The present invention relates to a method and system for emitting and receiving laser pulses.
Although not exclusively, a system for emitting and receiving laser pulses, as considered, may form part of a high-frequency laser telemeter that is in particular intended to be used in various applications in the space field.
Such a laser telemeter may, in particular, be used for implementing laser trajectography or laser telemetry on a satellite of the SLR. (standing for Satellite Laser Ranging) type. The great increase in debris in orbit and the development of threats are spurring on the development of optical means, in particular active optical means of the laser trajectography type, in order to know very precisely the orbits of space objects (satellites, debris).
Moreover, another possible application of a system for emitting and receiving laser pulses, at high frequency, is to implement a laser communication link between a ground station and a drone (or an object or craft in orbit) using a modulated retroreflector technology. To do this, provision is made, in the ground station, for the laser system intended to emit a laser beam in order to illuminate a retroreflector mounted on the drone (or on the object or craft in orbit). This retroreflector is designed to modulate the reflected intensity. It is constructed (in the form of a cube corner or a spherical reflector for example) so that the laser beam is reflected exactly in the same direction as that of the laser beam received. The modulation is detected and processed by the system on the ground.
Other applications are also possible for such a system for emitting and receiving laser pulses.
For these applications, by emitting low-energy laser pulses (less than 1 mJ), which is limited for safety reasons, the difficulty is being able to process the signals, because of ratios between the return signals and noise, which are extremely small.
Usually, single pulses of medium energies (greater than 0.1 mJ) are emitted. However, if it is attempted to increase the firing rate, the spatial resolution of the measurement is degraded, or even impossible if firing is carried out continuously at high frequency (more quickly than the round-trip time of the pulses).
The object of the present invention is to remedy these drawbacks by proposing a method for emitting and receiving laser pulses making it possible to increase the firing rate (and thus the probability of detection).
According to the invention, said method for emitting and receiving laser pulses includes at least the following steps:
Advantageously, the analysis step consists in deducing, from the sequence of pulses identified, a so-called reception time at which the first pulse in said sequence of pulses identified is received, and calculating the duration between said emission time and said reception time.
Thus, by means of the invention, it is possible to differentiate from each other the pulses in a set formed by a plurality of pulses by defining (timewise) the durations between, on each occasion, two successive pulses in order to make them unique within the set of pulses, in accordance with said pattern of pulses. It is possible consequently to emit sets (or packets) of pulses (in the form of a so-called burst emission mode), knowing that it is possible to identify the reception of the set of (returned) pulses, and in particular to determine the reception time at which the first pulse in said set of (returned) pulses is received.
This makes it possible in particular to increase the probability of detection by increasing the number of pulses, therefore using a set (or packet) of pulses instead of a single pulse.
The method for emitting and receiving laser pulses thus makes it possible, in particular, to reduce the energy of each laser pulse emitted (for example to 10 μJ), to distribute this energy in a plurality of laser pulses (forming the set of pulses) and to sign these laser pulses timewise (in accordance with the pattern of pulses). This makes it possible to emit at a higher firing rate in order to improve the probability of detection, while keeping great precision of emission in the case in particular of telemetry, and maintaining low average energy, which is favourable to ocular safety.
In a preferred embodiment, the analysis step consists in determining, by means of said duration between the emission time and the reception time, a distance between a station comprising the emitting/receiving unit and an object (or target) receiving the laser pulses emitted and returning them.
In a variant or as a complement, advantageously, the analysis step consists in analysing at least one set of pulses emitted and the corresponding sequence of pulses received, issuing for example from a modulation and a retroreflection, in order to deduce information therefrom, for example in the context of a laser link communicating with a drone or an object in orbit in space.
Moreover, advantageously, the analysis step consists in making a correlation between said pattern of pulses and the light pulses received on a correlation window in order to identify the sequence of light pulses received, which is in accordance with said pattern of pulses.
Preferably; the emission step consists in emitting, successively, a plurality of sets of pulses. Advantageously, the duration between two sets of pulses emitted successively is greater than a duration of round-trip movement of a set of pulses between a station comprising the emitting/receiving unit and an object receiving the laser pulses emitted and returning them.
Furthermore, in a particular embodiment, the generating step consists in generating at least two different patterns of pulses and the emission step consists in emitting a plurality of successive sets of pulses that are in accordance with different patterns of pulses; generated at the generating step.
The present invention also relates to a system for emitting and receiving laser pulses, including an emitting/receiving unit.
According to the invention, said system for emitting and receiving laser pulses includes:
Advantageously, said memory is configured also to record a so-called emission time, at which the first pulse in the sequence of laser pulses in said set of laser pulses emitted by the emitting/receiving unit is emitted.
Furthermore, advantageously, the data processor unit is also configured:
Moreover, advantageously; said system for emitting and receiving laser pulses also includes at least one filtering unit configured to perform at least one frequency filtering of the light pulses received, in relation to the frequency or frequencies of the laser pulses emitted.
The present invention further relates to a laser telemeter and/or a communication system, including a system for emitting and receiving laser pulses as described above.
The accompanying figures will give a clear understanding of how the invention can be implemented. On these figures, identical references designate similar elements. More particularly:
This system 1, which is mounted on a station 2, installed for example on the ground, can be used in numerous applications, as indicated above. The system 1 may also be mounted on a land, sea or air vehicle (not shown).
The system 1 includes an emitting/receiving unit 3. The emitting/receiving unit 3 comprises, as shown in
According to the invention, said system 1 also includes, as shown in
In the context of the present invention, a pattern of pulses comprises, as shown for a pattern of pulses M1 in
Two directly successive pulses in the pattern of pulses are in each case separated in time by an associated separation duration, namely, in the example in
The various separation durations T1, T2 and T3 of the patterns of pulses M1 and M2 are variable, that is to say different from one another, and in accordance with a given model (of separation durations), that is to say each separation duration is equal to a particular duration. The pattern of pulses therefore represents a (time) signature of the pulses in question.
The emitting module 4 of the emitting/receiving unit 3 is configured to emit at least one set of pulses EI1 comprising a sequence of laser pulses, in accordance with the pattern of pulses in question, as shown in
In addition, the receiving module 6 of the emitting/receiving unit 3 is configured to receive light pulses ILi (
This object 9 is preferably an object that is movable in the sky, for example a drone or a satellite (or any other object) in orbit. This object 9 may be situated at a great distance from the station 2, for example at several tens of kilometres from the station 2.
The system 1 also includes, as shown in
In a preferred embodiment, as shown in
The system 1 further includes a data processing unit 12. The data processing unit 12 comprises, as shown in
To do this, the processing element 13 is configured to make a correlation between the pattern of pulses M2 used and the light pulses ILi received, on a correlation window F, in order to identify the sequence of light pulses received, which is in accordance with said pattern of pulses M2, as shown in
To make the correlation, the pattern of pulses M2 (with four pulses in this example) is moved, as illustrated by the arrow A in
Thus the system 1 is able to differentiate from each other the pulses in a set EI1 of a plurality of pulses by defining (timewise) the durations between, in each case, two successive (or consecutive) pulses in order to make them unique within the set of pulses EI1, in accordance with the pattern of pulses M1, M2 used.
Consequently the system 1 can emit sets (or packets) EI1 of pulses (in the form of a so-called burst emission mode), knowing that it will be able to identify the reception of the set of pulses emitted (and returned); and in particular to determine the reception time at which the first pulse in said set of pulses thus identified is received.
This makes it possible in particular to increase the probability of detection by increasing the number of pulses emitted, through the use of a set (or packet) EI1 of pulses instead of a single pulse.
Furthermore, the data processing unit 12 also includes, as shown in
This duration T0 can be used to deduce therefrom various items of information and in particular to make a calculation of distance. To do this, in a preferred embodiment, the data processing unit 12 includes a processing element 15. This processing element 15 is configured to calculate, in the usual fashion; by means of this duration T0 between the emission time tE, and the reception time tR (received from the processing element 14), taking into account the speed c of light, the distance D0 between the station 2 comprising the emitting/receiving unit 3 and the object 9 that received the laser pulses emitted and returned them (
In a variant or as a complement of the processing element 15, the data processing unit 12 includes a processing element 16. This processing element 16 is configured to analyse at least one set of pulses EI1 emitted and the corresponding sequence of pulses (received). This sequence of pulses results, for example, from a modulation and a retroreflection implemented on the object 9. From this analysis, the processing element 16 is able to deduce, in a usual fashion, various items of information. This particular embodiment can, for example, be used in the context of a laser communication link between the station 2 and the object 9, for example a drone or an object in orbit in space.
The duration of firing TR (between two sets of pulses EI1 emitted successively) is greater than a duration of round-trip movement of a set of laser pulses between the station 2 comprising the emitting/receiving unit 3 and the object 9 receiving the laser pulses emitted 1.0 and returning them. By way of illustration, this duration of round-trip movement may be between 1 and 5 milliseconds.
The data processing unit 12 can transmit the results of its processing operations, for example the distance calculated by the processing element 15 and/or the information deduced by the processing element 16, to a user system (not shown) via a connection 19.
Moreover, in a particular embodiment, the generating unit 7 is configured to generate at least two different patterns of pulses, and the emitting module 4 is configured to emit a plurality of sets of successive pulses that are in accordance with these different patterns of pulses, generated by the generating unit 7. In this particular embodiment, the processing operations performed by the data processing unit 12 are similar to the aforementioned ones, taking account simply of the difference between the patterns of pulses used.
Moreover, in a particular embodiment (shown in
The system 1 also includes at least one filtering unit 18 preferably forming part of the emitting/receiving unit 3. The filtering unit 18 is configured to perform filterings, and at least one frequency filtering, of the light pulses detected by the receiving module 6, in order to keep (with a view to processing thereof by the data processing unit 12) only the light pulses detected that have frequencies situated in domains defined around the frequency or frequencies of the laser pulses emitted by the emitting module 4.
The system 1 (for emitting and receiving laser pulses), as described above, is highly advantageous. In particular, it makes it possible to reduce the energy of each laser pulse (for example to 10 μJ), to distribute the energy in a plurality of laser pulses (forming the set of pulses EI1) and to sign these pulses timewise (in accordance with the pattern of pulses in question, for example M1 or M2). This makes it possible to emit at a higher firing rate TR in order to improve the probability of detection, while keeping the required precision in the case of telemetry, and maintaining a low average energy of the laser pulses emitted, which is advantageous in terms of ocular safety.
Furthermore, it is possible to increase the resolution by increasing the number of pulses and/or by reducing the size of the correlation window F.
The system 1 as described above is able to implement a method for emitting and receiving laser pulses at high frequency.
This method for emitting and receiving laser pulses includes, as shown in
The analysis step E4 also consists in deducing, from the sequence of pulses thus identified, a so-called reception time tR at which the first pulse I1 in said sequence of pulses identified is received, and calculating the duration T0 between said emission time tE and said reception time tR.
In a preferred embodiment, the analysis step E4 consists in determining, by means of the duration T0 (thus calculated) between the emission time tE and the reception time tR, a distance D0 between the station 2 comprising the emitting/receiving unit 3 and the object 9 that received the laser pulses emitted and that returned them.
In a variant or as a complement, the analysis step E4 may consist in analysing at least one set of pulses emitted and the corresponding sequence of pulses received, resulting for example from a modulation and a retroreflection, in order to deduce therefrom information, for example in the context of a laser communication connection.
Numerous applications are possible for such a system 1 (for emitting and receiving laser pulses), equally well land, sea and/or air (or space) applications, with in particular transmissions at great distances (greater than ten kilometres).
According to a first application, the system 1, as described above, forms part of a high-frequency laser telemeter (not shown) that can be employed in various uses in the space field. In this application, the telemeter uses in particular the distance between the (measuring) station 2 and the object 9, as determined by the processing element 15 of the processing unit 12.
Such a laser telemeter can, in particular, by used for implementing laser trajectography via laser telemetry on a satellite (of the SLR type, standing for Satellite Laser Ranging), in particular in order to very precisely determine the orbits of space objects (satellites, debris).
Moreover, in another possible application, the system 1 (for emitting and receiving laser pulses) is used for effecting a high-frequency laser (communication) connection between the station 2, for example on the ground, and an object 9; for example a drone, using modulated-retroreflector technology. To do this, the system 1 illuminates a retroreflector mounted on the object 9. This retroreflector is designed to modulate the reflected intensity. It is produced, for example, in the form of a cube corner or a spherical reflector, so that the laser pulse returned is reflected exactly in the same direction as that of the laser pulse received. The modulation is detected and processed by the system 1, for example by means of the processing element 16, in order to deduce therefrom the corresponding information.
The system 1 can also be used, in another application, to implement the active locking of targets at very long distance.
Number | Date | Country | Kind |
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1800272 | Apr 2018 | FR | national |
Filing Document | Filing Date | Country | Kind |
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PCT/FR2019/050719 | 3/28/2019 | WO | 00 |