PAYLOAD FOR A MULTI-BEAM SATELLITE

Abstract

A payload includes one or more antennas for receiving polarized radiofrequency signals; a device for regenerating radiofrequency signals by filtering, frequency transposition, and amplification; and antennas for transmitting the regenerated radiofrequency signals to one or more terrestrial terminals. The regeneration device includes a plurality of regeneration channels, each channel including an amplification device capable of amplifying a plurality of radiofrequency signals having separate frequency bands, and in that the transmission antennas are capable of transmitting regenerated radiofrequency signals, via a single regeneration channel, to non-contiguous basic coverage areas, respectively, the basic coverage areas belonging to a single cellular layout that uses at least two separate frequency bands and two separate polarizations.

Description

TECHNICAL FIELD OF THE INVENTION

The present invention relates to a forward link payload for a multi-beam satellite, a forward link allowing receipt of radiofrequency signals from at least one main terrestrial station so as to re-transmit said signals to at least one terrestrial terminal, said payload comprising:

• • one or more reception antennas for receiving polarised radiofrequency signals;
  • a regeneration device for regenerating radiofrequency signals by filtering, frequency, transposition and amplification; and
  • transmission antennas for transmitting the regenerated radiofrequency signals to one or more terrestrial terminals, each signal being destined for a basic coverage area.

The present invention also relates to a return link payload for a multi-beam satellite, a return link allowing receipt of radiofrequency signals from at least one terrestrial terminal and re-transmission of said signals to at least one main terrestrial station, said payload comprising:

• • one or more reception antennas for receiving radiofrequency signals, each signal coming from a basic coverage area; and
  • a regeneration device for regenerating radiofrequency signals by filtering, frequency transposition and amplification; and
  • transmission antennas for transmitting the polarised regenerated radiofrequency signals to one or more main terrestrial stations.

The present invention is applied particularly in the field of multi-beam satellites.

TECHNICAL BACKGROUND OF THE INVENTION

In the field of multi-beam satellites, a known prior art forward link payload for a multi-beam satellite, a forward link allowing receipt of N_GW radiofrequency signals from at least one main terrestrial station so as to re-transmit said signals to at least one terrestrial terminal, comprises:

• • one or more reception antennas for receiving polarised radiofrequency signals;
  • a regeneration device for regenerating radiofrequency signals, also called a repeater, comprising:
    • N_GW low noise amplifiers LNA for amplifying each of the radiofrequency signals;
    • N_GW signal divider devices for separating each radiofrequency signal distributed over N_GW uplink channels;
    • N_C frequency converter circuits generally for frequency translating and filtering the N_GW radiofrequency signals so as to re-distribute said signals in accordance with a frequency plan of the downlink over N_C downlink channels;
    • N_C high-power amplifiers for amplifying the N_C downlink radiofrequency signals; and
    • N_C output bandpass filters for filtering each of the N_C radiofrequency signals.
  • transmission antennas for transmitting the regenerated radiofrequency signals to one or more terrestrial terminals, each signal being associated with a basic coverage area.

According to the same principle, a known prior art return link payload for a multi-beam satellite, a return link allowing receipt of N_C radiofrequency signals from at least one terrestrial terminal and re-transmission of said signals to at least one main terrestrial station, comprises:

• • one or more reception antennas for receiving radiofrequency signals, each radiofrequency signal coming from a single basic coverage area called a cell; and
  • a regeneration device for regenerating radiofrequency signals, comprising:
    • N_C low noise amplifiers LNA;
    • N_C frequency converter circuits for frequency translating and filtering the N_C radiofrequency signals so as to distribute them in accordance with a frequency plan of the downlink over N_GW downlink channels over the return link;
    • a multiplexer (with N_C inputs and N_GW outputs) for regrouping the radiofrequency signals destined for the same main terrestrial station; and
    • N_GW high-power amplifiers HPA for amplifying each of the N_GW radiofrequency signals.
  • transmission antennas for transmitting N_GW radiofrequency signals to one or more main terrestrial stations.

A drawback of this prior art is that the combination of the forward link and of the return link leads to the use of a very considerable number of components, which leads to a significant increase in the mass of the multi-beam satellite.

In addition, patent application WO 2004/103325 describes a multi-beam satellite using two cell plannings of the honeycomb type superposed on, one another in an offset manner. Each cell planning uses three different frequency bands and the same given polarisation for all their cells, which makes it possible to use a six-colour frequency re-use pattern. The polarisation used by one cell planning is orthogonal to the polarisation used by the other cell planning. The superposition of the two layouts combined with the orthogonal arrangement of the polarisations of the two layouts makes it possible to obtain central regions in which the interferences between cells are reduced.

A drawback of this prior art is that the frequency re-use pattern is not optimal.

GENERAL DESCRIPTION OF THE INVENTION

The object of the present invention is to provide a payload which makes it possible to reduce the“dry” mass of a multi-beam satellite (that is to say the mass of the multi-beam satellite without fuel) whilst using a more effective frequency re-use pattern.

In accordance with a first subject of the invention, this object is achieved by a forward link payload for a multi-beam satellite, a forward link allowing receipt of radiofrequency signals from at least one main terrestrial station so as to re-transmit said signals to at least one terrestrial terminal, said payload comprising:

• • at least one reception antenna for receiving polarised radiofrequency signals;
  • a regeneration device for regenerating radiofrequency signals by filtering, frequency transposition and amplification; and
  • transmission antennas for transmitting the regenerated radiofrequency signals to at least one terrestrial terminal, each signal being destined for a basic coverage area, characterised in that the regeneration device comprises a plurality of regeneration chains, each chain comprising an amplification device able to amplify a plurality of radiofrequency signals having different frequency bands, and in that the transmission antennas are able to send regenerated radiofrequency signals, via a single regeneration chain, to non-contiguous basic coverage areas, said basic coverage areas belonging to a single cell planning which uses at least two frequency bands and two different polarisations.

As will be seen in detail hereinafter, the use of one regeneration chain for management of two radiofrequency signals makes it possible to reduce the number of chains used and therefore to reduce the dry mass of the multi-beam satellite, without having a multi-path effect on a radiofrequency signal thanks to the combination of radiofrequency signals from non-contiguous basic coverage areas, which makes it possible to obtain spatial isolation.

In accordance with non-limiting embodiments, the forward link payload may further comprise one or more additional features from the following:

• • the transmission antennas associated with a regeneration chain are able to transmit two regenerated radiofrequency signals having orthogonal directions of polarisation. This makes it possible to obtain isolation by polarisation and to thus further reduce the multi-path effects between the radiofrequency signals at the output of the multi-beam satellite.
  • an amplification device comprises a channel amplifier and a travelling wave tube amplifier.

In accordance with a second subject, the invention relates to a return link payload for a multi-beam satellite, a return link allowing receipt of radiofrequency signals from at least one terrestrial terminal and re-transmission of said signals to at least one main terrestrial station, said payload comprising:

• • at least one reception antenna for receiving radiofrequency signals, each signal being associated with a basic coverage area;
  • a regeneration device for regenerating radiofrequency signals by filtering, frequency transposition and amplification; and
  • transmission antennas for transmitting polarised regenerated radiofrequency signals to at least one main terrestrial station, characterised in that the regeneration device comprises a plurality of regeneration chains, each chain comprising an amplification device able to amplify a plurality of radiofrequency signals having different frequency bands, and in that the reception antennas are able to receive radiofrequency signals destined for the same regeneration chain from non-contiguous basic coverage areas, said basic coverage areas belonging to a single cell planning which uses at least two frequency bands and two different polarisations.

In accordance with a non-limiting embodiment, an amplification device comprises a channel amplifier and a travelling wave tube amplifier.

In accordance with a third subject, the invention relates to a multi-beam satellite comprising a payload characterised by a forward link according to at least one of the above features, and characterised by a return link according to at least one of the above features.

In accordance with a fourth subject, the invention relates to a telecommunications network for establishing radiofrequency links between at least one main terrestrial station and at least one terrestrial terminal via a multi-beam satellite, said network comprising at least one main terrestrial station, at least one terrestrial terminal, and a multi-beam satellite, in accordance with which the multi-beam satellite comprises a payload according to at least one of the above features.

The invention and its various applications will be better understood upon reading the following description and studying the accompanying figures.

BRIEF DESCRIPTION OF THE FIGURES

The figures are given merely by way of indication and in no way limit the invention.

FIG. 1 is a simplified schematic view of a telecommunications network comprising a multi-beam satellite comprising a payload according to the invention;

FIG. 2 is a functional block diagram of an architecture of a forward link payload according to a non-limiting embodiment of the invention;

FIG. 3 illustrates a four-colour pattern for European coverage area used by the payload of FIG. 2;

FIG. 4 illustrates uplink frequency channels used by the forward link payload of FIG. 2;

FIG. 5 illustrates downlink frequency channels used by the forward link payload of FIG. 2;

FIG. 6 illustrates part of the four-colour pattern of FIG. 4 with axes of displacement;

FIG. 7 shows an attenuation curve of filters included in a regeneration chain of the payload of FIG. 2 in the case where radiofrequency signals are transmitted by the antennas of the payload with orthogonal directions of polarisation;

FIG. 8 shows a schematic diagram of radiation of antennas of the payload of FIG. 2 in the direction of a terrestrial terminal which would be displaced along an axis of displacement of FIG. 6 when the terminal does not exhibit polarisation discrimination;

FIG. 9 is an enlarged view of part of FIG. 8;

FIG. 10 shows a schematic diagram of radiation of antennas of the payload of FIG. 2 in the direction of a terrestrial terminal which would be displaced along an axis of displacement of FIG. 6 when the terminal exhibits polarisation discrimination;

FIG. 11 shows an attenuation curve of filters included in a regeneration chain of a payload of the prior art;

FIG. 12 is a first power curve of a ripple of a radiofrequency signal received by the payload of FIG. 2 as a function of overall rejection;

FIG. 13 is a functional block diagram of an architecture of a return link payload according to a non-limiting embodiment of the invention;

FIG. 14 illustrates the uplink frequency channels used by the return link payload of FIG. 13; and

FIG. 15 illustrates the downlink frequency channels used by the return link payload of FIG. 13.

DETAILED DESCRIPTION OF THE INVENTION

Like elements are denoted by like reference numerals in all the figures.

FIG. 1 illustrates a telecommunications network 1 for establishing radiofrequency links between at least one main terrestrial station 2 and at least one terrestrial terminal 6 via a multi-beam satellite 3. Such a network is also called a satellite telecommunications network.

In practice, the telecommunications network 1 is formed by a plurality of main terrestrial stations 2 which are interconnected via a terrestrial network (Internet network in a non-limiting example). It should be noted that, in a non-limiting example, a main terrestrial station 2 (also called a central station) is a terrestrial “gateway” connected to an Internet backbone 5.

In particular, the multi-beam satellite 3 comprises

• • a payload according to the invention; and
  • a platform.

The payload of a multi-beam satellite 3 denotes the part which allows said satellite to carry out the task for which it was designed, that is to say, in particular for a multi-beam satellite 3 as shown in FIG. 1, to ensure receipt, processing (filtering, frequency transposition, amplification) and re-transmission of telecommunications signals from the main terrestrial station 2 to terrestrial terminals 6, or the re-transmission of telecommunications signals from terrestrial terminals 6 to the main terrestrial station 2. A payload thus comprises in particular antennas and repeaters, whereas a platform comprises in particular control, propulsion or electrical power equipment.

A multi-beam satellite 3 allows use of a plurality of radiofrequency signals SP to cover basic coverage areas called cells C which belong to a single cell planning N (as illustrated in FIG. 3 and in part in FIG. 6). “Cell planning” means a network of cells in which a cell is surrounded by a maximum of six cells. The cells are circular areas which overlap so as to cover a specific geographical area. A plurality of radiofrequency links occupying the same frequency band can also be established over different radiofrequency signals SP so as to cover cells, for example which are contiguous.

It should be noted that “radiofrequency signal” means a signal which is received/transmitted over a specific bandwidth and in a specific frequency channel of this bandwidth. In addition, a radiofrequency signal comprises a plurality of primary signals destined for a plurality of users or provided by a plurality of users, said primary signals having the same direction of polarisation and having both different frequencies (in the channel) and different transmission/receipt times.

If the satellite telecommunications network is a broadband network, the multi-beam satellite 3 is used in a bi-directional manner, that is to say to both:

• • relay data transmitted by the main terrestrial station 2 (connected to the terrestrial network) to one or more terrestrial terminals 6: This first link, of the point to multipoint type, is called the forward link;
  • relay to the main terrestrial station 2 the data transmitted by one or more terrestrial terminals 6: This second link, of the multipoint to point type, is called the return link.

As will be seen hereinafter,

• • in the forward link, radiofrequency signals RF are sent over a link called an uplink LM1 to the multi-beam satellite 3 by the main terrestrial station 2, as illustrated in FIG. 1. These radiofrequency signals RF are then processed at the multi-beam satellite 3, then re-transmitted over a link called a downlink LD1 to the terrestrial terminals 6, as illustrated in FIG. 1;
  • in the return link, radiofrequency signals SP are sent over a link called an uplink LM2 to the multi-beam satellite 3 by the terrestrial terminals 6, as illustrated in FIG. 1. These radiofrequency signals SP are then processed at the multi-beam satellite 3, then re-transmitted over a link called a downlink LD2 to the main terrestrial station 2, as illustrated in FIG. 1.

It is recalled that a general frequency band for establishing radiofrequency links called the Ka-band associated with a coverage area for region 1 (Europe) is defined within the scope of a regulation drafted by the International Union of Telecommunications (IUT).

The following frequency distribution is provided in accordance with this Ka-band:

	Forward	Uplink LM1	Bandwidth:
	link	(from the terrestrial	27.5 GHz to 29.5 GHz
		station)
		Downlink LD1 (to the	Bandwidth:
		terrestrial terminals)	19.7 GHz to 20.2 GHz
	Return link	Uplink LM2	Bandwidth:
		(from the terrestrial	29.5 GHz to 30.0 GHz
		terminals)
		Downlink LD2 (to the	Bandwidth:
		terrestrial station)	17.7 GHz to 19.7 GHz

This Ka-band will be considered in the description below as a non-limiting example.

It should be noted that a geographical coverage area such as Europe is formed of a plurality of cells C belonging to a single cell planning N, each cell C being represented schematically by a circle.

The payload 10 is described hereinafter firstly with regard to the forward link and secondly with regard to the return link.

Forward Link

A forward link payload 10 for a multi-beam satellite 3, a forward link allowing receipt of radiofrequency signals from at least one main terrestrial station 2 so as to re-transmit said signals to at least one terrestrial terminal 6, is described in a non-limiting embodiment in FIG. 2.

In particular, this forward link payload comprises:

• • one or more reception antennas A_RX for receiving polarised radiofrequency signals;
  • a regeneration device REP for regenerating radiofrequency signals RF by filtering, frequency transposition and amplification, the regeneration device comprising a plurality of regeneration chains 100, each chain comprising an amplification device HPA able to amplify a plurality of radiofrequency signals having different frequency bands; and
  • transmission antennas A_TX1, A_TX2 for transmitting the regenerated radiofrequency signals SP to one or more terrestrial terminals 6, each signal SP being destined for a basic coverage area, called a cell C, and the transmission antennas being able to transmit the regenerated radiofrequency signals SP, via a single regeneration chain 100, to non-contiguous basic coverage areas C, said basic coverage areas belonging to a single cell planning N which uses at least two frequency bands F′, F″ and two different polarisations.

As will be seen hereinafter, the ability to manage two radiofrequency signals in a single regeneration chain 100 makes it possible to reduce the number of components used, without having multi-path effect's caused by signal replicas thanks to the transmission of regenerated radiofrequency signals SP to two non-contiguous basic coverage areas.

It should be noted that the terms “basic coverage area” and “cell” will be used synonymously in the description below.

The forward link payload 10 functions in the following manner.

In a first step 1), the reception antennas A_RX for receiving the payload 10 receive polarised radiofrequency signals RF. These signals RF are sent by one or more main terrestrial stations 2 over an uplink LM1. In the non-limiting example taken from FIG. 2 and throughout the rest of the description, only a single main station 2 will be considered.

In a first non-limiting embodiment, the polarisation is linear. In this case, the polarisation includes two directions: horizontal and vertical.

In a second non-limiting embodiment, the polarisation is circular: In this case, the polarisation includes two directions: left-hand circular and right-hand circular.

A circular polarisation will be considered by way example in the rest of the description.

It should be noted that the radiofrequency signals RF are received by a method called frequency re-use. This method makes it possible to use the same frequency range a number of times in the same multi-beam satellite 3 so as to increase the overall capacity of the multi-beam satellite 3 without increasing the assigned bandwidth. In a non-limiting embodiment, a frequency re-use pattern called a colour pattern is used and frequency plans are determined using this pattern.

The uplink LM1 leaving the main terrestrial station 2 uses a given polarisation, in this case a circular polarisation, having two directions of polarisation.

Frequency channels CH are associated with a given polarisation and are distributed among the two directions of polarisation. In accordance with a four-colour pattern (red, yellow, blue, green), the signal transmissions being polarised in one of the two directions of polarisation (right-hand circular or left-hand circular), each colour is associated with a band of 250 MHz and a given direction of polarisation, and therefore with a given channel CH.

It should be noted that the use of a four-colour pattern is a non-limiting example, and that a pattern of any number of colours greater than three can be used. However, if it is desired to utilise isolation by polarisation (explained further below) to the best possible extent allowed by the use of two directions of polarisation, an even number of colours is used.

The following is adopted throughout the rest of the description;

• • the colour red is represented by lines hashed to the left;
  • the colour green is represented by disperse dots;
  • the colour blue is represented by lines hashed to the right;
  • the colour yellow is represented by dense dots.

It should be noted that this type of pattern is just as applicable in uplink LM1 as in downlink LD1.

Also, in a non-limiting embodiment, in the downlink LD1 a colour is associated with each regenerated radiofrequency signal SP from the multi-beam satellite 3 (and thus to a cell C) in such a way that the regenerated radiofrequency signals of the same “colour.” are not adjacent: The contiguous cells thus correspond to different colours. An example of a four-colour pattern for the coverage area of Europe is shown in FIG. 3. In the case of the Ka-band, 80 cells C are used to cover the area of Europe, said cells belonging to a single cell planning N, as illustrated in FIG. 3.

FIGS. 4 and 5 show a frequency plan using the colour pattern and broken down as follows:

• • an uplink frequency plan PMVA over the forward link; and
  • a downlink frequency plan PDVA over the forward link.

The notations RHC and LHC refer to the right-hand and left-hand circular directions of polarisation respectively.

In the example of the Ka-band, the PMVA plan corresponding to the uplink LM1 over the forward link (from the main terrestrial station to the multi-beam satellite 3) has 2 GHz (from 27.5 to 29.5 GHz) of available frequency spectrum.

There are thus 16 channels CH for a given polarisation, that is to say 8 channels CH for each given direction of polarisation, and 2 channels distributed over the same frequency band of 250 MHz. In the example of FIG. 4, the channels CH1 to CH8 have the first direction of polarisation (left-hand circular LHC for example) and the channels CH9 to CH16 have the second direction of polarisation (right-hand circular RHC). The use of polarised signals makes it possible to reduce the total number of main terrestrial stations 2 because double the number of signals is sent via one main terrestrial station.

The main terrestrial station 2 thus distributes the radiofrequency signals RF over 16 channels of 250 MHz bandwidth (8 channels for each direction of polarisation). These radiofrequency signals RF distributed over these 16 channels after regeneration by the payload 10 of the multi-beam satellite 3 will be distributed over 4 downlink channels, as will be seen hereinafter.

It should be noted that it has been assumed that the entire spectrum of 2 GHz is used. However, it should be noted that it is also possible, in other embodiments and in particular for operational reasons, for only part of the spectrum to be used and for fewer channels CH to be generated.

Thus, for the forward link, a radiofrequency signal RF sent by the main terrestrial station 2 is associated with one of the four following colours:

• • a red colour corresponding to a first band of 250 MHz and to the left-hand circular direction of polarisation;
  • a yellow colour corresponding to the same first band of 250 MHz and to the right-hand circular direction of polarisation
  • a blue colour corresponding to a second band of 250 MHz and to the right-hand circular direction of polarisation;
  • a green colour corresponding to the same second band of 250 MHz and to the left-hand circular direction of polarisation.

Four adjacent channels CH of the same pattern are each associated with a different colour.

Thus, “different colour” means the fact of having different polarisation and/or a different frequency.

Thus, for two different colours it is possible to have:

• • either the same frequency band and different polarisation;
  • or a different frequency band and;
    • either different polarisation; or
    • same polarisation.

Thus, the cell planning described N is a network of cells in which a cell is surrounded by a maximum of six cells using different frequency bands and/or different polarisations.

In the non-limiting example above, the reception antennas A_RX for receiving the payload 10 thus receive radiofrequency signals RF distributed over the 16 channels CH.

As will be seen hereinafter, the radiofrequency signals RF multiplexed over the Channels CH are then regenerated at the payload 10 of the multi-beam satellite 3, each of these regenerated signals SP being distributed over downlink channels CH′ associated with a direction of polarisation RHC or LHC and with frequency bands in accordance with the downlink frequency plan PDVA.

In a second step 2), the regeneration devise REP regenerates the radiofrequency signals RF by filtering, frequency transposition and amplification, as will be seen hereinafter.

The regeneration device REP is called a repeater and, in a non-limiting embodiment as illustrated in FIG. 2, comprises a plurality of regeneration chains 100, each chain 100 comprising an amplification device 100 able to amplify radiofrequency signals RF having different frequency bands.

In a non-limiting embodiment adopted throughout the rest of the description, the antennas A_RX of a single regeneration chain 100 receive the radiofrequency signals RF destined for two cells C. One regeneration chain 100 will thus process two radiofrequency signals RF. There are thus 40 regeneration chains 100 in the repeater REP.

In a non-limiting embodiment, a regeneration chain 100 comprises:

• • one low noise amplifier 12 (LNA) for amplifying the two radiofrequency signals RF as a function of the noise generated by the components of the regeneration chain 100;
  • one signal divider device 13 (demultiplexer) for separating the two radiofrequency signals RF which are distributed channels CH of the uplink PMVA;
  • one frequency converter circuit CONV formed:
    • by a local oscillator 14 for frequency translating the radiofrequency signals and for adjusting them over two of the four channels CH′ in accordance with the frequency plan of the downlink PDVA. In the case of the Ka-band, each of the four channels CH′ is associated with a frequency band from the two frequency bands [19.7; 19.95] and [19.95; 20.2] and with a polarisation RHC or LHC, as shown in the downlink frequency plan PDVA for the forward link in FIG. 5; and
    • by an input filter 15 for filtering the part of the signal useful for amplification in the radiofrequency signals.
  • one amplification device which is a high power amplifier (HPA) formed, in a non-limiting embodiment, by a channel amplifier 17 (CAMP) and a travelling wave tube amplifier for amplifying the radiofrequency signals; and
  • two output bandpass filters 19 (also called output demultiplexers) for filtering the regenerated radiofrequency signals SP as a function of their destination cell and thus as a function of the transmission antennas A_TX1, A_TX2 associated with these cells.

At the output of a regeneration chain 100, regenerated radiofrequency signals SP will thus be distributed over two downlink frequency channels CH′ (also called output channels).

Thus, at the output of a repeater REP, regenerated radiofrequency signals SP will thus be distributed over four downlink frequency channels CH′1 to CH′4.

In a non-limiting embodiment, the following frequencies are assigned to the output channels CH′, as illustrated in FIG. 5:

• • a first frequency F′ between 19.7 GHz and 19.95 GHz for the first output channel CH′1 and the third output channel CH′3′
    • a second frequency F″ between 19.95 GHz and 20.2 GHz for the second output channel CH′2 and the fourth output channel CH′4.

The cell planning N thus uses at least two frequency bands F′, F″ and two different polarisations.

The use of one regeneration chain 100 to amplify a plurality of radiofrequency signals RF thus makes it possible to reduce the number of components used in the payload 10.

In addition, the two radiofrequency signals RF amplified by an amplification device HPA of a regeneration chain 100 have different frequency bands. This makes it possible to differentiate between them in the regeneration chain 100 and more specifically in the converter CONY and the demultiplexers 19.

It should be noted that the regeneration of a plurality of radiofrequency signals in a single regeneration chain 100 and thus the use of at least two demultiplexers 19 and antennas A_TX associated with each demultiplexer 19 may lead to multi-path effects caused by a replica of a radiofrequency signal R_SP. Such a replica is created just after the high-power amplifier HPA. In fact, since the filters 19 and transmission antennae A_TX are not perfect, part of the regenerated radiofrequency signal SP destined for a given cell C is filtered by the wrong filter 19 and is sent to said cell C by the wrong antenna A_TX, which results in the creation of the replica of a signal R_SP.

Thus, as illustrated in FIG. 2, a first filter 19 makes it possible to filter a first radiofrequency signal SP destined for a first given cell, whereas a second filter 19 of the same regeneration chain 100 makes it possible to filter a second radiofrequency signal (not shown) destined for a second given cell. This second filter 19 will also filter the replica R_SP of the first filtered signal. Depending on the attenuation of this second filter, the first cell C may or may not receive the replica of the signal R_SP as interference.

Moreover, as illustrated in FIG. 2, a first antenna A_TX1 will radiate the first regenerated radiofrequency signal SP destined for a first specific cell C, and a second antenna A_TX2 will radiate the replica of the signal S_RP towards, the same cell C. This leads to poor reception of the first regenerated radiofrequency signal SP by the first cell C to which it is destined and therefore by the terrestrial terminals 6 of this cell C. In fact, a terrestrial terminal 6 will receive, in combination, the regenerated radiofrequency signal SP via the first antenna A_TX1, this signal being destined for said terminal, but also the replica R_SP of this signal via the second antenna A_TX2.

The replica R_SP of a signal will thus produce multi-path effects which will be attenuated as a function of the filters 19 used in a regeneration chain 100, but also as a function of the radiation of the antennas A_TX1, A_TX2 used and associated with a single regeneration chain 100.

It should be noted that the combination of the replica of the signal with the radiofrequency signal itself introduces an undulation PPR, called a ripple, into the power of the regenerated radiofrequency signal SP destined for a terrestrial terminal 6. The greater the amplitude of this undulation, called the peak-to-peak ripple, the more significant the multi-path effects caused by a signal replica.

As will be seen hereinafter, the multi-path effects are reduced by influencing in particular a spatial component of the radiofrequency signal SP received by a terrestrial terminal 6.

The form of the radiofrequency signal SP received by terrestrial terminal 6 is represented as follows:

S _r(t,F,x)=β(x)S_t(t)(1+α_F(F)·α_A(x))  [1]

where:

• • S_r(t, F, x) is the radiofrequency signal SP received by the terrestrial terminal 6 at a frequency F and when the terminal 6 is located in a position x in the coverage area of the Ka-band;
  • S_t(t) is the radiofrequency signal RF received by the multi-beam satellite 3;
  • β(x) is the losses over the radiofrequency signal RF caused by the multi-beam satellite 3 and by the propagation of the signal towards the terrestrial terminal 6;
  • α_F(F) is a frequential parameter, also called the frequential component, representative of the attenuation caused by the filters 19 of a regeneration chain 100 of the payload 10;
  • α_A(x) is a spatial parameter which is also called the spatial component and is representative of spatial isolation of the terminal 6 in position x in the coverage area of the Ka-band.

It should be noted that the product of the frequential and spatial components α_F(F) and α_A(x) is representative of a signal replica, the signal received by a terrestrial terminal 6 not being pure due to the fact that the filters 19 of the payload 10 and the transmission antennas A_RX are not perfect, as explained above.

It should also be noted that the smaller the frequential component α_F(F), the greater the rejection of the filters 19. Likewise, the smaller the spatial component α_A(x), the greater the rejection caused by the transmission antennas A_TX. The overall rejection will thus vary as a function of the spatial component α_A(x) and also as a function of the frequential component α_F(F).

By influencing only one of the two components, it is possible to increase overall rejection and thus minimise the multi-path effects caused by a signal replica. In fact, by influencing the spatial component α_A(x), the overall rejection can be increased for example, since the smaller the spatial component α_A(x), the smaller the product of the components α_F(F) and α_A(x).

As will be seen hereinafter, external spatial isolation is carried out so as to reduce the spatial component α_A(x), and, in a non-limiting embodiment, additional isolation by polarisation is carried out, which increases overall rejection and thus reduces the multi-path effects and therefore the ripple PPR in the power of the regenerated radiofrequency signal SP.

In a third step 3), the transmission antennas A_TX1, A_TX2 transmit the regenerated radiofrequency signals SP to one or more terrestrial terminals 6, each regenerated radiofrequency signal SP being destined for a basic coverage area C.

External Spatial Isolation by Non-Adjacent Cells

So as to reduce the spatial component α_A(x), the transmission antennas A_TX1, A_TX2 associated with a regeneration chain 100 are able to transmit the regenerated radiofrequency signals SP by said regeneration chain 100 to non-contiguous cells C.

Without Isolation by Polarisation

For example, two regenerated radiofrequency signals SP regenerated by the same regeneration chain 100 are thus radiated to two cells which are not adjacent but which are paired as follows:

• • a green cell (left-hand circular polarisation) and a non-adjacent red cell (left-hand circular polarisation); or
  • a yellow cell (right-hand circular polarisation) and a non-adjacent blue cell (right-hand circular polarisation).

In this case, the transmission antennas A_TX1, A_TX2 associated with a regeneration chain 100 are able to transmit at least two regenerated radiofrequency signals SP regenerated by said regeneration chain 100 and having the same direction of polarisation.

With reference to FIG. 6, which illustrates part of the coverage area of the Ka-band of FIG. 2, in this case for example the transmission antennas A_TX of the same regeneration chain 100 which are able to radiate a regenerated radiofrequency signal SP33 destined for a cell C33 (green cell) for example can also be used to radiate a regenerated radiofrequency signal destined for the non-adjacent cell C13 (red cell) or destined for the non-adjacent cell C11 (red cell) or destined for the non-adjacent cell C36 (red cell).

The cells C33 and C13 have an edge-to-edge distance Dc measuring half a diameter θ_C of a cell (case a)).

The cells C33 and C11 have an edge-to-edge distance Dc measuring 1.3 times the diameter θ_C of a cell (case b)).

The cells C33 and C36 have an edge-to-edge distance Dc measuring 1.6 times the diameter θ_C of a cell (case c)).

The radiation of an antenna in the direction of a cell includes a main lobe Lb0, Lb0′, Lb0″, a primary lobe Lb1, Lb1′, Lb1″, and a secondary lobe Lb2, Lb2′, Lb2″.

Likewise, for example the transmission antennas A_TX of the same regeneration chain 100 which are able to radiate a regenerated radiofrequency signal SP42 destined for a cell C42 (yellow cell) for example can also be used to radiate a regenerated radiofrequency signal of the non-adjacent cell C22 (blue cell) or of the non-adjacent cell C24 (blue cell) or of the non-adjacent cell C45 (blue cell).

The cells C42 and C22 have an edge-to-edge distance Dc measuring half a diameter θ_C of a cell (case a)).

The cells C42 and C24 have an edge-to-edge distance Dc measuring 1.3 times the diameter θ_C of a cell (case b)).

The cells C42 and C45 have an edge-to-edge distance Dc measuring 1.6 times the diameter θ_C of a cell (case c)).

The cells are thus isolated spatially from one another.

Case a) C33 and C13

In the case of external spatial isolation of a half-cell (Dc=0.5), a terrestrial terminal 6 positioned in a green cell, cell C33 for example, will receive:

• • a first regenerated radiofrequency signal SP33 destined for said green cell; and
  • a signal replica R_SP33 filtered by the primary lobe Lb1′ of the radiation of the antenna which transmits in the direction of the non-adjacent red cell C13.

The replica of the signal R_SP33 will be filtered by this primary lobe Lb1′ instead of by the main lobe Lb0′. Filtering (rejection of the filter) is thus more substantial and therefore the replica of the signal received by the terminal 6 for which the regenerated radiofrequency signal SP33 is destined will be weaker.

Thus, in the case of external spatial isolation of half cell diameter, if the terminal 6 is located next to the cell and is at a border frequency F2 (described, further below) of a channel CH′, the reduction in the multi-path effects will be −18 dB. The spatial component α_A(x)<<1 is obtained.

Case b) C33 and C11

In the case of external spatial isolation of 1.3 times cell diameter (Dc=1.3), a terrestrial terminal 6 positioned in a green cell, cell C33 for example, will receive:

• • a first regenerated radiofrequency signal SP33 destined for said green cell; and
  • a signal replica R_SP33 filtered by a secondary lobe Lb2′ of the radiation of the antenna which transmits in the direction of the non-adjacent red cell C11.

The replica of the signal R_SP33 will be filtered by this secondary lobe Lb2′ instead of by the main lobe Lb0′ or the primary lobe Lb1′. Filtering (rejection of the filter) is thus more substantial and therefore the replica of the signal received by the terminal 6 for which the regenerated radiofrequency signal SP33 is destined will be weaker.

Thus, in the case of external spatial isolation of cell diameter Dc=1.3, if the terrestrial terminal 6 is located next to the cell and is at a border frequency F2 (described further below) of a channel CH′, the reduction in the multi-path effects will be −24 dB compared to a situation with no external spatial isolation. The spatial component α_A(x)<<1 is obtained.

Case c) C33 and C36

In the case of external spatial isolation of 1.6 times cell diameter (Dc=1.6), a terrestrial terminal 6 positioned in a green cell, cell C33 for example, will receive:

• • a first regenerated radiofrequency signal SP33 destined for said green cell; and
  • a signal replica R_SP33 filtered by a secondary lobe Lb2′ of the radiation of the antenna which transmits in the direction of the non-adjacent red cell C36.

The replica of the signal R_SP33 will be filtered by this secondary lobe Lb2′ instead of by the main lobe Lb0′ or the primary lobe Lb1′. Filtering (rejection of the filter) is thus more substantial and therefore the replica of the signal received by the terminal 6 for which the regenerated radiofrequency signal SP33 is destined will be weaker.

Thus, in the case of external spatial isolation of cell diameter Dc=1.6, if the terrestrial terminal 6 is located next to the cell and is at a border frequency F2 (described further below) of a channel CH′, the reduction in the multi-path effects will be −24 dB compared to a situation with no external spatial isolation. The spatial component α_A(x)<<1 is obtained.

Thus, thanks to external spatial isolation, the spatial component α_A(x) of the signal received by a terrestrial terminal 6 is reduced, thus increasing overall rejection.

It is thus irrelevant that the frequential component α_F(F) might be large. It is thus irrelevant that a terrestrial terminal 6 uses a channel border frequency (described further below). It will not be too disturbed by a signal replica since this replica will be well filtered.

It should be noted that, in each case, the amplification device HPA of the same regeneration chain 100 makes it possible to reduce intrinsically the rate of rejection by 20 dB.

It should be noted that, in practice, for external spatial isolation, the transmission antennas A_TX are assembled at the factory site, wherein an input of the antennas is configured so that they transmit in the desired direction of polarisation and they are assembled together and associated with the different regeneration chains 100 in such a way that the transmission antennas A_TX associated with the same regeneration chain 100 transmit two radiofrequency signals to two different non-contiguous cells.

With Isolation by Polarisation

In a non-limiting embodiment, so as to further reduce the spatial component α_A(x), the transmission antennas A_TX1, A_TX2 associated with a regeneration chain 100 are also able to transmit two regenerated radiofrequency signals SP having orthogonal directions of polarisation.

Thus, the two radiofrequency signals RF having mutually orthogonal directions of polarisation are destined for two cells which are not adjacent but which are paired as follows:

• • a green cell (left-hand circular polarisation) and a yellow cell (right-hand circular polarisation); or
  • a red cell (left-hand circular polarisation) and a blue cell (right-hand circular polarisation).

With reference to FIG. 6, which illustrates part of the coverage area of the Ka-band of FIG. 2, in this case for example the antennas A_TX1 and A_TX2 of the same regeneration chain 100 will be able to radiate respectively:

• • a radiofrequency signal SP33 destined for a cell C33 (green cell) and a radiofrequency signal SP21 destined for the non-adjacent cell C21 (yellow cell) and
  • a radiofrequency signal SP33 destined for a cell C33 (green cell) and a radiofrequency signal SP25 destined for the non-adjacent cell C25 (yellow cell).

In this way, the antennas A_TX1 and A_TX2 will be able to radiate, respectively, these radiofrequency signals SP33 and SP21 or SP33 and SP25 having mutually orthogonal directions of polarisation and destined for the non-adjacent cells C33 and C21 or C33 and C25 respectively, said cells belonging to the same cell planning N, as illustrated in FIG. 6.

The cells C33 and C21 have an edge-to-edge distance Dc measuring half a diameter θ_C of a cell (case a)).

The cells C33 and C25 have an edge-to-edge distance Dc measuring 1.3 times the diameter θ_C of a cell (case b)).

Likewise, for example, the antennas A_TX1 and A_TX2 of the same regeneration chain 100 will be able to radiate, respectively:

• • a radiofrequency signal SP34 destined for a cell C34 (red cell) and a radiofrequency signal SP22 of the non-adjacent cell C22 (blue cell) and/or
  • a radiofrequency signal SP34 destined for a cell C34 (red cell) and a radiofrequency signal SP26 of the non-adjacent cell C26 (blue cell).

In this way, the antennas A_TX1 and A_TX2 will be able to radiate, respectively, these radiofrequency signals SP34 and SP22 or SP34 and SP26 having mutually orthogonal directions of polarisation and destined for the non-adjacent cells C34 and C22 or C34 and C26 respectively, said cells belonging to the same cell planning N, as illustrated in FIG. 6.

The cells C34 and C22 have an edge-to-edge distance Dc measuring half a diameter θ_C of a cell (case a)).

The cells C34 and C26 have an edge-to-edge distance Dc measuring 1.3 times the diameter θ_C of a cell (case b)).

A terrestrial terminal 6 positioned in a green cell for example will thus receive:

• • a first regenerated radiofrequency signal SP1 destined for said green cell which will be in the right-hand circular direction of polarisation.
  • signal replica R_SP1 which will be in the left-hand circular direction of polarisation.

The multi-path effects will be reduced thanks to the discrimination by polarisation of the terminal 6. In a non-limiting example, the effects will be reduced by approximately 20 dB for isolation by polarisation alone.

The regenerated radiofrequency signal SP received by the terrestrial terminal 6 destined for the cell C in which the terminal 6 is located will be filtered by a first filter 19, of which the attenuation curve is shown in FIG. 7 (by a dashed line), and the replica R_SP of this signal will be filtered by a second filter 19, of which the attenuation curve (solid line) will be reduced by 20 dB as a result of the discrimination by polarisation and the orthogonal directions of polarisation. The signal replica R_SP therefore will not generate too much interference on the regenerated radiofrequency signal SP received by the terminal 6.

Isolation by polarisation of the radiofrequency signal SP destined for the cell C in which the terrestrial terminal 6 is located is thus obtained.

Combined with external spatial isolation, isolation by polarisation gives the following results. The same explanations as those given above with regard to filtering by the different lobes can be applied in this case, wherein the cell 13 is replaced by the cell 21, and the cell 11 is replaced by the cell 25.

Case a) C33 and C21

In the case of external spatial isolation of a half-cell (Dc=0.5), a terrestrial terminal 6 positioned in a green cell, cell C33 for example, will receive:

• • a first regenerated radiofrequency signal SP33 destined for said green cell; and
  • a signal replica R_SP33 filtered by the primary lobe Lb1′ of the radiation of the antenna which transmits in the direction of the non-adjacent yellow cell C21.

In combination with isolation by polarisation, an overall reduction by 38 dB is thus achieved.

Case b) C33 and C25

In the case of external spatial isolation of 1.3 times cell diameter (Dc=1.3), a terrestrial terminal 6 positioned in a green cell, cell C33 for example, will receive:

• • a first regenerated radiofrequency signal SP33 destined for said green cell; and
  • a signal replica R_SP33 filtered by a secondary lobe Lb2′ of the radiation of the antenna which transmits in the direction of the non-adjacent yellow cell C25.

In combination with isolation by polarisation, an overall reduction by 44 dB is thus achieved.

Thanks to external spatial isolation and additional isolation by polarisation of the regenerated radiofrequency signals SP, the spatial component α_A(x) of the signal received by a terrestrial terminal 6 is thus reduced, thereby increasing overall rejection.

It is thus irrelevant that the frequential component α_F(F) might be large. It is thus irrelevant that a terrestrial terminal 6 uses a channel border frequency (described further below). It will not be too disturbed by a signal replica since this replica will be well filtered.

It should be noted that, in practice, for isolation by polarisation and for external spatial isolation, the transmission antennas A_TX are assembled at the factory site, wherein an input of the antennas is configured so that they transmit in the desired direction of polarisation and they are assembled together and associated with the different regeneration chains 100 in such a way that the transmission antennas A_TX associated with the same regeneration chain 100 transmit two radiofrequency signals having orthogonal directions of polarisation to two different non-contiguous cells.

It should be noted that the multi-path effects can also be reduced by:

• • 1) internal spatial isolation if a terrestrial terminal 6 is far from a cell edge, and
  • 2) frequential isolation if a terrestrial terminal 6 receives a regenerated radiofrequency signal SP which uses a middle frequency of the channel CH′.

As will be seen hereinafter, applied to isolation by polarisation and to external spatial isolation, this reduces the multi-path effects even further.

Internal Spatial Isolation

So as to explain internal spatial, isolation, the situation in which the regenerated radiofrequency signals SP transmitted by transmission antennas of the same regeneration chain 100 are transmitted in the direction of the adjacent cells C and have orthogonal directions of polarisation will be considered.

FIGS. 8, 9 and 10 illustrate, in a non-limiting example, the radiation of the antennas of the same regeneration chain 100, said antennas radiating regenerated signals SP in the direction of two cells and the regenerated radiofrequency signals SP having different frequency bands and orthogonal directions of polarisation, for example in the direction of a green cell and in the direction of a yellow cell.

On the abscissa, THETA represents the position of an imaginary observer, which would move along cells C located over the path of a section CC′ of FIG. 6, FIG. 6 showing part of the frequency plan of cells C assigned to the Ka-band.

On the ordinate, EIRP represents the radiation of an antenna which is representative of the power of a regenerated radiofrequency signal SP received by a cell C, called the effective isotropically radiated power or equivalent isotropically radiated power (EIRP).

It should be noted that, as illustrated in FIGS. 8, 9 and 10, the radiation of an antenna in the direction of a cell includes a main lobe Lb0, Lb0′, Lb0″, a primary lobe Lb1, Lb1′, Lb1″, and a secondary lobe Lb2, Lb2′, Lb2″.

As can be seen in FIG. 6, the cells C14, C23, C33, C42 and C52 are arranged along the section CC′.

The green cells are the cells C14, C33 and C52 and the radiation of the respective associated antennas are shown by dots.

The yellow cells are the cells C23 and C42 and the radiation of the respective associated antennas are represented by solid lines.

When a terrestrial terminal 6 which is not sensitive to the direction of polarisation of a regenerated radiofrequency signal SP (it does not discriminate by polarisation) is located at the edge of a cell, for example next to the cell C33 (position THETA=2 approximately), it can be seen that it will receive the regenerated radiofrequency signal SP33 associated with cell C33 as well as its replica R_SP33 with the same power of approximately −3 dB, the latter being filtered by the main lobe Lb0′ (solid lines) of the antenna associated with cell C23. The multi-path effect is thus significant. The terrestrial terminal 6 will be disturbed by said signal replica R_SP33, The spatial component α_T(x)≈1 of the signal received by the terrestrial terminal 6 is thus obtained, as illustrated in FIG. 9, which is an enlarged view of part of FIG. 8.

By contrast, when a terrestrial terminal 6 is located in the middle of a cell, for example in the middle of cell C33 (position THETA=0), it can be seen that it will receive the regenerated radiofrequency signal SP33 with a maximum power of 0 dB and the signal replica R_SP33 with a power of approximately −20 dB, the latter being filtered by the first lobe Lb1′ (solid lines) of the antenna associated with cell C23. The multi-path effect is thus negligible. The spatial component α_A(x)<<1 of the signal received by the terrestrial terminal 6 is thus obtained, as illustrated in FIG. 9, which is an enlarged view of part of FIG. 8.

FIG. 10 applies to the same arrangement of cells as in FIG. 8, but when a terrestrial terminal 6 is sensitive to the direction of polarisation of a regenerated radiofrequency signal SP.

In this case, when a terrestrial terminal 6 is located at the edge of a cell C, for example next to the cell 33 (position THETA=2 approximately), it can be seen that it will receive the regenerated radiofrequency signal SP33 associated with cell C33 with a power of approximately −3 dB and its replica R_SP33 with a lower power of approximately −17 dB, the latter being filtered by the main lobe Lb0′ (solid lines) of the antenna associated with cell C23. The multi-path effect produced is thus less significant than when the terminal 6 does not discriminate by polarisation.

By contrast, when a terrestrial terminal 6 is located in the middle of a cell C, for example in the middle of cell C33 (position THETA=0), it can be seen that it will receive the regenerated radiofrequency signal SP33 with a maximum power of 0 dB and it will not receive its replica R_SP33. The multi-path effect produced is thus non-existent in this case.

Frequential Isolation

So as to explain internal frequential isolation, the situation in which the regenerated radiofrequency signals SP transmitted by transmission antennas of the same regeneration chain 100 have the same direction of polarisation and are transmitted towards non-adjacent cells will be considered.

In FIG. 11, in a non-limiting example, the dashed curve represents the attenuation curve of a first filter 19 of a regeneration chain 100 for filtering the regenerated radiofrequency signals SP destined for a green cell when a terminal 6 is located in a green cell, whereas the solid curve represents the attenuation curve of the second filter of the same regeneration chain 100 for filtering the radiofrequency signals destined for a non-adjacent red cell, the replica of a signal R_SP destined for the green cell thus passing through this filter.

As can be seen, if a terrestrial terminal 6 uses a middle frequency F1 located in the middle of the frequency band of an associated downlink channel CH′, the rejection Rej1 of the filter 19 will be high and the frequential component α_F(F) of the signal received will therefore by very low. The terrestrial terminal 6 will not be disturbed by the replica of the signal R_SP.

α_F(F1)<<1 is thus obtained. The frequency F1 used is far from the limits of the frequency band of the downlink channel CH′ used and is thus far from any other adjacent frequency band.

By contrast, the situation is very different if a terrestrial terminal 6 uses a border frequency F2 which is located at the edge of the frequency band of an associated downlink channel CH′ and therefore close to the frequency band of a channel CH′ associated with a non-adjacent cell.

In FIG. 11, this frequency is located on the descending slope of the attenuation curve of the filter 19. In this case, the rejection Rej2 of the filter 19 will thus be low and the frequential component α_F(F) of the received signal will thus be high. The terrestrial terminal 6 will be disturbed by the replica of the signal R_SP. α_F(F2)≈1 is thus obtained. The frequency F2 used is close to the limits of the frequency band of the downlink channel CH′ used and is therefore close to any other adjacent frequency band.

It should be noted that the second border frequency F2 defines a guard band for the green cell with a third frequency F3 illustrated in FIG. 11, the latter frequency being located next to the attenuation curve of the first filter 19 (represented by a dashed line).

It should be noted that, in a known earlier prior art, this guard band is generally defined in such a way that the radiofrequency signal destined for the red cell is sufficiently filtered so as not to disturb the radiofrequency signal destined for the green cell, and the replica of the signal is therefore sufficiently filtered. The guard band is therefore quite large. For example, the third frequency F3 is located between 10 and 20 MHz below the second frequency F2. Likewise, as is known from the prior art, a guard band with a fourth frequency F4 is defined for the red cell. The fourth frequency F4 is located between 10 and 20 MHz above the second frequency F2 and next to the attenuation curve of the second filter 19 (represented by a solid line).

Thus, in a non-limiting example, if the frequency band of the channel is from 19.7 to 19.95 GHz, F1 would be located between 19.7 GHz and 19.95 GHz less the guard band of 20 MHz for example (therefore where the rejection of the filter is significant, that is to say 20 dB), whereas the border frequency F2 would be located at 19.95 GHz (that is to say in the middle of the overall bandwidth from 19.7 to 20.2 GHz).

Internal spatial isolation and frequential isolation thus give the following results when applied to external spatial isolation.

Internal Spatial Isolation and Frequential Isolation Applied to External Spatial Isolation

Case a): External Spatial Isolation of a Half-Cell (Dc=0.5)

Applied to spatial isolation of a half-cell, the following results are thus obtained:

1) internal spatial isolation if the terrestrial terminal 6 is positioned far from a border of the cell C: This isolation will thus be approximately 20 dB, leading to a total reduction of 38 dB;2) additional frequential isolation if a middle frequency F1 of a channel CH′ is used: This isolation will thus be approximately 20 dB, leading to a total reduction of 38 dB without internal spatial isolation 1) or 58 dB with internal spatial isolation 1).

The multi-path effects on the ripple produced over the regenerated radiofrequency signal SP are shown in FIG. 12, where the amplitude PPR of the ripple is plotted on the abscissa and the overall rejection REJ, which represents the regrouped effect of the frequential α_F(F) and spatial α_A(x) components, as seen before, is plotted on the ordinate.

As can be seen, in the case with external spatial isolation of a diameter Dc=0.5, at the edge of a cell and at a border frequency F2, the amplitude of the ripple is 2.2 dB, as indicated at point PT1 in FIG. 12.

In the case of addition of internal spatial isolation 1), in the centre of the cell, the amplitude of the ripple decreases to 0.22 dB, as indicated at point PT2 in FIG. 12.

In the case of addition of additional frequential isolation 2), with use of a middle frequency F1, the amplitude of the ripple decreases to 0.02 dB, as indicated at point PT3 in FIG. 12 and becomes negligible.

Case b): in the Case of External Spatial Isolation of Diameter Dc=1.3)

Applied to spatial isolation of a cell diameter of 1.3, the following results are thus obtained:

1) internal spatial isolation if the terrestrial terminal 6 is positioned far from a border of the cell C: This isolation will thus be approximately 20 dB, leading to a total reduction of 44 dB; and/or2) additional frequential isolation if a middle frequency F1 of a channel CH′ is used: This isolation will thus be approximately 20 dB, leading to a total reduction of 44 dB without internal spatial isolation 1) or 64 dB with internal spatial isolation 1).

As can be seen, in the case with external spatial isolation of a diameter Dc=1.3, at the edge of a cell and at a border frequency F2, the amplitude of the ripple is 1.1 dB and is located at point PT1 in FIG. 12.

In the case of addition of internal spatial isolation 1), in the centre of the cell, the amplitude of the ripple decreases to 0.11 dB and is located at point PT2 in FIG. 12.

In the case of addition of additional frequential isolation 2), with use of a middle frequency F1, the amplitude of the ripple decreases to 0.01 dB and is located at point PT3 in FIG. 12 and becomes negligible.

Applied to isolation by polarisation combined with external spatial isolation, the following results are thus obtained:

Internal Spatial Isolation and Frequential Isolation Applied to Isolation by Polarisation Combined with External Spatial Isolation

Case a): External Spatial Isolation of a Half-Cell (Dc=0.5)

Applied to spatial isolation of a half-cell, the following results are thus obtained:

1) internal spatial isolation if the terrestrial terminal 6 is positioned far from a border of the cell C: This isolation will thus be approximately 20 dB, leading to a total reduction of 60 dB;2) additional frequential isolation if a middle frequency F1 of a channel CH′ is used: This isolation will thus be approximately 20 dB, leading to a total reduction of 60 dB without internal spatial isolation 1) or 80 dB with internal spatial isolation 1).

As can be seen, in the case with isolation by polarisation in combination with external spatial isolation, at the edge of a cell and at a border frequency F2, the amplitude of the ripple PPR is 0.22 dB, as indicated at point PT2 in FIG. 12.

In the case of additional internal spatial isolation 1), in the centre of the cell, the amplitude of the ripple decreases to 0.02 dB, as indicated at point PT3 in FIG. 12.

In the case of additional frequential isolation 2), with use of a middle frequency F1, the amplitude of the ripple decreases to 0.002 dB and thus cannot be measured using conventional measuring instruments.

Case b): in the Case of External Spatial Isolation of Diameter Dc=1.3)

Applied to spatial isolation of a cell diameter of 1.3, the following results are thus obtained:

1) internal spatial isolation if the terrestrial terminal 6 is positioned far from a border of the cell C: This isolation will thus be approximately 20 dB, leading to a total reduction of 64 dB; and/or2) additional frequential isolation if a middle frequency F1 of a channel CH′ is used: This isolation will thus be approximately 20 dB, leading to a total reduction of 64 dB without internal spatial isolation 1) or 84 dB with internal spatial isolation 1).

Table 1, below, summarises the situations described above when a terrestrial terminal 6 is located next to a cell C.

		Isolation by
		polarisation +
	External spatial	external spatial
	isolation only Dc = 0.5	isolation Dc = 0.5
	Suppression of		Suppression of
	multi-path		multi-path
Frequency	effects	PPR	effects	PPR
F1	38 dB	0.22 dB	60 dB	0.02 dB
F2	18 dB	2.2 dB	40 dB	0.2 dB
		Isolation by
		polarisation +
	External spatial	external spatial
	isolation only Dc = 1.3	isolation Dc = 1.3
	Suppression of		Suppression of multi-
Frequency	multi-path effects	PPR	path effects
F1	44 dB	0.11 dB	64 dB
F2	24 dB	1.1 dB	44 dB

with

		Amplification	Internal
		device	spatial	Isolation by
	Frequency	Rejection	isolation	polarisation
	F1	20 dB	0 dB	20 dB
	F2	0 dB	0 dB	20 dB

Table 2, below, summarises the situations described above when a terrestrial terminal 6 is located far from the edge of a cell C (there is internal spatial isolation)—in the middle in a non-limiting example.

		Isolation by
	External spatial	polarisation + external
	isolation only Dc = 0.5	spatial isolation Dc = 0.5
	Suppression of		Suppression of
	multi-path		multi-path
Frequency	effects	PPR	effects	PPR
F1	58 dB	0.02 dB	80 dB	0.002 dB
F2	38 dB	0.22 dB	60 dB	0.02 dB
	External spatial	Isolation by
	isolation only Dc = 1.3	polarisation + external
	Suppression of		spatial isolation Dc = 1.3
	multi-path		Suppression of multi-
Frequency	effects	PPR	path effects
F1	64 dB	0.01 dB	84 dB
F2	44 dB	0.11 dB	64 dB

with

		Amplification	Internal
		device	spatial	Isolation by
	Frequency	Rejection	isolation	polarisation
	F1	20 dB	20 dB	20 dB
	F2	0 dB	20 dB	20 dB

Thus, in the forward link, not only has the number of components used been reduced, but the multi-path effects (signal replica) generated by the regenerated radiofrequency signals have also been reduced.

Return Link

The return link of the terrestrial terminals 6 to the terrestrial station 2 functions identically to a reverse direction of communication.

In a non-limiting embodiment, the polarisations are reversed over the return link so that the colours red and green have left-hand circular polarisation and the colours blue and yellow have right-hand circular polarisation. The terrestrial terminals 6 transmit and receive according to reverse polarisation so that the signals of the return link uplink LM2 can be easily separated from the signals of the forward link downlink LD1. Such a configuration makes it possible to use less costly terminals.

A return link payload 10 for a multi-beam satellite 3, return link allowing receipt of regenerated radiofrequency signals SP from at least one terrestrial terminal 6 and re-transmission of said signals to at least one main terrestrial station 2, is described in a non-limiting embodiment in FIG. 13.

In particular, this return link payload comprises:

• • at least one reception antenna, A_RX for receiving radiofrequency signals SP, each signal coming from a basic coverage area, the reception antennas A_RX being able to receive radiofrequency signals SP destined for the same regeneration chain 200 from basic non-contiguous coverage areas C, said basic coverage areas belonging to a single cell planning which uses at least two frequency bands and two different polarisations; and
  • a regeneration device REP for regenerating radiofrequency signals by filtering, frequency transposition and amplification, comprising a plurality of regeneration chains 200, each chain comprising an amplification device HPA able to amplify a plurality of radiofrequency signals having different frequency bands; and
  • transmission antennas A_TX for transmitting polarised regenerated radiofrequency signals to at least one main terrestrial station 2.

The return link payload 10 functions as follows:

In a first step 1), the reception antennas A_RX for receiving the payload 10 receive polarised radiofrequency signals SP. These radiofrequency signals SP are sent by one or more terrestrial stations 6 over an uplink LM2.

FIGS. 14 and 15 illustrate a frequency plan using the colour pattern described previously and broken down as follows:

• • an uplink frequency plan. PMVR over the return link; and
  • a downlink frequency plan PDVR over the return link.

The notations RHC and LHC refer to the right-hand and left-hand circular directions of polarisation respectively.

In the example of the Ka-band, the PMVR plan corresponding to the uplink LM2 over the return link (from a terrestrial station 6 to the multi-beam satellite 3) has two frequency intervals [29.5; 29.75] and [29.75; 30].

The plan PDVR corresponding to the downlink LD2 over the return link (from the multi-beam satellite 3 to the main terrestrial station) has 2′GHz (from 17.7 to 19.7 GHz) of available frequency spectrum.

Radiofrequency signals SP will thus be distributed over four channels of 250 MHz bandwidth (associated with a frequency interval from the two frequency intervals [29.5; 29.75] and [29.75; 30] and polarised according to the directions of polarisation RHC or LHC, as shown over the uplink frequency plan PMVR in FIG. 14, provided by the terrestrial terminals 6 of the cells.

These radiofrequency signals are regenerated (by filtering, frequency transposition, amplification) at the multi-beam satellite 3 so as to be re-sent in the form of polarised radiofrequency signals RF to the main terrestrial station 2 via eight channels for each direction of polarisation.

In the example of FIG. 15, the channels CH′17 to CH′24 are provided for the first direction of polarisation (left-hand circular LHC for example) and channels CH′25 to CH′32 are provided for the second direction of polarisation (right-hand circular RHC), as shown in the downlink frequency plan PDVR in FIG. 15.

A terrestrial terminal 6 distributes radiofrequency signals SP over four channels CH of 250 MHz bandwidth (two channels for each direction of polarisation). These radiofrequency signals SP distributed over these four channels after processing by the payload 10 of the multi-beam satellite 3 will form polarised radiofrequency signals RF, as will be seen below.

It is still assumed that the entire spectrum of 2 GHz is used. However, it should be noted that it is also possible, in another non-limiting embodiment and in particular for operational reasons, for only part of the spectrum to be used and for fewer channels CH to be generated.

In the example above, the return link payload 10 thus receives radiofrequency signals SP distributed over the four channels CH of different frequency bands.

The radiofrequency signals SP multiplexed over the channels CH are then processed at the payload 10 of the multi-beam satellite 3 so as to provide radiofrequency signals RF, each of these radiofrequency signals RF being distributed over the downlink channels CH′ associated with a direction of polarisation. RHC or LHC and over frequency bands in accordance with the downlink frequency plan PDVR.

The reception antennas A_RX associated with a regeneration chain 200 are able to receive the radiofrequency signals SP destined for said regeneration chain 200 from non-contiguous cells C.

In a first non-limiting embodiment of this mode, the non-contiguous cells are separated by half a cell diameter.

In a second non-limiting embodiment of this mode, the non-contiguous cells are separated by a cell diameter equal to 1.3.

In a third non-limiting embodiment of this mode, the non-contiguous cells are separated by a cell diameter equal to 1.6.

In a second step 2), the regeneration device REP for regenerating radio frequency signals SP regenerates said signals by filtering, frequency transposition and amplification.

The regeneration device REP is called a repeater and, in a non-limiting embodiment as illustrated in FIG. 13, comprises ten regeneration chains 200, each chain making it possible to manage radiofrequency signals SP and to regenerate said signals so as to transmit them to associated antennas designed to radiate in the direction of eight cells C.

It is recalled that there are 80 cells for the Ka-band.

In a non-limiting embodiment; a regeneration chain 200 comprises:

• • one low noise amplifier 22 (LNA) for amplifying the radiofrequency signals SP as a function of the noise generated by the components of the regeneration chain 200;
  • one frequency converter circuit CONV formed:
    • by a local oscillator 24 for frequency translating the two radiofrequency signals and for adjusting them over eight channels CH′ in accordance with the frequency plan of the downlink PDVR. In the case of the Ka-band, each of these channels CH′ is associated with a frequency band from the frequency bands included in the interval [17.7; 19.7] and with polarisation RHC or LHC, as shown in the downlink frequency plan PDVR for the return link in FIG. 14; and
    • by an input filter 25 for filtering the part of the signal useful for amplification in the radiofrequency
  • a multiplexer 23 (with eight inputs and one output in a non-limiting example) for regrouping all the frequency transposed signals over the same amplifier HPA; and
  • one amplification device which is a high power amplifier (EPA) formed, in a non-limiting embodiment, by a channel amplifier 27 (CAMP) and a travelling wave tube amplifier 28 for amplifying each of the regrouped signals.

At the output of a regeneration chain 200, regenerated radiofrequency signals RF will thus be distributed over 8 downlink frequency Channels CH′ (also called output channels).

Thus, at the output of a repeater REP, regenerated radiofrequency signals will thus be distributed over 16 downlink frequency channels CH′17 to CH′32, as illustrated in FIG. 15.

The use of a regeneration chain 200 to manage the radiofrequency signals SP thus makes it possible to reduce the number of components used in the payload 10.

In addition, the radiofrequency signals SP received and managed by a regeneration chain 200 have different frequency bands. This makes it possible to differentiate between them in the regeneration chain 200, in particular at the converter CONV.

It should be noted that the management of the radiofrequency signals SP in the same regeneration chain 200 may lead to multi-path effects (signal replica), as in the case of the forward link, but this time at the inputs of the payload 10, in particular at the reception antennas A_RX and at the low noise amplifiers LNA and the converters CONV of the regeneration chains 200. These effects lead to poor reception of said radio signals RF by the main terrestrial station 2. These effects R_SP are illustrated in FIG. 13.

As in the case of the forward link, in order to overcome this problem, the reception antennas are able to receive the radiofrequency signals SP destined for the same regeneration chain 200 from basic coverage areas C, which are not contiguous, as described above.

In addition, in a non-limiting embodiment, in order to further overcome this problem, the radiofrequency signals SP received and managed by a regeneration chain 200 have different frequency bands.

It should be noted that; in non-limiting embodiments; the transmission antennas A_RX (from the multi-beam satellite 3 to a main terrestrial station 2) for the return link are the reception antennas A_RX for the forward link (from the main terrestrial station 2 to the multi-beam satellite 3). It is sufficient to configure one of the inputs of an antenna for transmission and to configure the other for reception.

It is the same for the reception antennas A_RX in the return link (terrestrial terminals 6 to the multi-beam satellite 3), which are the transmission antennas A_TX in the forward link (from the multi-beam satellite 3 to the terrestrial terminals 6).

It should be noted that the same explanations as those given for the forward link payload can be used in the return link for external spatial isolation.

Similarly to the forward link, not only will the number of components used in the return link thus be reduced, but the multi-path effects will also be reduced.

Of course, the invention is not limited to the embodiments described above.

The invention has thus been described more specifically in the case of an amplifier formed by a CAMP followed by a TWTA. However, it should be noted that, in non-limiting examples, the invention can also be applied to the case of an amplifier of the SSPA type (solid state power amplifier) or to more sophisticated architectures of the MPA type (multipoint amplifier).

In addition, the example of circular polarisation has been considered as a non-limiting example. Of course, the invention can also be applied to other types of polarisation, for example linear or elliptical polarisation.

Moreover, the example of the Ka-band has been considered as a non-limiting example. Of course, the invention can be applied to other bands representing areas other than Europe.

Lastly, the downlink bandwidth in the forward link between 19.7 GHz and 20.2 GHz and the uplink bandwidth in the return link between 29.5 GHz and 30.0 GHz have been considered as a non-limiting example, since users do not require a licence in these two bandwidths. Of course; other bandwidth ranges can be used. It will be noted that, in general, a user will be assigned his transmission and reception frequencies by a satellite telecommunications network operations centre in accordance with known mechanisms of the DAMA type (demand assigned multiple access).

Lastly, in a non-limiting embodiment, an amplification chain 100 may comprise a plurality of low noise amplifiers (LNA) 12, each cooperating with a plurality of signal divider devices 13 (demultiplexers), the latter each cooperating with a plurality of frequency converter circuits CONV, the set of converter circuits CONV cooperating with the amplification device HPA of the regeneration chain 100. Of course, other variants of this embodiment can be considered, such as only having a single low noise amplifier cooperating with a plurality of signal divider devices 13.

The same non-limiting embodiment can be applied a regeneration chain 200.

The invention thus provides the following advantages:

• • it makes it possible to reduce the guard band between two filters 19 of the same regeneration chain 100 and to thus increase the bandwidth which can be used to transmit the regenerated radiofrequency signals;
  • it is easily implemented;
  • it makes it possible to influence only a single component of the received signal, in this case the spatial component, without disturbing the frequential component;
  • it allows a terrestrial terminal to receive correctly the regenerated radiofrequency signal SP destined for said terminal without too much interference by the signal replica;
  • it allows a main terrestrial station to receive correctly the regenerated radiofrequency signal RP destined for said station without too much interference by the signal replica;
  • it makes it possible to reduce the cost of the multi-beam satellite thanks to the reduction in the number of components in the payload of said satellite;
  • it makes it possible to use only terrestrial terminals which are designed to manage only a single polarisation, a terrestrial terminal being located in a cell able to receive a radiofrequency signal of a given polarisation; such a terrestrial terminal is thus less complex and less expensive than a terrestrial terminal which has to manage two polarisations, as in the prior art where two cell plannings are used;
  • it makes it possible to achieve greater efficacy in terms of re-use of frequencies compared to the prior art since it uses a four-colour pattern instead of a six-colour pattern: With the four-colour pattern, more band frequency will be used for all cells over a given surface area compared to with a six-colour pattern. In a non-limiting example, for a frequency band of 500 MHz and for 100 cells, 25 GHz will thus be used for the four-colour pattern compared to 16.6 GHz for the six-colour pattern; and
  • it makes it possible for end users to use the Internet by means of satellite telecommunication. This is useful in particular when the users are isolated without means for Internet access by a standard wireline.

Claims

1. A forward link payload for a multi-beam satellite, a forward link allowing receipt of radiofrequency signals from at least one main terrestrial station so as to re-transmit said signals to at least one terrestrial terminal, said payload comprising: at least one reception antenna configured to receive polarised radiofrequency signals;a regeneration device configured to regenerate radiofrequency signals by filtering, frequency transposition and amplification; andtransmission antennas configured to transmit the regenerated radiofrequency signals to at least one terrestrial terminal, each signal being destined for a basic coverage area, wherein the regeneration device comprises a plurality of regeneration chains, each chain comprising an amplification device configured to amplify a plurality of radiofrequency signals having different frequency bands, and wherein the transmission antennas are configured to transmit regenerated radiofrequency signals, via a single regeneration chain, to non-contiguous basic coverage areas, said basic coverage areas belonging to a single cell planning which uses at least two frequency bands and two different polarisations.

2. The payload according to claim 1, wherein the transmission antennas associated with a regeneration chain are configured to transmit two regenerated radiofrequency signals having orthogonal directions of polarisation.

3. The payload according to claim 1, wherein the amplification device comprises a channel amplifier and a travelling wave tithe amplifier.

4. A return link payload for a multi-beam satellite, a return link allowing receipt of radiofrequency signals from at least one terrestrial terminal and re-transmission of said signals to at least one main terrestrial station, said payload comprising: at least one reception antenna configured to receive radiofrequency signals, each signal being associated with a basic coverage area;a regeneration device configured to regenerate radiofrequency signals by filtering, frequency transposition and amplification; andtransmission antennas configured to transmit the polarised regenerated radiofrequency signals to at least one main terrestrial station, wherein the regeneration device comprises a plurality of regeneration chains, each chain comprising an amplification device configured to amplify a plurality of radiofrequency signals having different frequency bands, and wherein the reception antennas are configured to receive radiofrequency signals destined for the same regeneration chain from non-contiguous basic coverage areas, said basic coverage areas belonging to a single cell planning which uses at least two frequency bands and two different polarisations.

5. The payload according to claim 1, wherein the amplification device comprises a channel amplifier and a travelling wave tube amplifier.

6. A multi-beam satellite comprising a payload, comprising a forward link according to claim 1.

7. A telecommunications network for establishing radiofrequency links between at least one main terrestrial station and at least one terrestrial terminal via a multi-beam telecommunications satellite, said network comprising at least one main terrestrial station, at least one terrestrial terminal, and a multi-beam telecommunications satellite, in accordance with which the multi-beam satellite comprises a payload according to claim 1.

8. A multi-beam satellite comprising a payload, comprising a forward link, and a return link according to claim 4.

9. A telecommunications network for establishing radiofrequency links between at least one main terrestrial station and at least one terrestrial terminal via a multi-beam telecommunications satellite, said network comprising at least one main terrestrial station, at least one terrestrial terminal, and a multi-beam telecommunications satellite, in accordance with which the multi-beam satellite comprises a payload according to claim 4.