interrogations exploiting by beam formation all the radiating elements 40 of the antenna.
Like the passive type transmit antenna, the semi-active type transmitting antenna only allows transmission in a single azimuth and the switching of the emission from one azimuth to another is slow enough because the switching of strong signals. Nevertheless, for both the active-type transmit antenna and the semi-active type transmit antenna, the separation of the transmit and receive beams offers the possibility of a complete spatio-temporal management of the IFF function.
FIG. 6 illustrates the principle of the invention, which proposes a new spatio-temporal management (GST), different from that of antennas with mechanical rotation or electronic scanning with non-active type emission, in the sense that it distinguishes: monitoring tasks on targets that can not be managed remotely (SSR surveillance or new Mode S targets); - Surveillance tasks (mode S) and IFF identification (designation on primary track) pre-located in distance and in azimuth.
FIG. 6 shows an exemplary embodiment, in the case of a semi-active type electronic transmission antenna, based on two medium power IFF interrogators 51, 52 connected to a power amplifier device 53 associated with a formation. the beam and its switching to the P radiating elements 54, 55, the device 53 switching on one or the other IFF interrogators. In this configuration: - The first interrogator (IFF interrogator n ° 1), is dedicated to SSR surveillance and the collection of new Mode S targets; - The second interrogator (IFF interrogator n ° 2) can be switched from a surveillance opposite to TIFF n ° 1 (in the background spot in the absence of the following tasks) towards: - IFF identifications according to a window depending on the position the target defined by the primary radar; - Selective mode S transactions.
The reception being permanent over 360 °, the FFC makes it possible to form beams in different azimuthal directions 56, 57 simultaneously and thus allow a simultaneous listening in several azimuth mode S responses.
In the example of FIG. 6, TIFF No. 1 provides SSR monitoring at a given azimuth, while TIFF No. 2 simultaneously provides Mode S monitoring at another azimuth.
FIG. 7 illustrates an example of a GST ensuring a succession of the monitoring sequences with the method according to the invention, more particularly the SSR monitoring N followed by the SSRn ° N + 1 monitoring. This example corresponds to the case of Figure 6 based on the use of two IFF interrogators. FIG. 7 shows the sequence of the interrogation periods 61, 63 and periods dedicated to the responses 62, 64 in given azimuths where these are indicated by a sequence number 1, 2, 3, 4 corresponding to the azimuth predicts referenced targets. In SSR surveillance N: - The IFF interrogator n ° 1 provides azimuthal monitoring at azimuth 0 in the conventional modes, SSR and Mode S in particular; The IFF interrogator n ° 2 can: - either ensure, in the other azimuths 1, 2, 3, 4 ..., the management of the tracks referenced in distance azimuth, in IFF or mode S, almost without latency; - In the absence of these, ensure, in the azimuth opposite to azimuth 0 (+ 180 °), an azimuth monitoring opposite TIFF No. 1 to acquire new targets.
For TIFF # 1, since the targets are unknown, the listening periods 62, dedicated to the responses, are long and are also a function of the instrumented distance. The duration of a monitoring at a given azimuth depends on the number of SSR modes to be interrogated and decoded. All azimuths must be covered one after the other. After SSR monitoring No. N, IFF interrogator No. 1 points to another azimuth, the azimuth 10 in the example of FIG.
The choice of a single interrogator, IFF No. 2, to manage the transactions at different azimuths nevertheless requires ensuring the non-overlap of the responses 64, to allow the successful decoding of the response as shown in the sequences of FIG. .
Figure 8 shows an implementation of the more elaborate invention where a third IFF interrogator, IFF # 3, is added. This figure shows at the same time the three antenna beams 71, 72, 73 on the periphery of the antenna, corresponding to the three interrogators IFF No. 1, IFF No. 2 and IFF No. 3.
This configuration makes it possible in particular to temporally overlap responses to different azimuths to ensure separation in azimuth, according to the antenna beam formed with the P elements, and thus to ensure the successful decoding of the two simultaneous responses respectively by IFF n. ° 2 and IFF No. 3. This is applicable even in the case of a semi-active type emitting electronically scanned antenna, a single transmitting beam may be created at a given time while several simultaneous receiving beams are possible.
FIG. 9 shows the successions of interrogation and listening periods corresponding to a configuration with three IFF interrogators, as illustrated by FIG. 8. In this representation, the notations by sequence numbers, azimuth 0 or 10 and azimuth 1 , 2, 3 ..., mean that these azimuths are sufficiently spaced, with distinct main lobes, to allow the simultaneous reception of signals from different targets without causing overlapping responses, which would result in non-detection by garbling. More specifically, with reference to FIG. 8, an angle ΔΘ between two beams 72, 73 must remain above a minimum value in order to avoid overlaps. Conventionally, a detection is obtained when the signal-to-jammer ratio is greater than 10 dB. As a result, the GST defines the angle ΔΘ by calculating the level of interference received by a secondary lobe of the adjacent beam and the target targeted by this beam. Similarly, with reference to FIG. 4, the maximum difference between two standby beams, azimuth 0 and azimuth 10 in the example of FIG. 9, is defined by the expected minimum gain corresponding to the overlap 34 of their radiation diagrams. . The standby beam step between azimuths therefore depends on the beam and the desired range. We can thus discretize the azimuthal space and point a series of azimuths to cover all the space, in standby and almost independently in interrogation / response transactions.
Thus, the watch still guaranteed at constant azimuthal speed is decorrelated from the monitoring Mode S / IFF identification designated, these being now carried out on a time basis only, both independently by aircraft and decorrelated from the previous day.
The watch makes it possible to locate the targets, by the IFF interrogator No. 1. A target being located, the transactions can then be done by the other two interrogators, and more generally on the other interrogators in a configuration comprising more than three interrogators. The invention thus makes it possible to manage, in time and in space, the movement of the beams 71, 72, 73 and the triggering of the interrogations and the responses and thus to optimize the different tasks as a function of the available time, by playing on the beam agility offered by an active or semi-active electronic transmitting antenna.
To do this, an antenna pattern manager has a time-managed interface for setting the start time, the end time of the beam in a given azimuth for each interrogator.
The interrogations 61, 63 emitted by the transmission beam can not be superimposed in the case of a semi-active type transmission. On the other hand, responses 62, 64 may be overlaid in time due to the fact that multiple receive beams may be produced simultaneously. It is thus possible to perform several IFF reception in parallel with a single antenna which simplifies the constraints of the GST. Indeed, before, it was necessary to guarantee a total non-overlapping of the answers since these were in the same azimuth.
According to the method according to the invention, an IFF radar in an electronic antenna version with a semi-active or active type of transmission can therefore achieve optimal spatial and temporal management, in particular: the refresh rate of the SSR monitoring can to be at its optimum, considering that it is carried out by a single interrogator, the IFF interrogator n ° 1, because this task 61, 62 has priority and is now decorrelated from the mode S surveillance or directed interrogations (DI), its acceleration can be envisaged by adding another interrogator dedicated to the SSR monitoring, denoted IFF n ° Ibis, managing an azimuth opposite to IFF n ° 1 - the refresh rate of the mode S surveillance or directed interrogations (DI) can also be at its optimum since it is possible in all directions, avoiding those in the course of SSR monitoring to limit pollution, as needed functional.
FIG. 10 illustrates a possible implementation of spatio-temporal management in a radar according to the invention, equipped with a transmitting electronic scanning antenna of the active or semi-active type. In this example, three IFF interrogators 91, 92, 93 are used. It is of course possible to provide embodiments with a higher number of interrogators (from 2 to N). A first interrogator 91, IFF interrogator No. 1 is assigned to SSR monitoring, the other interrogators 92, 93, IFF interrogators No. 2 and IFF interrogator No. 3, are mainly assigned to transaction tasks (mode S and DI monitoring for IFF identification).
This example is also presented with a cylindrical electronic antenna 1 with semi-active type emission. The antenna is cylindrical, but other types of configurations are possible provided that the antenna covers 360 °. The antenna may also consist of several panels of radiating elements, four for example as shown in Figure 11. A supervisor 90 coordinates the IFF interrogators. In particular, it defines 901 the IFF monitoring tasks of the interrogator No. 1 allowing an operator to define according to the azimuth the nature of the monitoring tasks to be done. It defines the IFF modes, the identi- fication IFF standby in a given azimuthal sector, the power and the standby sensitivity in particular.
According to the 902,903 availabilities of the interrogators n ° 2 and n ° 3, the supervisor distributes 904, 905: - the selective interrogations mode S with the transactions mode S associated with each target, either periodically, or as a result of external requests; - directed interrogations for IFF identification according to requests external to the IFF radar; these interrogations being performed according to the target refresh rate desired by the operator for each of the detected targets. From now on, the service rendered by the IFF radar is operated on a time base that the operator defines for each target according to the level of interest that it carries to him.
Likewise, a new Mode S target detected during surveillance 906 is very rapidly confirmed by a selective interrogation, thus delivering to the operator as soon as it is detected all the Mode S information required 907, 908 as Mode S targets, in particular the identification flight or the capacity of the data links.
Each of the IFF interrogators 91, 92, 93 requires access to a transmission resource by specifying the transmit azimuth 941, 942, 943 and providing the sum and control signals 911, 921, 931 to be transmitted. For this purpose, the antenna 1 being a semi-active emission type, a centralized amplifier 94 provides the power required for transmission. The sum and low level control signals are transmitted to the amplifier via a switch 97, switching one or the other of the interrogators to the amplifier. The signals are amplified and the sum Σ and control Ω beams are calculated (FFC) by beamforming means 95. At a given instant the amplified signals calculated by the beamforming means 95 are transmitted via a matrix of switching 44, to the groups of Q radiating elements, to form a beam pointing in the required azimuth 941, 942, 943.
In reception, the beams respectively assigned to the interrogator No. 1, the interrogator No. 2 and the interrogator No. 3 can be formed in parallel. Each interrogator therefore independently requires the formation in parallel of a reception beam, from P radiating elements, for the sum signals Σ, the difference signals Δ and the control signals Ω in its required azimuth 961, 962, 963. The beams are received by the receiving and processing means 96. A FFC, calculating the beams Σ, Δ, Ω is assigned to each interrogator. The signals 961 ', 962', 963 'from the FFCs are transmitted to their respective interrogators.
The standby and interrogation sequences produced by the system of FIG. 10 are, for example, the sequences illustrated in FIG. 9.
FIG. 11 shows the application of this spatio-temporal management principle to the case of a non-cylindrical fixed antenna, it is here a fixed panel antenna equipped in this mimic of a single IFF interrogator per panel. In this example, while the top panel provides SSR monitoring and the collection of new Mode S targets, the side and bottom panels simultaneously provide 2 mode S transactions and directional identification at other azimuths.
Figure 12 shows the application of this spatio-temporal management principle to the case of a plane rotating antenna consisting of a single panel. In this example, the IFF interrogator n ° provides SSR monitoring and the collection of new mode S targets, while the IFF interrogator n2 successively performs a mode S transaction and a directed identification at 2 other azimuths than the previous day. performed by the IFF processor n ° ^. Again, this antenna configuration although lighter than that in Figure 11, therefore certainly less powerful, nevertheless allows to limit the constraint brought by the rotation of the antenna both by decorrelating: - SSR monitoring and collection new Mode S targets, allocated to the No. 1 processor and the antenna orthogonal beam, - Mode S transaction management and directed identification allocated to the No. 2 processor and the deflected beams thus providing azimuthal independence on the width of the beam deflection area.
The principle of spatio-temporal management of the IFF interrogations in a radar according to the invention, illustrated in particular by FIG. 10, may be described in particular, in whole or in part, by the characteristics below, advantageously using the fact that the less the reception can be simultaneous for the different interrogators in independent azimuths: a first IFF interrogator 91, for example TIFF No. 1, is dedicated both to the SSR monitoring and to the collection of new mode targets S; one or more IFF interrogators 92, 93, for example the IFF interrogators n ° 2 and n ° 3, are dedicated to the mode S surveillance and the IFF identification directed interrogations (DI), originating from the primary or secondary radar tracks. or any other location means, each interrogator performing the decoding of its mode S or DI responses by ensuring the placement in time of the selective interrogations or DI to avoid the overlap of its responses; the receptions of the 3 interrogators can be authorized simultaneously when the azimuth spacing of the beams generated during reception ensures a low level (> 10 dB) of interference between the responses expected by the respective sidelobes of the 3 beams; the interrogator IFF n ° 1 of collection of new targets mode S informs the other interrogators of selective surveillance 92, 93, IFF n ° 2 and n ° 3, during the detection of a new target which is then managed by l one of them, in particular at least one interrogator 92, 93 controls the pointing of its reception beam in the direction of the detected target. By way of example, with reference to FIG. 8, a target being detected in the transmission beam 71 of the interrogator No. 1, the receiving beam 72 of the interrogator No. 2 is then switched in the the response of the transmission beam 71 when the level of the sidelobes of the new position of the beam 71 so permits, it would be possible to switch the receiving beam 73 of the interrogator No. 3 in the same direction. the direction of the transmission beam 71, this being dependent on the respective working load of the interrogators 72 and 73; - SSR monitoring can be accelerated, ie the increased refresh rate, by allocating additional IFF No. 1 dedicated to SSR monitoring with independent beams, when using two independent interrogators. beams that can be opposed (+ 180 °) whereas with four interrogators the beams can be in quadrature (+ 90 °) leading to a rate of the SSR monitoring respectively two to four times faster than with a single interrogator; in the case where the transmission regime of the antenna 1 is of the semi-active type, the common transmission resource 94 can be allocated in priority to the IFF interrogator No. 1, then to the other interrogators, IFF interrogator No. 2 and IFF interrogator No. 3 in the example of FIG. 10, thus giving priority to SSR monitoring since it transmits infrequently; in the case where the transmission regime of the antenna 1 is of the active type, a supervisory device can be provided to allow simultaneous interrogations in sufficiently distinct azimuths, taking into account the beam formed, to avoid the blocking of the transponders , by ensuring a lower level (> 10dB) of residual interrogations by the sidelobes. In addition to the advantages provided by a secondary electronic scanning antenna (notably the elimination of motors and rotary joints), the invention advantageously allows independence of the "SSR monitoring and new Mode S target acquisition" phase and the "monitoring" phase. Selective Mode S or IFF Directed ID ". It also advantageously allows the suppression of sectoral surcharges since the selective transactions (mode S or DI monitoring) can be maintained the time necessary to the desired azimuth without penalizing the other tasks. Significant functional gain is achieved by removing virtually all sectoral load limit problems. From now on, the service rendered by the IFF radar is operated on a time base that the operator defines for each target according to the level of interest that it carries to him almost without azimuthal constraint.

权利要求:
Claims (9)
[1" id="c-fr-0001]
1. Secondary radar equipped with an electron scanning antenna (1) with an active or semi-active emission regime, covering the 360 ° azimuth space, characterized in that said radar: - is mechanically independent of the primary radar ; - applies separation principles O of transmission and reception diagram; O assignment of tasks specific to it to separate bodies; - includes a first IFF interrogator (91) dedicated to both SSR surveillance and the collection of new Mode S targets; - furthermore includes one or more other selective monitoring IFF interrogators (92, 93) dedicated to Mode S monitoring and directed IFF identification queries; - simultaneously receiving (71, 72, 73) responses to said interrogators (91, 92, 93) in different azimuths, said simultaneous reception being allowed when the azimuthal spacing of the beams formed on reception provides a decoupled level of less than 10 dB of interference between the responses expected by the respective side lobes of the three beams formed in reception; control of the interrogators to ensure between them the temporal separation of the reception periods when the spacing of the beams in azimuth is insufficient to guarantee the detection.
[2" id="c-fr-0002]
2. Secondary radar according to claim 1, characterized in that the first interrogator (91) dedicated to both the SSR monitoring and the collection of new mode S targets, informs said interrogators (92, 93), dedicated to monitoring mode S and directed interrogations, of the detection of a new target, said new target then being managed by said interrogators (92, 93), at least one of said interrogators controlling the pointing of its emission beam and of its reception beam in the direction (71) of said target as soon as the aforementioned simultaneous reception authorization is acquired.
[3" id="c-fr-0003]
3. Secondary radar according to any one of the preceding claims, characterized in that the operator defines for each target the refresh rate that he wishes for monitoring / IFF identification regardless of the azimuth of the detected target and of unconnected way of the day before.
[4" id="c-fr-0004]
4. Secondary radar according to any one of the preceding claims, characterized in that, to accelerate the SSR monitoring, said radar comprises at least one other SSR monitoring interrogator SSF independent of said first interrogator (91), having an associated beam pointing in a direction other than that of the beam associated with said first interrogator (91), opposite in the case of use of a single other IFF interrogator or in quadrature in the case of use of three other IFF interrogators.
[5" id="c-fr-0005]
5. Secondary radar according to any one of claims 1 to 3, characterized in that, when the transmission regime is of the active type, a supervisory device is provided to allow simultaneous interrogations in sufficiently distinct azimuths, taking into account of the formed beam, to avoid the blocking of the transponders and in that, when the transmission regime is of semi-active type, the common transmission resource (94) can be allocated in priority to the IFF interrogator No. 1 , then to the other interrogators.
[6" id="c-fr-0006]
6. Secondary radar according to any one of claims 1 to 3, characterized in that said antenna (1) is cylindrical.
[7" id="c-fr-0007]
7. Secondary radar according to any one of claims 1 to 3, characterized in that said antenna (1) is constituted by panels to each of which is associated with at least one IFF interrogator.
[8" id="c-fr-0008]
8. Radar according to any one of the preceding claims, characterized in that said antenna is fixed.
[9" id="c-fr-0009]
9. Radar according to any one of claims 1 to 7, characterized in that said antenna is a rotating antenna.

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JP2019521332A|2019-07-25|

ES2887252T3|2021-12-22|

EP3472641A1|2019-04-24|

EP3472641B1|2021-07-21|

WO2017220461A1|2017-12-28|

FR3052870B1|2018-06-15|

US10823838B2|2020-11-03|

US20190146078A1|2019-05-16|

引用文献:

公开号 | 申请日 | 公开日 | 申请人 | 专利标题

EP0497652A1|1991-01-31|1992-08-05|Agence Spatiale Europeenne|Device for the electronic control of the radiation pattern of a single or multi beam antenna with variable direction and/or width|

FR2680581A1|1991-05-09|1993-02-26|Toshiba Kk|Secondary surveillance radar system|

EP2259085A1|2009-06-05|2010-12-08|Thales Nederland B.V.|An apparatus for sharing an omnidirectional antenna between an IFF transponder and an IFF interrogator|

JP2011176512A|2010-02-24|2011-09-08|Nec Corp|Active phased array antenna device|

EP2911240A1|2014-02-21|2015-08-26|Thales|IFF antenna system|

EP2930531A1|2014-04-11|2015-10-14|Thales|Secondary surveillance radar with high refresh rate|

US5955990A|1997-12-16|1999-09-21|Raytheon Company|Linear interferometer antenna capable of making error-free azimuth and elevation angle measurements|

US8703113B2|2004-07-08|2014-04-22|Reva Medical Inc.|Side-chain crystallizable polymers for medical applications|

US9658325B2|2014-07-31|2017-05-23|James Francis Harvey|Secondary surveillance radar signals as primary surveillance radar|

IL242004A|2015-10-11|2021-08-31|Israel Aerospace Ind Ltd|Identification friend or foe system and method|CN109901150B|2019-03-04|2021-01-26|四川九洲空管科技有限责任公司|Multifunctional phased array radar device and detection method thereof|

RU2742944C1|2020-05-12|2021-02-12|Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации|System for determining coordinates of target|

RU2742945C1|2020-05-12|2021-02-12|Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации|Method of determining coordinates of target in request-response system|

法律状态:
2017-05-30| PLFP| Fee payment|Year of fee payment: 2 |

2017-12-22| PLSC| Publication of the preliminary search report|Effective date: 20171222 |

2018-05-29| PLFP| Fee payment|Year of fee payment: 3 |

2020-05-26| PLFP| Fee payment|Year of fee payment: 5 |

2021-05-27| PLFP| Fee payment|Year of fee payment: 6 |

优先权:

申请号 | 申请日 | 专利标题

FR1600982A|FR3052870B1|2016-06-21|2016-06-21|SECONDARY RADAR WITH OPTIMIZED SPATIO-TEMPORAL MANAGEMENT|

FR1600982|2016-06-21|FR1600982A| FR3052870B1|2016-06-21|2016-06-21|SECONDARY RADAR WITH OPTIMIZED SPATIO-TEMPORAL MANAGEMENT|

JP2018563730A| JP7005529B2|2016-06-21|2017-06-19|Secondary radar with optimized spatiotemporal management|

ES17730186T| ES2887252T3|2016-06-21|2017-06-19|Secondary radar with optimized space-time management|

PCT/EP2017/064875| WO2017220461A1|2016-06-21|2017-06-19|Secondary radar with optimized spatio-temporal management|

EP17730186.8A| EP3472641B1|2016-06-21|2017-06-19|Secondary radar with optimized spatio-temporal management|

US16/302,062| US10823838B2|2016-06-21|2017-06-19|Secondary radar with optimized spatio-temporal management|

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