• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    A method of multibeam coverage of a region of the earth's surface comprising: - generating, by an on-board telecommunications payload on a satellite, a plurality of radio frequency beams, called elementary beams (FE1, FE2, FE4); the formation of a plurality of radiofrequency beams, called composite (FC ") beams, having footprints of different sizes, each said composite beam being obtained by grouping together one or more elementary beams, and the emission or receiving data through said composite beams, identical data being transmitted or received through all the elementary beams forming the same composite beam.
    公开号:FR3076138A1
    申请号:FR1701345
    申请日:2017-12-21
    公开日:2019-06-28
    发明作者:Pierre Bosshard；Didier Le Boulc'H
    申请人:Thales SA；
    IPC主号:
    专利说明:

    MULTI-BEAM COVERING METHOD BY GROUPING BASIC BEAMS OF THE SAME COLOR, AND TELECOMMUNICATIONS PAYLOAD FOR IMPLEMENTING SUCH A COLOR
    The invention relates to the field of satellite telecommunications. More particularly, it relates to a method for producing multi-beam coverage of a region of the earth's surface, as well as to a telecommunications payload, intended to be carried on a satellite, allowing the implementation of such a method.
    The search for high transmission capacities in satellite communication systems requires the use of multi-beam antennas to produce so-called "multibeam" covers of a region of interest on the earth's surface. Such coverage is in the form of a juxtaposition of geographically distinct, contiguous or non-contiguous individual covers, generally of circular or elliptical shape and corresponding to the footprints on the ground of different beams generated by a telecommunications satellite. It should be noted that the term "beam" can cover two distinct realities: when we consider a downlink, we are actually talking about beams of electromagnetic radiation propagating from the satellite to the ground; in the case of an uplink, on the other hand, the term "beam" indicates a lobe of the reception diagram of the satellite antenna system.
    Multibeam covers generally allow the reuse of the frequency according to a so-called "N-color" scheme. According to such a scheme, in order to avoid interference, two adjacent beams have a different "color", each "color" corresponding to a frequency-polarization state pair.
    The disparity in data traffic needs between different parts of the region of interest can be very large; it is therefore necessary to vary the size of the beams serving these different parts. Thus, it is usual to use thin beams with minimum angular opening in areas with high user density, and wide beams with large angular opening in areas with low user density. For example, Figure 1 shows a multibeam coverage of Australia with very wide beams in sparsely populated areas in the center and north and much finer beams in the coastal regions of the southwest and southeast. East.
    In a satellite adapted to provide multi-beam coverage, the beams are generally generated by antenna systems comprising source antennas (or simply "sources"; these are generally horns or sets of horns) and reflectors. Typically, each source antenna generates a respective beam, while the same reflector can contribute to the generation of several distinct beams. The size of a beam depends on both the characteristics of the source antenna and those of the reflector; in addition, a reflector is optimized for a source having certain characteristics. In practice, different sources can generate beams of slightly different size using the same reflector, but the mismatch between source and reflector quickly becomes problematic. Consequently, in order to be able to generate a multi-beam cover comprising beams of very different sizes (ratio between the surfaces of the footprints on the ground which may reach, or even exceed, a factor of 4) it is necessary to use several different reflectors. This leads to complex and expensive antenna systems.
    Furthermore, large beams have much less steep emission diagram slopes than more directive beams; in other words, their intensity decreases more gradually as they move away from the center of the beam. Consequently, the "tails" of large beams tend to interfere with the smaller beams. The invention aims to remedy, in whole or in part, at least one of the aforementioned drawbacks of the prior art. More particularly, the invention aims to enable multi-beam coverage to be achieved by means of a simpler and more easily industrializable antenna system, and / or to minimize interference between beams. Certain embodiments of the invention also make it possible to obtain greater flexibility in the definition of the beams.
    An object of the invention, making it possible to achieve these goals, is therefore a method of multi-beam coverage of a region of the earth's surface comprising: the generation, by a telecommunications payload on board a satellite, of a plurality of radiofrequency beams, called elementary beams (FE1, FE2, FE4); the formation of a plurality of radiofrequency beams, called composite beams (FC ’, FC”), having footprints of different sizes, each said composite beam being obtained by grouping one or more elementary beams; and the transmission or reception of data through said composite beams, identical data being transmitted or received through all the elementary beams forming a single composite beam; wherein at least one said composite beam is formed by grouping a plurality of non-adjacent elementary beams of the same color, a color being defined by a frequency band and a polarization state.
    Advantageously, the method comprises the introduction of a phase shift between at least two of said elementary beams of the same color.
    Advantageously, said phase shift is a phase inversion.
    As a variant, said phase shift is a phase quadrature setting.
    Advantageously, a plurality of said elementary beams has footprints on the ground of substantially identical size.
    Advantageously, all of said elementary beams have footprints on the ground of substantially identical size.
    Advantageously, the footprints on the ground of said composite beams have sizes which vary progressively across said region of the earth's surface.
    Advantageously, all the elementary beams forming the same composite beam are generated at the same time.
    As a variant, all the elementary beams forming the same composite beam are generated in turn. The invention also relates to a satellite telecommunications payload for the implementation of a predefined method comprising: a plurality of source antennas (S1 - S4); at least one reflector (R) arranged to cooperate with said source antennas so as to generate a radiofrequency beam, called elementary beam, for each said source antenna; and a plurality of transmit or receive modules (MTRA, MTRb) configured to transmit or receive respective data in the form of radio frequency signals; each said source antenna belongs to a group of source antennas, at least some of said groupings comprising a plurality of source antennas; each said transmission module is connected to all the source antennas belonging to the same grouping, so that the elementary beams generated by the source antennas of the same grouping form a composite beam; said groups of source antennas being configured so that a plurality of said composite beams have footprints of different sizes; and the elementary antennas of at least one said array are configured to generate non-adjacent elementary beams of the same color, a color being defined by a frequency band and a polarization state
    Advantageously, a phase shifter (ΏΦ) is arranged between at least one elementary antenna of at least one said array configured to generate non-adjacent elementary beams of the same color and the corresponding transmission or reception module.
    Advantageously, said or each said phase shifter is a phase inverter.
    Advantageously, said or each said phase shifter is configured to effect a 90 ° phase shift.
    Advantageously, said groups of source antennas are configured so that all of said elementary beams have footprints on the ground of substantially identical size.
    Advantageously, at least one said transmitting or receiving module is equipped with a switch configured to connect said module to the corresponding elementary antennas in turn. Other characteristics, details and advantages of the invention will emerge on reading the description made with reference to the accompanying drawings given by way of example and which represent, respectively:
    FIG. 1, described above, the multibeam coverage of a region having a highly variable user density; FIGS. 2A to 2C, an embodiment of a multibeam cover; and FIG. 3, a telecommunications payload according to an embodiment of the invention.
    A basic principle of the invention consists in covering the region of interest with fine beams of identical size - or at most having a reduced number (for example 2 or 3) of different sizes - which can be combined together , in particular in areas of less dense traffic, to generate wider "composite" beams. Thus, the beams of larger dimensions are not generated by dedicated reflectors or by sources unsuited to the size of the reflectors, but by combining fine elementary beams. This has several advantages compared to the prior art: the antenna system is much simpler and modular, since it can consist only of identical sources and a small number of reflectors, also identical to each other; the slopes of the diagrams remain steep even for larger beams, minimizing interference; there is greater freedom in the choice of the shape of the composite beams; moreover, a composite beam can result from the combination of non-contiguous elementary beams which, as will be explained below, allows greater flexibility in the allocation of spectral and / or power resources.
    FIGS. 2A to 2C illustrate two variants of a multibeam cover in which three non-adjacent elementary beams of the same color, FE1, FE2 and FE4 - whose iso-intensity curves are illustrated in FIG. 2A - are combined to form a composite beam designated by FC 'in Figure 2B and by FC ”in Figure 2C. As in the previous case, this means that the same data pass through these three elementary beams, in order to serve regions - geographically separated from each other - with low traffic density. The FC ’and FC’ composite beams are obtained very simply by connecting the corresponding source antennas to the same power amplifier (in transmission) or low noise (in reception). In the case of FIG. 2B, the elementary beams of the same color are summed in phase (so-called power summation). In the case of FIG. 2C, on the other hand, a 90 ° phase shifter is introduced between this amplifier and the source antenna of the elementary beam FE2, and a 180 ° phase shifter is introduced between this amplifier and the source antenna of the elementary beam EF4. As can be seen by comparing Figures 2B and 2C, the phase opposition between the beams FE1 and FE4 produces field cancellation between the beams FE1 and FE4. The phase quadrature of the beams FE1 and FE2, and also of the beams FE2 and FE4, also makes it possible to concentrate the electromagnetic intensity in the regions which must actually be covered, by steepening the slope of the radiation diagram of the composite beam, without qu 'there is total field cancellation as is the case in phase opposition. The three elementary beams interfere with each other because they are the same color, even if these interferences are moderate due to the spatial separation between beams. The introduction of such phase shifts loses its interest when the elementary beams are so far apart that their interference becomes negligible.
    More complex configurations, associating several beams - and if necessary with different phase differences of 90 ° and 180 ° between them - are of course possible.
    It is also possible to produce composite beams combining non-adjacent elementary beams of different colors.
    Forming "unconnected" composite beams from non-adjacent elementary beams can be beneficial from a resource management perspective. In fact, in a composite beam, several distinct geographic regions share the same resources: frequencies, power, or even transmission time, as will be explained below. If these regions are distant from each other, their meteorological conditions will be uncorrelated: if, for example, the region covered by the elementary beam FE1 is in conditions of strong attenuation due to a thunderstorm, the attenuation will probably be less in the regions covered by FE2 and FE4. It will therefore be possible to allocate more resources to FE1 without degrading the service offered by FE2 and FE4 too much. In the case of adjacent beams, this is more difficult due to the high correlation between weather conditions between nearby regions. If the elementary beams are very far from each other, it will even be possible to take advantage of a time difference between the corresponding regions, by removing resources from the beams covering regions in “off-peak hours” in favor of those forming part of the same composite beam and covering regions in "peak hours".
    Until now, we have only considered the case where data is passing at the same time through all the elementary beams of the same composite beam, these elementary beams sharing the frequency and power resources allocated to the composite beam. As a variant, it is possible to activate in turn the various elementary beams of the same composite beam, by means of a switch arranged in the payload of the satellite. Thus, each elementary beam uses - but only for a fraction of time - all of the available resources.
    FIG. 3 illustrates, very schematically, the structure of a telecommunications payload, on board a satellite, enabling multi-beam coverage as described above. Such a payload, given solely by way of nonlimiting example, includes:
    Two transmission or reception modules - MTRa and MTRb to generate the signals to be transmitted via respective composite beams (in transmission) or to acquire the signals received by these beams (in reception). Each transmission or reception module comprises at least one power and / or low noise amplifier.
    Four source antennas S1 - S4 (electromagnetic horns) each intended to generate a respective elementary beam.
    A reflector R cooperating with the source antennas to generate said beams.
    In reality, an antenna system according to the invention typically includes several reflectors and a much higher number of source antennas.
    The MTRA module is connected to three source antennas S1, S2, S3 to produce a “non-connected” composite beam, of the type of FIGS. 2A to 2C. A phase shifter D <D is disposed between the module and the source antenna S3.
    Finally, the MTRb module is connected to a single source antenna, S4, to produce a fine “composite” beam, consisting of a single elementary beam.
    Note that the antenna system of the payload shown in Figure 3 only includes source antennas identical to each other, cooperating with a single reflector (or identical reflectors). It is therefore a simpler and more modular structure than that of a conventional multibeam antenna system, comprising source antennas and / or reflectors of different sizes.
    权利要求:
    Claims (15)
    [1" id="c-fr-0001]
    1. A method of multibeam coverage of a region of the earth's surface comprising: the generation, by a telecommunications payload on board a satellite, of a plurality of radiofrequency beams, called elementary beams (FE1, FE2, FE4); the formation of a plurality of radiofrequency beams, called composite beams (FC ’, FC”), having footprints of different sizes, each said composite beam being obtained by grouping one or more elementary beams; and the transmission or reception of data through said composite beams, identical data being transmitted or received through all the elementary beams forming a single composite beam; wherein at least one said composite beam is formed by grouping a plurality of non-adjacent elementary beams of the same color, a color being defined by a frequency band and a polarization state.
    [2" id="c-fr-0002]
    2. Method according to claim 1 comprising the introduction of a phase shift between at least two of said elementary beams of the same color
    [3" id="c-fr-0003]
    3. The method of claim 2 wherein said phase shift is a phase inversion.
    [4" id="c-fr-0004]
    4. The method of claim 2, wherein said phase shift is a phase quadrature.
    [5" id="c-fr-0005]
    5. Method according to one of the preceding claims wherein a plurality of said elementary beams has footprints on the ground of substantially identical size
    [6" id="c-fr-0006]
    6. The method of claim 5 wherein all of said elementary beams have footprints on the ground of substantially identical size.
    [7" id="c-fr-0007]
    7. Method according to one of the preceding claims, in which the footprints of said composite beams have sizes which vary progressively across said region of the earth's surface.
    [8" id="c-fr-0008]
    8. Method according to one of the preceding claims wherein all the elementary beams forming a single composite beam are generated at the same time.
    [9" id="c-fr-0009]
    9. Method according to one of claims 1 to 7 wherein all the elementary beams forming a single composite beam are generated in turn.
    [10" id="c-fr-0010]
    10. Satellite telecommunications payload for the implementation of a method according to one of the preceding claims comprising: a plurality of source antennas (S1 - S4); at least one reflector (R) arranged to cooperate with said source antennas so as to generate a radiofrequency beam, called elementary beam, for each said source antenna; and a plurality of transmit or receive modules (MTRa, MTRb) configured to transmit or receive respective data in the form of radio frequency signals; characterized in that: each said source antenna belongs to a group of source antennas, at least some of said groupings comprising a plurality of source antennas; in that each said transmission module is connected to all the source antennas belonging to the same grouping, so that the elementary beams generated by the source antennas of the same grouping form a composite beam; said groups of source antennas being configured so that a plurality of said composite beams have footprints of different sizes; and in that the elementary antennas of at least one said array are configured to generate non-adjacent elementary beams of the same color, a color being defined by a frequency band and a polarization state
    [11" id="c-fr-0011]
    11. Telecommunications payload according to claim 10, in which a phase shifter (ϋΦ) is arranged between at least one elementary antenna of at least one said grouping configured to generate non-adjacent elementary beams of the same color and the transmission module. or corresponding reception.
    [12" id="c-fr-0012]
    12. Payload of telecommunications according to claim 11 wherein said or each said phase shifter is a phase inverter.
    [13" id="c-fr-0013]
    13. Telecommunications payload according to claim 11, in which said or each said phase shifter is configured to effect a 90 ° phase shift.
    [14" id="c-fr-0014]
    14. Telecommunication payload according to one of claims 10 to 13 in which said groups of source antennas are configured such that all of said elementary beams have footprints on the ground of substantially identical size
    [15" id="c-fr-0015]
    15. Telecommunications payload according to one of claims 10 to 14 wherein at least one said transmitting or receiving module is equipped with a switch configured to connect said module to the corresponding elementary antennas in turn.
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    EP3503431A1|2019-06-26|
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    CA3028305A1|2019-06-21|
    FR3076138B1|2019-11-15|
    US20190199433A1|2019-06-27|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    DE10021112A1|2000-05-02|2001-11-22|Deutsch Zentr Luft & Raumfahrt|Satellite communication system combines single beam to meta-beam and provides same partial signal current to all single beams in transmission direction|
    US20170181160A1|2015-12-18|2017-06-22|Thales|Method of satellite communication with flexible capacity distribution based on beam hopping and on a fractional reuse scheme|
    US20170289822A1|2016-03-29|2017-10-05|Space Systems/Loral, Llc|Satellite system using time domain beam hopping|
    US5495258A|1994-09-01|1996-02-27|Nicholas L. Muhlhauser|Multiple beam antenna system for simultaneously receiving multiple satellite signals|
    AU4008600A|1999-03-25|2000-10-16|Ali Atia|Ground-satellite distributed multi-beam communication system|
    US8600292B2|2006-06-30|2013-12-03|Qualcomm Incorporated|Beam focusing in multi-beam satellite systems by combining signals from multiple satellite beams on the ground|
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    法律状态:
    2018-11-27| PLFP| Fee payment|Year of fee payment: 2 |
    2019-06-28| PLSC| Publication of the preliminary search report|Effective date: 20190628 |
    2019-11-28| PLFP| Fee payment|Year of fee payment: 3 |
    2020-11-25| PLFP| Fee payment|Year of fee payment: 4 |
    2021-11-26| PLFP| Fee payment|Year of fee payment: 5 |
    优先权:
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    FR1701345A|FR3076138B1|2017-12-21|2017-12-21|MULTIFUNCTION COVERING METHOD BY REGROUPING ELEMENTARY BEAMS OF THE SAME COLOR, AND USEFUL TELECOMMUNICATIONS CHARGE FOR CARRYING OUT SUCH A METHOD|
    FR1701345|2017-12-21|FR1701345A| FR3076138B1|2017-12-21|2017-12-21|MULTIFUNCTION COVERING METHOD BY REGROUPING ELEMENTARY BEAMS OF THE SAME COLOR, AND USEFUL TELECOMMUNICATIONS CHARGE FOR CARRYING OUT SUCH A METHOD|
    US16/226,522| US20190199433A1|2017-12-21|2018-12-19|Method for multibeam coverage by the grouping of elementary beams of the same colour, and telecommunications payload for implementing such a method|
    CA3028305A| CA3028305A1|2017-12-21|2018-12-20|Method for multibeam coverage by the grouping of elementary beams of the same colour, and telecommunications payload for implementing such a method|
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    CN201811571533.XA| CN110011708A|2017-12-21|2018-12-21|The method for the multi-beam antenna being grouped by the basic wave beam to same color and the communication payload for realizing this method|
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