MULTI-ANTENNA GROUND STATION FOR IMPLEMENTING A TRANSPARENT SWITCH WITH DIVERSITY FROM A SAILING SCR

专利摘要:
A ground station with individual satellite tracking antennas from a first starting satellite S1 and a second passing satellite S2 comprises, connected in series, a multi-channel reception and processing device (122) and a communication device. configurable diversity combination (124), and includes a transparent diversity and failover management device (126) for a reception communication link from the first originating satellite S1 to the second destination satellite S2. The transparent diversity and failover management device (126) is configured to manage and co-ordinate the execution of a succession of k transparent and unitary antenna k-switches, and during each transparent and unitary switchover Bi, to control the antennas ( 112, 114, 116), the multichannel reception and processing device (122) and the configurable diversity combining device (124) by determining and sending respectively: * satellite acquisition pointing commands, and the time and phase alignment commands of the P signals received at the input of the multi-channel reception and processing device produced as a function of time difference measurements and in phase of P-1 signals received as input with respect to the signal. received as a reference signal, and. * a selection set of processed output signals to be combined according to the planning of the switchover of the first signal. re C1 diversity configuration to the second configuration C2 diversity and function signals quality measurements received at the input of the receiving and processing device.
公开号:FR3066664A1
申请号:FR1700518
申请日:2017-05-16
公开日:2018-11-23
发明作者:Mathieu Arnaud；Jean Francois Boutillon；Jean Luc Almeida
申请人:Thales SA；
IPC主号:

专利说明:

Multi-antenna ground station for implementing transparent switching with diversity from a starting moving satellite to a moving moving satellite, and corresponding switching method
The present invention relates to a multi-antenna ground station, for accessing a constellation of scrolling telecommunications satellites, and capable of implementing transparent switching with diversity of a communication link from a departure satellite to a destination satellite , and a corresponding tilting method
On telecommunications satellite systems using a constellation of satellites traveling on HEO (in English High Earth Orbit) or MEO (in English Medium Earth Orbit) or LEO (Low Earth Orbit) type orbits, and fixed or mobile ground stations forming terminals of the satellite access system, the use of at least two antennas is required to allow a switchover (in English "handover") of the communication link providing the service provided to the ground station from a first satellite descending from departure at the end of visibility on a second ascending destination satellite at the start of visibility, as soon as the antennas of ground stations are directional.
So far, the multi-antenna ground stations, manufactured or which have been proposed, have two antennas and use only one of them during the whole period between two consecutive failovers. Furthermore, during the implementation of a switchover, these ground stations require a double demodulation chain.
Recently ground stations have appeared which allow the reception of the same carrier from the same satellite pointed by the two antennas between two link switches, and thus achieve diversity of reception on the two antennas.
Patent application EP 2 779 482 A1 describes the architecture of such a ground station with two antennas which makes it possible to process in diversity only the signal received from two antennas coming from the same satellite.
The architecture described in the aforementioned document, and the architectures of the ground stations produced and in service to date, do not allow a transparent switchover (in English "seamless") of link between two satellites during which a diversity of reception on at least two antennas pointed at the two satellites can be used to enhance the quality and reliability of the switchover. These architectures also do not allow uninterrupted use of a diversity of multi-antenna reception during a switching of link between two departure and arrival configurations with diversity of antenna reception pointing exclusively on the first satellite for the configuration of departure and on the second satellite for the arrival configuration. These architectures also do not have the required modularity allowing an addition as a new antenna to improve reception performance.
A first technical problem is to propose a ground station architecture having at least two mobile directive antennas which improves the transparency of a link failover between a first satellite and a second satellite.
A second technical problem is to propose a ground station architecture which makes it possible to achieve, during the switching of the reception link, a diversity in reception on at least two antennas, one pointing to the first satellite and another pointing to the second satellite.
A third technical problem is to propose a ground station architecture which allows uninterrupted use of a diversity of multi-antenna reception during a link switching between two departure and arrival configurations with diversity of antenna reception pointing exclusively at the first satellite for the starting configuration and pointing exclusively to the second satellite for the arrival configuration.
A fourth technical problem is to propose a modular architecture which allows the addition of a new antenna as and when necessary to improve reception performance.
A fifth technical problem is to propose a multi-antenna ground station architecture, solution of at least one of the first, second, third, fourth technical problems, which allows, when there is a plurality of at least two antennas pointing towards the same satellite to send to said satellite a plurality of carriers carrying an identical communication signal, said carriers being adapted during transmission to provide a reception of the wavefront of the carriers aggregated in a coherent manner.
To this end, the invention relates to a multi-antenna ground station of a satellite telecommunications system using a constellation of traveling satellites. The ground station includes:
an integer P, greater than or equal to two, of antennas capable of reception each to follow, for the same predetermined period of time, a satellite taken from a first satellite S1 of origin and a second satellite S2 of destination, both in visibility during said period, a multi-channel reception and processing device, with P input terminals, connected respectively to P output terminals of the P antennas, for receiving at input of said device and processing P antenna signals received and output said receiving antennas, and with P output terminals for delivering in parallel P output processed signals, aligned with each other in time and in phase, obtained respectively from the PP antenna signals received, and a configurable diversity combination device, connected in input to the multi-channel reception and processing device, to combine some or all of the processed signals of e output as a function of a selection instruction of the processed output signals and processed signals to be combined, and a diversity management device and transparent switching of a reception communication link from the first original satellite S1 to the second S2 destination satellite.
The ground station is characterized in that the diversity management and transparent tilting device is configured to:
manage and coordinate the execution of a switchover of the communication link from the first satellite S1 of origin to the second satellite S2 of destination, said switchover of the communication link being constituted by a succession of a number k, greater than or equal to 2, of transparent and unitary Bi tilting of antennas, selected according to a predetermined sequence, each transparent and unitary Bi tilting of antenna being a tilting of an antenna from a first configuration of diversity in operational reception C1 (i) in which the selected antenna is pointed with tracking on the first satellite S1, towards a second diversity configuration in operational reception C2 (i) in which the selected antenna is pointed with tracking on the second satellite S2, at least one of the first and second configurations C1 (i), C2 (i) of diversity in reception being a configuration in which the diversity in reception is implemented on the two first and second satellites S1, S2, and during each transparent and unitary switchover Bi (32, 34; 84, 86, 88), check the antennas, the multi-channel reception and processing device and the combination device with configurable diversity by determining and sending them respectively:
. * satellite acquisition pointing commands, and. * time and phase alignment commands for the P signals received at the input of the multi-channel reception and processing device developed as a function of time and phase difference measurements of P-1 signals received at input with respect to the signal received at input taken as reference signal, and. * an instruction for selecting the processed output signals to be combined as a function of the planning of the switching of the first diversity configuration C1 ( i) towards the second diversity configuration C2 (i) and as a function of quality measurements of the signals received at the input of the reception and processing device.
According to particular embodiments, the multi-antenna ground station comprises one or more of the following characteristics:
the integer number P of reception antennas, each capable of pointing and tracking, for the same predetermined period of time, a satellite taken from a first satellite S1 and a second satellite S2, and channels of the reception and processing device is greater than or equal to three, and preferably equal to three, and the first and second configurations C1 (i), C2 (i) of diversity in reception of each unitary transparent switching Bi are each of the configurations in which the diversity in reception is implementation on the two first and second satellites S1, S2, and during each unitary transparent switchover Bi and during the switchover of the communication link, a diversity in reception on at least two antennas is permanently ensured;
the multi-channel reception and processing device (122) is configured to:
. * receive, normalize and filter on P distinct and separate channels, the P received antenna signals output by the P antennas (112, 114, 116), in P normalized and filtered signals, then. * estimate time differences, phase deviations and quality deviations between a normalized and filtered reference signal, taken from among the P normalized and filtered signals, and the remaining P-1 normalized and filtered signals, and supplying said deviations to the management and switching device; then. * for each channel, apply time compensation and phase compensation to the filtered signal associated with the channel from the time alignment and corresponding phase commands, developed and sent by the diversity and switching device;
the multi-channel reception and processing device further comprises a battery of P automatic gain control devices AGC for normalizing the signals received at the input of the multi-channel reception and processing device, and a battery of P band pass filters for filtering normalized signals, for example SRRC filters;
.- the multi-channel reception and processing device also comprises a battery of complex P-1 cross-correlators for estimating time differences, phase differences and quality differences between a normalized and filtered reference signal, taken from among the P normalized and filtered signals, and the P-1 normalized and filtered signals remaining, and supplying said deviations to the management and switching device, by seeking for each crosscorrelator a correlation peak which makes it possible to deduce the time difference between the compared signals , by exploiting the argument of the cross-correlated signal to determine the phase difference between the compared signals, and by exploiting the level of correlation between the compared signals to determine an indication of difference in quality;
.- the multi-channel reception and processing device further comprises a battery of P of delay lines FIFOs with programmable time offset, connected downstream to a battery of multipliers with programmable phase compensation, the multipliers allowing the phase compensations being connected as input to the diversity combination device;
the multi-channel reception and processing device is configured to selectively adjust the gain of each of the channels so as to be able to gradually attenuate the output level of the output signal of a search for an output chain that is desired remove from the diversity combination, and the diversity management and switching device is configured during an antenna switching from the first satellite to the second satellite to control a decreasing gain ramp on the channel to be removed by the combination device diversity, and when the differential quality has exceeded a predetermined threshold commanding the diversity combination device to remove said chain;
.- the multi-antenna ground station comprises a demodulator connected at the output of the diversity combination device and a device for implementing an adaptive modulation control loop ACM, and in which the dynamics of the declining gain ramp is coordinated with the dynamic characteristics of the ACM adaptive modulation control loop;
.- the multi-channel reception and processing device is configured to selectively adjust the gain of each of the channels so as to be able to gradually increase the output level of the output signal of an output chain which it is desired to add in the diversity combination, and the diversity management and switching device is configured for, during a unitary antenna switching from the first satellite to the second satellite and during the phase of attachment of the antenna to the destination satellite, controlling a progressive gain ramp on the chain to be added by the diversity combination device;
.- the diversity management and switching device is configured on detection of an absence of signal on an active chain in the combination to send a withdrawal command to the diversity combination device;
.- the ground station comprises a device for supplying the same source signal to be transmitted in an integer N, less than or equal to P, of supply terminals, and a transmission and processing device for generating on N channels a wave front for a satellite, taken from the first satellite S1 and the second satellite S2, connected at the input to the N supply terminals, and having N emission output terminals connected to N antennas among the P antennas d 'emission or equal to P, to deliver in parallel N processed output signals, shifted between them in time and in phase so that the wave fronts of each antenna are aggregated in satellite reception, and a device for managing diversity in transmission configured to control the multichannel transmission and processing device by determining and sending it time and phase shift commands of the N signals transmitted at the output of the transmission device on and multi-channel processing developed as a function of calibration measurements of the transmission chains, estimates of the contributions internal to the terminal on reception and of the contributions linked to the difference in distance between the transmission channels;
the multi-antenna ground station includes a retroactive calibration chain for the transmission channels, connected to the input ports of the N antennas in transmission mode through connection cable sampling couplers and an N: 1 channel selection switch , calibrated for the internal contributions of the station's transmission channels in terms of differential time and phase differences;
the multichannel transmission and processing device, and the transmission diversity management device are arranged and configured to implement closed-loop compensation for time differences and in phases of the N transmission channels of a diversity configuration in which, the N antennas used in transmission diversity on the pointed satellite are at the same time reception diversity antennas pointing on the same satellite, and send N identical signals shifted between them in time and in phase to generate a coherent wavefront at the pointed satellite, and the transmission diversity management device receives a measurement of the quality of the aggregation of the carriers transmitted by the N antennas in mode, the measurement of the quality of the aggregation of the carriers having been determined in terms of time and phase differences by a receiver from a remote external ground station and retrans set via a terrestrial return channel transmission channel or via a symmetrical return channel channel of the pointed satellite, and corrects the time and phase offset instructions, supplied to the multichannel transmission and processing device, based on temporal differences and phase measured by the external ground station;
the N identical signals, shifted between them in time and in phase to generate a coherent wavefront at the level of the pointed satellite, are signals of an identical reference sequence, and the differential signals of the receiver of the external ground station are determined by correlation, or the N identical signals, shifted between them in time and in phase to generate a coherent wavefront at the level of the pointed satellite, are signals obtained from replicas of the same traffic signal, and the differential signals of the receiver of the external ground station are determined by correlation of the received signal retransmitted by the satellite.
The invention also relates to a method for transparent switching of a communication link in a reception mode or a dual reception / transmission mode from a first satellite S1 of origin to a second satellite S2 of destination. The tilting process is implemented by a ground station comprising:
.- an integer P, greater than or equal to two, antennas capable of receiving each, for the same predetermined period of time, a satellite taken from a first satellite S1 of origin and a second satellite S2 of destination, both visible during said period, .- a multi-channel reception and processing device, with P input terminals, connected respectively to P output terminals of the P antennas, for receiving at input of said device and processing P received antenna signals and supplied at the output of said reception antennas, and at P output terminals for delivering in parallel P processed output signals, aligned with each other in time and in phase, obtained respectively from the P antenna signals received, and .- a combination device with configurable diversity), connected as input to the multi-channel reception and processing device, to combine some or all of the tr signals output units as a function of a selection instruction for processed output signals and processed signals to be combined, and .- a diversity management device and transparent switching of the communication link.
The method for switching the communication link is characterized in that the switching of the communication link is constituted by a succession of a number k, greater than or equal to 2, of transparent and unitary Bi switches of antennas, selected according to a sequence predetermined, each transparent and unitary antenna bi switchover being an antenna switchover from a first diversity configuration in operational reception C1 (i) in which the selected antenna is pointed with follow-up on the first satellite S1, towards a second diversity configuration in operational reception C2 (i) in which the selected antenna is pointed with follow-up on the second satellite S2, at least one of the first and second configurations C1 (i), C2 (i) of diversity in reception being a configuration in which diversity in reception is implemented on the two first and second satellites S1, S 2.
According to particular embodiments, the method for transparent switching of a communication link comprises one or more of the following characteristics:
each transparent and unitary switching Bi comprises steps for controlling the multi-channel reception and processing device as well as the combination device with configurable diversity by determining and sending them respectively:
. * satellite acquisition pointing commands, and. * time and phase alignment commands for the P signals received at the input of the multi-channel reception and processing device developed as a function of time and phase difference measurements of P-1 signals received at input with respect to the signal received at input taken as reference signal, and. * an instruction for selecting the processed output signals to be combined as a function of the planning for switching from the first diversity configuration C1 to the second diversity configuration C2 and as a function of quality measurements of the signals received at the input of the reception and processing device, the control steps being implemented by the diversity management device and transparent switching of the communication link.
The invention will be better understood on reading the description of several embodiments which will follow, given solely by way of example and made with reference to the drawings in which:
FIG. 1 is a view of the progress of a switchover on reception of a communication link from a first satellite S1 to a second satellite S2, implemented by a ground station with two mobile directive antennas according to the invention and according to a first embodiment;
Figure 2 is a view of the progress of a switchover in reception of a communication link from a first satellite S1 to a second satellite S2, implemented by a ground station with three mobile directional antennas according to a second embodiment;
FIG. 3 is a view of a general modular architecture of a multi-antenna ground station concerning the devices of said station and their arrangement which allows the implementation of a transparent switchover when receiving a communication link from a first departure satellite S1 to a second satellite S2 with optimization of the use of diversity in reception, as shown in the examples of Figures 1 and 2;
Figure 4 is a flowchart of a unitary transparent antenna switchover from the first departure satellite S1 to the second satellite S2, the unitary transparent switchover being implemented by the multi-antenna ground station according to the invention of Figure 3, and being a generic step of a succession of unitary transparent switching steps, said succession forming a switching operation on reception of a communication link from the first satellite S1 to the second satellite S2;
FIG. 5 is a partial view of a communications system in which a ground station according to the invention is limited to simplify the illustration with two transmission channels in transmission diversity and with two mobile directional antennas, operating in mode transmission and pointing with tracking to the same satellite, the partial view making it possible to identify the respective contributions made by the equipment of the ground station on each of the channels and by the differentiated geometric paths between the antennas of the ground station and the satellite pointed to the time and phase shifts from channel inputs to satellites;
Figure 6 is a partial view of a modular architecture of a multi-antenna ground station, limited to a multi-channel transmission and processing device with N channels which makes it possible to transmit N carriers at the same frequency by carrying the same communication signal, through N antennas operating in transmission mode and pointed to the same satellite, so as to perform reception by the pointed satellite of the N carriers aggregated in a coherent manner;
FIG. 7 is a view of a system for calibrating the RF transmission chains, connected between the outputs of N transmission channels of the multichannel transmission and processing device and the associated antennas in transmission mode;
FIG. 8 is a view of an example of a closed-loop compensation system for the time and phase shifts applied to the signals of the N transmission channels of the transmission and processing device of the ground station, the compensation system using a reference sequence or message.
Fixed or mobile ground stations on telecommunications satellite systems using a constellation of satellites traveling on HEO (in English High Earth Orbit) or MEO (in English Medium Earth Orbit) or LEO (Low Earth Orbit) type orbits satellite system terminals are used to access one or more of the satellites and exchange telecommunications signals carried by one or more carriers with them.
Ground stations include and must use at least two antennas to allow them to implement switching (in English "handover") of communication links from a first downlink satellite at the end of visibility to a second upward satellite destination. beginning of visibility, as soon as the said ground station antennas are directive.
The underlying concept of the invention is to reinforce the diversity use of antennas in reception mode and / or in transmission mode during a tilting and non-tilting mode and to offer the possibility of adding additional antennas over time. increase the availability and RF radio performance of the ground station and also ensure maintenance of the ground station without compromising the availability of the current service.
The underlying concept of the invention is based on the exploitation of measurements, carried out for example using one or more cross-correlators, of path differences, undergone by the signals received or transmitted by two or more antennas of the station, these measurements allowing the signals received or to be transmitted to be then readjusted in time, in phase and in amplitude and to be later summed in a coherent manner. Thus, an improvement in the signal to noise ratio of 101og (W) dB can be achieved, N being the number of antennas involved in the coherent summation or aggregation operation.
According to Figure 1 and a first embodiment, a multi-antenna ground station 2 of a satellite telecommunications system 12 using a constellation 14 of traveling satellites here comprises two directional and mobile antennas 22, 24, capable of receiving each , during the same predetermined period of time, a satellite taken from a first satellite 32 S1 of origin and a second satellite 34 S2 of destination, both in visibility during said period.
The multi-antenna ground station 2 according to the invention is configured to implement a switching 42 of a communication link from the first departure or origin satellite S1 to the second destination satellite S2.
The switching of the communication link 42 is constituted here by a succession of two switches B1, B2, designated respectively by the references 44, 46, transparent and unitary of the antennas 22, 24, selected according to a predetermined sequence, here B1 then B2.
The first transparent and unitary switchover B1 44 is the switchover of the first antenna 22 from a first diversity configuration in operational reception C1 (1) in which the first antenna 22 selected for the first switchover B1 is pointed with follow-up on the first satellite S1 towards a second diversity configuration in operational reception C2 (1) in which the first antenna 22 selected is pointed with follow-up on the second satellite S2.
The first transparent and unitary tilting B1 is broken down into first, second, third phases, executed successively, designated respectively by "phase # 1", "phase # 2", "phase # 3".
In the first phase "phase # 1", the first and second antennas 22, 24 receive from and transmit to the first satellite S1 according to the first diversity configuration C1 (1).
During the second phase "phase # 2", when the first satellite S1 reaches the end of the race (ie has an elevation relative to the ground station strictly less than 15 ° typically), the first antenna 22 stops transmitting and to receive towards the first satellite S1 to go and join the second satellite S2 in the third phase "phase # 3".
During the third phase "phase # 3" the first antenna 22 receives and transmits to the second satellite S2 while the second antenna 24 receives and transmits to the first satellite S1, according to the second configuration of diversity in reception C2 (1).
The second transparent and unitary B2 switchover is the switchover of the second antenna 24 from a first diversity configuration in operational reception C1 (2), identical to the second diversity configuration in reception C2 (1) of the first unitary switchover B1, in which the second antenna 24 selected for the second unitary tilting B2 is pointed with tracking on the first satellite S1 towards a second configuration of diversity in operational reception C2 (2) in which the first antenna 22 and the second antenna 24 selected are pointed with tracking towards the second satellite S2.
The second switchover 46 B2, transparent and unitary, is broken down into the third phase "phase # 3" and the fourth, fifth phases, designated respectively by "phase # 4", "phase # 5", the third, fourth, fifth phases being executed successively.
During the third phase "phase # 3" the first antenna 22 receives and transmits to the second satellite S2 while the second antenna 24 receives and transmits to the first satellite S1, according to the first configuration of diversity in reception C2 (1) of the second unit failover.
During the fourth phase "phase # 4", the end of travel of the first satellite S1 progressing, the second antenna 24 stops transmitting and receiving towards the first satellite S1 to go and join the first antenna, and receive from and transmit to the second satellite S2 in the fifth phase "phase # 5".
In the fifth phase, the first and second antennas 22, 24 receive from and transmit to the second satellite S2 according to the second diversity configuration in reception C2 (2) of the second unit tilting.
This process is repeated with each new link switch from a first satellite to a second satellite.
According to FIG. 2 and a second embodiment, a multi-antenna ground station 50 of a satellite telecommunications system 52 using a constellation 54 of traveling satellites here comprises three directive and mobile antennas 62, 64, 66, capable of receiving each follow, during the same predetermined period of time, a satellite taken from a first satellite 72 S1 of departure and a second satellite 74 S2 of destination, both in visibility during said period.
The multi-antenna ground station 50 according to the invention is configured to implement a switching 82 of a communication link from the first departure satellite 72 S1 to the second destination satellite 74 S2.
The switching of the communication link 82 is constituted here by a succession of three switches 84 B1, 86 B2, 88 B3 transparent and unitary of the antennas 62, 64, 66 selected in turn, according to a predetermined sequence, here B1 then B2 then B3 .
The first transparent and unitary switchover 84 B1 is the switchover of the first antenna 62 from a first diversity configuration in operational reception C1 (1) in which the first antenna 62 selected for the first switchover B1 is pointed with follow-up on the first satellite S1 towards a second diversity configuration in operational reception C2 (1) in which the first antenna 62 selected is pointed with follow-up on the second satellite S2.
The first transparent and unitary tilting B1 is broken down into first, second, third phases, executed successively, designated respectively by "phase # 1", "phase # 2", "phase # 3".
In the first phase "phase # 1", the first, second and third antennas 62, 64, 64 receive from and transmit to the first satellite S1 according to the first diversity configuration C1 (1).
During the second phase "phase # 2", when the first satellite S1 begins to arrive at the end of the race (ie has an elevation relative to the ground station strictly less than 15 ° typically), the first antenna 62 ceases to send and receive to the first satellite to join the second satellite S2 in the third phase "phase # 3".
During the third phase "phase # 3" the first antenna 62 receives and transmits to the second satellite S2 while the second and third antennas 64, 66 receive and transmit to the first satellite S1, according to the second configuration of diversity in reception C2 ( 1) of the first unitary transparent tilting B1.
The second transparent and unitary switchover B2 B2 is the switchover of the second antenna 64 from a first diversity configuration in operational reception C1 (2), identical to the second diversity configuration in reception C2 (1) of the first unitary switchover B1, in which the second antenna 64 selected for the second unitary tilting B2 is pointed with follow-up on the first satellite S1 towards a second configuration of diversity in operational reception C2 (2) with three antennas in which the first antenna 62 and the second antenna 64 selected are pointed with tracking to the second satellite while the third antenna 66 remains pointed with tracking to the first satellite S1.
The second transparent and unitary switchover B2 B2 is broken down into the third phase “phase # 3” and the fourth and fifth phases, designated respectively by “phase # 4”, “phase # 5”, the third, fourth and fifth phases being executed. successively.
During the third phase "phase # 3" the first antenna 62 receives and transmits to the second satellite S2 while the second and third antennas 64, 66 receive from and transmit to the first satellite S1, according to the first diversity configuration in reception C2 (1) of the second unitary tilting B2.
During the fourth phase "phase # 4", the end of travel of the first satellite S1 progressing, the second antenna 64 stops transmitting and receiving towards the first satellite S1 to go and join the first antenna 62, and receive from and transmit to the second satellite S2 in the fifth phase "phase # 5".
In the fifth phase and according to the second diversity configuration in reception C2 (2) with three antennas of the second unitary tilting B2, the first and second antennas 62, 64 receive from and transmit to the second satellite S2 while the third antenna 66 receives from and transmits to the second satellite S2.
The third transparent and unitary switching 88 B3 is the switching of the third antenna 66 from a first diversity configuration in operational reception C1 (3), identical to the second diversity configuration in reception C2 (2) of the second unitary switching B2, in which the third antenna 66 selected for the third unitary tilting B3 is pointed with follow-up on the first satellite S1 towards a second configuration of diversity in operational reception C2 (3) with three antennas in which the first, second and third antennas 62, 64, 66 are pointed with tracking towards the second satellite S2.
The third transparent and unitary tilting 88 B3 is broken down into the fifth phase “phase # 5” and the sixth and seventh phases, designated respectively by “phase # 6”, “phase # 7”, the fifth, sixth and seventh phases being executed. successively.
During the fifth phase "phase # 5" and following the first configuration of diversity in reception C1 (3) of the third unit tilting B3, the first and second antennas 62, 64 receive from and transmit to the second satellite S2 while the third antenna 66 receives from and transmits to the first satellite S1.
During the sixth phase “phase # 6”, the end of travel of the first satellite S1 still progressing, the third antenna 66 stops transmitting and receiving towards the first satellite S1 in order to join the first and second antennas 62, 64 and receive from and transmit to the second satellite S2 in the seventh phase "phase # 7".
In the seventh phase and following the second configuration of diversity in reception C2 (3) with three antennas of the third unitary tilting B3, the first, second and third antennas 62, 64, 66 receive from and transmit to the second satellite S2.
The advantage of using a ground station here having three directional mobile antennas according to the invention and the switching of link 82 of FIG. 3 is to permanently guarantee diversity with two antennas, including in the case where the two satellites S1 , S2 send the same carrier. It is always possible to combine at least two antennas from the ground station at all times.
In general, a multi-antenna ground station of a satellite telecommunications system using a constellation of traveling satellites comprises an integer P, greater than or equal to two, of antennas capable of receiving each to follow, during the same period of predetermined time, a satellite chosen from a first satellite S1 of origin and a second satellite S2 of destination, both in visibility during said period.
The multi-antenna ground station according to the invention is configured to implement a switching of a communication link from the first original satellite S1 to the second destination satellite S2. The switching of the communication link is constituted by a succession of a number P, greater than or equal to 2, of switching Bi (i being between 1 and P) transparent and unitary antennas, selected according to a predetermined sequence. Each transparent and unitary Bi tilting of the antenna is the tilting of an antenna from a first configuration of diversity in operational reception C1 (i) in which the selected antenna is pointed with tracking on the first satellite S1, towards a second configuration of diversity in operational reception C2 (i) in which the selected antenna is pointed with follow-up on the second satellite S2, at least one of the first and second configurations C1 (i), C2 (i) of diversity in reception being a configuration in which the diversity in reception is implemented on the two first and second satellites S1, S2.
More particularly, the whole number P of reception antennas, capable of pointing and each tracking, for the same predetermined period of time, a satellite taken from a first satellite S1 and a second satellite S2, and channels of the device reception and processing is greater than or equal to three. The first and second configurations C1 (i), C2 (i), of diversity in reception of each unitary transparent switchover Bi are each of the configurations in which diversity in reception is implemented on the two first and second satellites S1, S2.
During each unitary transparent switchover Bi and during the switchover of the communication link, diversity in reception on at least two antennas is permanently ensured.
According to FIG. 3 and a preferred embodiment of the invention, a multi-antenna ground station 102 comprises an integer P, greater than or equal to two, of directive mobile antennas 112 (antenna # 1), 114 (antenna # 2) , 116 (antenna #P), a multi-channel reception and processing device 122, a configurable diversity combination device 124 and a diversity management device 126 and transparent switching of a reception communication link from a first satellite S1 of departure towards a second satellite S2 of destination.
The P directional mobile antennas 112, 114, 116 are capable of reception, each of them tracking, during the same predetermined period of time, a satellite taken from a first departure satellite S1 and a second destination satellite S2, both in visibility during said period.
The multi-channel reception and processing device 122 comprises P input terminals 132, 134, 136, respectively connected to P output terminals of the P antennas 112, 114, 116, for receiving at the input of said device and processing P received antenna signals se1 (t), se2 (t), ..., seP (t) and supplied at the output of said reception antennas 112, 114, 116. The multi-channel reception and processing device 122 comprises P output terminals 142, 144, 146 for delivering in parallel P processed output signals st1 (t), st2 (t), ..., stP (t), aligned with each other in time and in phase, obtained respectively from the P antenna signals received se1 (t) , se2 (t) .....
seven).
The multi-channel reception and processing device 122 is configured to:
.- receive, normalize and filter on P distinct and separate channels, numbered by an integer index j varying from 1 to P, the P antenna signals received salt (t), se2 (t) ..... seP (t), supplied by P antennas 112, 114,
116, in P normalized and filtered signals, then .- estimate time differences, phase differences and quality differences between a normalized and filtered reference signal, taken from among the P normalized and filtered signals, and the P-1 signals normalized and filtered remaining, and providing said deviations to the management and switching device; then .- for each channel, apply time compensation and phase compensation to the normalized and filtered signal associated with the channel, from the corresponding time and phase alignment commands, developed and sent by the diversity management device and tipping.
The multi-channel reception and processing device 122 here comprises for example:
.- a battery of P automatic gain control devices AGC 152, 154, 156, for normalizing the signals received at the input of the multi-channel reception and processing device, and .- a battery of P bandpass filters 162, 164, 166 , to filter the normalized signals, here SRRC filters (in English Square Root Raised Cosine).
The multichannel reception and processing device 122 here also includes a battery of complex P-1 cross-correlators 172, 174 for estimating time differences, phase differences and quality differences between a normalized and filtered reference signal, taken among the P normalized and filtered signals, and the P-1 normalized and filtered signals remaining.
The battery of the complex P-1 cross-correlators 172, 174 is configured to supply said deviations to the management and switching device, by seeking for each cross-correlator a correlation peak which makes it possible to deduce the time difference between the compared signals , by exploiting the argument of the cross-correlated signal to determine the phase difference between the compared signals, and by exploiting the level of correlation between the compared signals to determine an indication of difference in quality.
The multi-channel reception and processing device 122 also includes a battery of P of delay lines 182, 184, 186 of the FIFOs type (in English First in First Out) with programmable time offset, connected downstream to a battery of P multipliers 192 , 194, 196 with programmable phase compensation, the multipliers 192, 194, 196 allowing the phase compensations being connected as an input to the diversity combining device 124.
The multi-channel reception and processing device 122 is configured to selectively adjust the gain of each of the channels so as to be able to selectively progressively attenuate the signal output level of the output chain which it is desired to remove from the combination to diversity.
The combination device 124 with configurable diversity is connected as an input to the multi-channel reception and processing device 122, to combine part or all of the output processed signals according to a selection instruction of the output processed and processed signals. combine, provided by the diversity management and switching device 126.
The transparent diversity and switching management device 126 is configured to manage and coordinate the execution of a switching of the communication link from a first original satellite S1 to a second destination satellite S2. The switching of the communication link consists of a succession of a number K, greater than or equal to 2, of transparent and unitary Bi switching of antennas, selected according to a predetermined sequence. Each transparent and unitary Bi switchover of antenna is a switchover of a predetermined antenna from a first configuration of diversity in operational reception C1 (i) in which the selected antenna is pointed with follow-up on the first satellite S1, towards a second configuration diversity in operational reception C2 (i) in which the selected antenna is pointed with follow-up on the second satellite S2, at least one of the first and second configurations C1 (i), C2 (i) of diversity in reception being a configuration in which diversity in reception is implemented on the two first and second satellites S1, S2.
The diversity management and transparent switching device 126 is also configured to, during each transparent and unitary switching Bi, control the antennas 112, 114, 116, the multi-channel reception and processing device 122 as well as the diversity combination device configurable 124 by determining and sending them respectively:
.- satellite acquisition pointing commands, and .- time and phase alignment commands for the P signals received at the input of the multi-channel reception and processing device developed as a function of time and phase difference measurements of P-1 signals received at input with respect to the signal received at input taken as reference signal, and an instruction for selecting the processed output signals to be combined as a function of the planning of the unitary transparent switches Bi (i varying from 1 to K ) constituting the switching from the first diversity configuration C1 (1) to the second diversity configuration C2 (K) and as a function of quality measurements of the signals received at the input of the reception and processing device.
The transparent diversity management and switching device 126 is configured on detection of an absence of signal on an active chain in the combination to send a withdrawal command to the diversity combination device.
The diversity management and transparent switching device 126 is configured during an antenna switching from the first satellite to the second satellite to control a decreasing gain ramp on the chain to be removed by the diversity combination device, and when the differential quality has dropped below a predetermined threshold commanding the diversity combination device to remove said chain.
The multi-antenna ground station 102 according to the invention may include a single demodulator, not shown in FIG. 3, connected at the output of the diversity combination device 124.
The multi-antenna ground station 102 according to the invention can optionally include a device for implementing an adaptive modulation control loop ACM (in English Adaptive Control Modulation).
When the multi-antenna ground station 102 according to the invention comprises a device for implementing an adaptive modulation control loop ACM, the dynamics of the decreasing gain ramp is coordinated with the dynamic characteristics of the control loop of ACM adaptive modulation.
When the ground station according to the invention 102 is in operation, the input signals se1 (t), se2 (t), ..., seP (t), received from the antennas 112, 114, 116 through possible RF reception Rx chains which can amplify and / or transpose in frequency er / or digitize, are first standardized thanks to an AGC on each channel, then filtered by filters 162, 164, 166 to isolate the signal of interest to be summed on each channel.
The normalized signals sn1 (t), sn2 (t) ..... snP (t) then feed the battery of the complex P-1 cross-correlators which makes it possible both by seeking the correlation peaks to deduce the time difference between signals, and through the argument of cross-correlation signals to measure the phase difference between the signals.
The signal se1 (t) supplied at input 132 of the first channel (channel # 1) is taken here as the reference signal.
In order to limit the operating frequency of each cross-correlator 172, 174, each input signal of said cross-correlators can be optionally passed through a fractional clock recovery loop 202, 204, 206 for fractional delays less than the duration of a digital sample based on an NDA rhythm recovery algorithm (in English Non Data-Aided) not assisted by the data, for example of the Gardner type.
These time and phase difference measurements will control the FIFO delay lines 182, 184, 186 with configurable time offset and the multipliers 192, 194, 196 in order to apply the necessary compensations to the signals before finally summing them.
The reception quality indication allows the diversity and switching management device 126 when it detects a difference in said quality between the two signals to reduce the contribution of the noisiest signal for link budget quality problems.
What is wanted is not an absolute indication of the signal quality but rather an indication of the difference in quality. From this point of view the level of correlation between the signals constitutes a perfect estimator all the more since it requires no a priori knowledge of the signal.
During a link switching or handover decision between a first satellite S1 and a second satellite S2 which can intervene and come either from an organ of the satellite system, different from the ground station, or either from the ground station itself , based for example on exceeding a minimum elevation threshold, the addition of an antenna by the combining device 124 with configurable diversity is not abruptly interrupted but a ramp of progressive gain reduction over the amplitude of the signal from the antenna to be removed is applied in order to limit the disturbance of a possible ACM loop used in the transmission This ramp is typically of the order of a few tenths of dB per RTT round trip period (in English Round Time Trip). For example on an MEO satellite and a typical RTT of 60ms, this process takes less than a second.
Symmetrically when adding a new signal and therefore a new receiving antenna, this signal addition must be done gradually in order to avoid a significant level difference at the input of the gain control device AGC of the corresponding channel of the reception and processing device 122 which by saturating the AGC device of the demodulator disposed downstream of the combination device 124 could produce a momentary loss of signal inducing a loss of traffic.
According to FIG. 4, a typical process 252 for managing a unitary transparent switchover of an antenna from a first a first departure satellite S1 to a second destination satellite S2 is illustrated.
When an absence of reception signal on an antenna is detected in a first step 254 due to the fact that the correlation no longer operates with a satisfactory level, the associated associated channel is immediately withdrawn in a second step 256 of the addition performed by the combination device 124 in order to prevent said noisy channel from bringing additional noise.
Following a request for a unitary transparent switchover of an antenna in reception mode from a first satellite S1 to a second satellite S2, the execution of this switchover is activated in a third step 258, and in a fourth step 260 a ramp decreasing gain is applied to the chain to be removed. In a fifth step 262, the differential quality associated with said chain to be removed is compared with a predetermined threshold value, here assumed to be 5 dB and which in practice is materialized by a minimum threshold of the correlation level,
As long as the difference in quality does not exceed the threshold value, the linear decrease in gain by gain step continues to be applied the repetition of the fourth and fifth steps 260, 262.
When the difference in quality exceeds 5 dB, the chain to be removed is completely removed from the final summation in the second step 256.
The antenna associated with the removed channel can then be freely repositioned to acquire a new satellite by performing an antenna pointing in a sixth step 264 and a re-acquisition loop of the carrier 266 (seventh step 268 and eighth step 270). When the acquisition of the carrier, materialized by a sufficient level of correlation, is reached, according to a ninth step 272 the channel connected to the antenna and to its RF reception chain is again included in the process of final summing of the device of combination to diversity.
According to Figure 5, a ground station 302 according to the invention, derived from the ground station 102 described in Figure 3, further comprises at least two transmission channels 304, 306, able to be combined and at least two directional antennas mobiles 314, 316, able to operate in transmission mode and to point with tracking to the same satellite 320.
Figure 5 illustrates the respective contributions 322, 324, made by the transmission equipment 328 of the ground station 302 on each of the channels 304, 306, and by the differentiated geometric paths between the antennas 314, 316, operating in transmission from the ground station 302 and the common satellite 320 pointed at the time offsets and in phase from the inputs of the channels 304, 306, to the common satellite 320 pointed.
In general, for both reception and transmission channels, in their RF and digital components, contributions should be separated into two parts:
.- a first part concerning the internal contribution to the terminal coming from the random start-up phase of the local oscillators OLs as well as delays induced in particular by the length of the cables, .- a second part concerning the contribution coming from the distance between the antennas and the satellite.
According to FIG. 6 and a general modular architecture of the multi-antenna ground station 302, the more specific devices of the transmission mode of the station and their arrangement are illustrated.
These devices are configured to allow the ground station to transmit N carriers at the same frequency carrying the same communication signal, through N antennas operating in transmission mode and pointed to the same satellite, and reception by the satellite of N carriers aggregated consistently.
According to FIG. 6, the multi-antenna ground station 302 comprises a device 354 for supplying the same source signal, a transmission and processing device 356 for generating on N channels a wavefront intended for the same satellite 320, and a device for managing diversity in transmission 358.
The device 354 for supplying the same source signal to be transmitted is configured to supply the source signal shared in an integer N, less than or equal to P, of supply terminals 362-I, 362 ₂ , ..., 362n.
The transmission and processing device 356, configured to generate on N transmission channels a wavefront intended for the satellite 320, pointed and in reception mode, taken from the first satellite S1 and the second satellite S2, is connected at the input to the N supply terminals 362-i, 362 ₂ , ..., 362n of the supply device 354.
The transmission and processing device 356 comprises N transmission output terminals 372i, 372 ₂ , ..., 372 _N connected to N antennas among the P transmission antennas, for delivering N processed output signals in parallel, temporally and phase-shifted between them so that the wave fronts of each antenna are aggregated when receiving the common satellite 320.
The transmission diversity management device 358 is configured to control the multichannel transmission and processing device 356, by determining and sending to it time and phase shift commands of the N signals transmitted at the output of the transmission device and multi-channel processing.
The time and phase shift commands for the N signals transmitted at the output of the multi-channel transmission and processing device are developed as a function of calibration measurements of the transmission chains, estimates of the contributions internal to the terminal on reception and the contributions related to the difference in distance between the transmission channels.
Thus, N differentiated emission channels are created from the same signal, by inserting a different delay at each output as well as a correction in phase and in amplitude, which makes it possible to generate a wave front intended for the common satellite, addressee in transmission mode, the wave front being composed of the wave fronts of each antenna which have aggregated constructively at the antenna reception point of the common satellite.
According to FIG. 7, the multi-antenna ground station 302 of FIGS. 5 and 6 comprises a retroactive calibration chain 392 of the RF transmission Tx chains 394i, 394 ₂ , ..., 394 _N
The retroactive calibration chain 392 of the transmission RF chains is connected to the input ports 396i, 396 ₂ ..... 396n of the N antennas in transmission mode through N sampling couplers 398i, 398 ₂ ..... 398 _N , connection cables 402i, 402 ₂ , ... 402 _N and a switch N: 1 404 for selecting the RF transmission channel.
The sampling couplers 398-I, 398 ₂ , ..., 398 _N , the connection cables 402 _1t 402 ₂ , ... 402n and the switch N: 1 404 are calibrated to allow an estimator 408 of the internal contributions of RF transmission chains determine the internal contributions of the transmission chains of the ground station in terms of time and phase differential deviations. These estimates are made from the calibration measurements of the emission RF chains retrieved by the retroactive calibration chain 392.
The retroactive calibration chain 392 thus makes it possible to measure the phase difference and the differential delay between two RF transmission chains selected as desired through a sequence of suitable commands sent by the estimator 408 to the switch 404.
The internal contributions to the ground station 302 in transmission in terms of phase and time differences, designated respectively by Δφ _{τχ ter} and At _{TX ter} , are thus estimated using the retroactive calibration chain 392. These two values are deduced by sending a reference signal on each RF transmission channel 394i, 394 ₂ , ..., 394 _N and an estimate of the phase shift and delay, the estimate using for example the same type of estimation device than the preferred one based on a correlator for the antenna reception mode.
Thus the phase differences of the local oscillators OLs of the RF transmission chains can be taken into account to determine the setpoint deviations of the transmission channels with a view to obtaining a coherent aggregation at the level of the satellite receiving the transmitted wave fronts. by the antennas in transmission mode.
It should be noted that this retroactive calibration chain 392 can be advantageously reused for an adaptive predistortion function of the BUC (Block Up-Converter) units for amplification and frequency conversion of the RF transmission chains in the measurement. where this chain 392 makes it possible to sample the signal at the output of the amplification chain.
As regards the estimation of the contribution coming from the differences in the distances between the antennas and the pointed common receiver satellite, the antennas 314, 316, operating in transmission mode to said common satellite are assumed to also operate in reception mode with respect to from the same common satellite.
For this estimation of the second part of the contributions, the phase measurements of the reception chains Rx cannot be taken back as they are. Indeed, any two RF reception chains, taken from all the Rx reception RF chains, being independent, even if these two Rx RF chains have the same clock reference, the absolute phase cannot be controlled. It is therefore necessary to start from the path difference given by the time offset of the signals received by the antennas. The phase part is, for its part, both affected by the relative phase difference between the local oscillators OLs of the two RF chains and by the difference in wavefront paths, i.e. the difference of the two corresponding received paths.
The internal contributions of the receiving ground station and in terms of phase and time differences being respectively designated by _ter and _ter and the contributions linked to the differences in distances between the two antennas and the satellite on the downlink being respectively designated by & (p _sat _ _ter and At _sat _ _ler , a first relation
Δψκχ ^ τ ⁼ AÏrx_ _t er ^{C +} ^ PrX LOs is satisfied in which _LOs denotes the difference in initial phases between the local oscillators OLs of the two reception chains and ç denotes the speed of light in a vacuum.
To estimate the time difference _ter , one method is for example to use low noise amplification units LNBs (in English Low Noise Blocks) as close as possible or calibrated as well as calibrated cable lengths.
It should be noted that in the case where the reception acquisition chain is integrated into the low noise amplification unit LNB and the signal comes out digitized, there is no longer any contribution from the cable.
The time difference measurements taken at reception being designated by _mes and the contributions linked to the difference in distance between the antennas and the satellite on the return path from the antennas in terms of phase and time differences being respectively designated by APtersat ^e t ^ ^es Tersat the estimated phase and time for compensation for the path from the satellite antenna to the transmission can then be estimated according to the expression:
ΔΛ, - At „ _v . —Èt _ov and Δ <ζ> ₍ , = ΔΛ, .c ter-sat RX ter RX mes τ ter-sat ter-sat
In this approach, we use the measurement in time of the time difference to predict that of the program. If one seeks to improve the quality of these predictions an autoregressive type approach can be used, this approach being based for example on a sliding GARCH (in English Generalized AutoRegressive Conditional Heteroskedasticity) algorithm, or on a Kalman filtering or on ephemeris.
The compensation on issue in a simplified way is then calculated as follows. Δ / ^ ^^ = - et _{RX ter} ~ et _tersat and Δφ _{τχ comp} = ~ 1 ^χ φ _{κχ ter} —Δφ _ια , _χαι
According to FIG. 8, the multichannel transmission and processing device 356, and the transmission diversity management device 358 are arranged and configured to implement closed-loop compensation 452 for the time and phase differences of the N channels d transmission of a broadcast diversity configuration. Here, in Figure 8 for the sake of simplification of the illustration, a diagram limited to two transmission channels and two antennas 314, 316 is provided. This scheme can easily be extended to a number N of antennas and emission channels greater than or equal to 3.
The N antennas used in transmission diversity on the pointed satellite
320, here the two antennas 314, 316, are at the same time reception diversity antennas pointing to the same satellite 320, and send N identical signals, here two signals in FIG. 8, time-shifted and in phase to generate a coherent wavefront at the pointed satellite.
The transmission diversity management device 358 receives a measurement of the quality of the aggregation of the carriers transmitted by the N antennas in transmission mode 314, 316.
This measurement of the quality of the aggregation of the carriers was carried out and determined beforehand in terms of time and phase differences by a receiver 462 from a remote external ground station 464 and retransmitted to the transmitting ground station 302 via a channel. terrestrial return channel 466. The transmitting ground station 302 corrects, via the transmission diversity management device 358, the time and phase offset instructions, supplied to the multichannel transmission and processing device 356, on the basis of time and phase differences measured by the external ground station 464.
Alternatively, the satellite system is bidirectional and includes a return link by the same pointed satellite. In this case, a measure of the quality of the carrier aggregation, determined beforehand in terms of time and phase differences by the receiver of the remote external ground station, is retransmitted via the symmetrical return channel of the pointed satellite.
This closed-loop compensation configuration makes it possible to test the quality of the compensation and possibly correct it by applying one or more corrections to it in order to constantly guarantee a required level of quality.
According to FIG. 8 and a first embodiment, the N identical signals, here the two signals 454, 456, shifted between them in time and in phase to generate a coherent wavefront at the level of the pointed satellite, are signals of an identical reference sequence but at different frequencies, and the differential signals from the receiver 462 of the external ground station 464 are determined by correlation.
The external receiver 462 of the external ground station 464 here receives the two signals at different carrier frequencies. By correlating these two signals, the external receiver 464 is able to determine a difference in terms of arrival time and phase difference, and then supply it to the ground station 302 in transmission mode via the channel. feedback 466 of the compensation loop 452.
The transmission diversity management device 358 of the ground station according to the invention is configured to compare this result with the offset setpoints used to deduce from the comparison a correction to be made to the future offset setpoints.
As a variant and according to a second embodiment, the N identical signals, shifted between them in time and in phase to generate a coherent wavefront at the level of the pointed satellite, are signals obtained from replicas of the same signal. traffic, and the differential signals from the receiver of the external ground station are determined by correlation of the received signal retransmitted by the satellite.
This second method fulfills the same objective as the first method of FIG. 8, without requiring a disengagement of the aggregation of the carriers transmitted in traffic mode in order to carry out the measurement or measurements required by the compensation loop.
If the autocorrelation measurement of the received signal is carried out, which is the result of the aggregate of the signals coming from the different antennas, the lack of compensation in time and in phase causes a reduction in the correlation peak and the appearance of secondary peaks.
This peak deviation corresponds to twice the delay between the signals and the phase of the autocorrelation signal indicates the phase difference between the compared signals.
The dynamic calibration system and method are intended to be activated and to operate either permanently, repeatedly periodically or a-periodically, or on request by sending remote controls from the ground for example.
Advantageously, the multi-antenna ground station according to the invention makes it possible to coherently add several aftershocks received from the same signal, a reshuffling of the aftershocks being made from the exploitation of time difference measurements. and in phase between tracks. The measurements of the time and phase differences between channels are preferably carried out by cross-correlators. The coherent aggregation of two carriers makes it possible to reach up to 3 dB on the signal to noise ratio and in general the coherent aggregation of N carriers received makes it possible to reach 10.log (N) dB of improvement in the ratio signal to noise.
Advantageously, the architecture and the configuration of the ground station according to the invention allow a harmonious integrated management of an inter-satellite link failover and of an ACM control mechanism by a gradual interruption of a carrier associated with an antenna when it is removed from a satellite during the switchover and by the ability to align carriers from the same satellite and / or from two different satellites.
Advantageously, the multi-antenna ground station according to the invention allows the coherence of a wave front on transmission for reception by the same satellite of several replicas of the same satellite. The coherent aggregation of two transmitted carriers makes it possible to achieve up to 6 dB of gain in radiated power emitted at the location of the satellite and in general the coherent aggregation of N transmitted carriers makes it possible to reach 20.log (N ) dB of radiated power gain emitted at the satellite location.
The invention allows the coherent addition of several replicas of the same signal whether or not it comes from the same satellite, whether or not at the same frequency / polarization thanks to the phase / frequency and time realignment of the different replicas. based on a band of crosscorrelators.
The path difference measurement at reception, associated with knowledge of the ephemeris of satellites is used to generate a prediction of the phase shift and time to be applied to the transmission in order to emit a coherent wavefront between the antennas .
The invention also allows hand-over management thanks to the signal quality measurements provided by the cross-correlators and to the ephemeris information. The use of a link severing procedure before the implementation of the hand-over allows for adaptive loops (ACM) to be used both on transmission and on reception.

权利要求:
Claims (16)
[1" id="c-fr-0001]
1. Multi-antenna ground station of a satellite telecommunications system (14) using a constellation of traveling satellites (32, 34; 72, 74), the ground station comprising:
.- an integer P, greater than or equal to two, of antennas (22, 24; 62, 64, 66; 112, 114, 116) capable of reception, each of them tracking, during the same predetermined period of time, a satellite (32 , 34; 72, 74) taken from a first satellite (32; 72) S1 of origin and a second satellite (34; 74) S2 of destination, both in visibility during said period, .- a device for receiving and multi-channel processing (122), with P input terminals (132, 134, 136), connected respectively to P output terminals of the P antennas (112, 114, 116), for receiving at input of said device and processing P antenna signals received and supplied at the output of said reception antennas, and at P output terminals (142, 144, 146) for delivering in parallel P processed output signals, aligned with each other in time and in phase, obtained respectively from the PP antenna signals received , and .- a configurable diversity combination device (124 ), connected as an input to the multi-channel reception and processing device (122), for combining part or all of the output processed signals according to a selection instruction of the output processed and processed signals to be combined, and. a device for managing diversity and transparent switching (126) of a reception communication link from the first satellite S1 of origin to the second satellite S2 of destination, the ground station being characterized in that the device for managing diversity and transparent failover (126) is configured to:
manage and coordinate the execution of a switching of the communication link from the first satellite (32; 72) S1 of origin to the second satellite (34; 74) S2 of destination, said switching of the communication link being constituted by a succession of a number k, greater than or equal to 2, of transparent and unitary Bi tilting of antennas, selected according to a predetermined sequence, each transparent and unitary Bi tilting of antenna (44, 46; 84, 86, 88) being a tilting of an antenna (22, 24; 62, 64, 66) from a first configuration of diversity in operational reception C1 (i) in which the selected antenna is pointed with follow-up on the first satellite S1, towards a second configuration diversity in operational reception C2 (i) in which the selected antenna is pointed with follow-up on the second satellite S2, at least one of the first and second configurations C1 (i), C2 (i) of diversity in reception being a configuration in which diversity in reception is implemented on the two first and second satellites S1, S2, and during each transparent and unitary switching Bi (32, 34; 84, 86, 88), check the antennas (22, 24; 62, 64, 66), the multi-channel reception and processing device as well as the combination device with configurable diversity by determining and sending them respectively:
. * satellite acquisition pointing commands, and. * time and phase alignment commands for the P signals received at the input of the multi-channel reception and processing device developed as a function of time and phase difference measurements of P-1 signals received at input with respect to the signal received at input taken as reference signal, and. * an instruction for selecting the processed output signals to be combined as a function of the planning of the switching of the first diversity configuration C1 ( i) towards the second diversity configuration C2 (i) and as a function of quality measurements of the signals received at the input of the reception and processing device.
[2" id="c-fr-0002]
2. Multi-antenna ground station according to claim 1, in which the integer number P of receiving antennas (22, 24; 62, 64, 66; 112, 114, 116), capable of pointing and tracking each, for the same predetermined period of time, a satellite selected from a first satellite S1 (32; 72) and a second satellite S2 (34: 74), and of channels of the reception and processing device (122) is greater than or equal to three , and preferably equal to three, and the first and second configurations C1 (i), C2 (i) of diversity in reception of each unitary transparent switching Bi are each of the configurations in which diversity in reception is implemented on both first and second satellites S1, S2 (32, 34; 72, 74), and .- during each unitary transparent switchover Bi and during the switchover of the communication link, a diversity in reception on at least two antennas (22, 24; 62 , 64, 66; 112, 114, 116) is permanently insured in this.
[3" id="c-fr-0003]
3. Multi-antenna ground station according to any one of claims 1 to 2, in which .- the multi-channel reception and processing device (122) is configured for:
. * receive, normalize and filter on P distinct and separate channels, the P received antenna signals output by the P antennas (112, 114, 116), in P normalized and filtered signals, then. * estimate time differences, phase deviations and quality deviations between a normalized and filtered reference signal, taken from among the P normalized and filtered signals, and the remaining P-1 normalized and filtered signals, and supplying said deviations to the management and switching device; then. * for each channel, apply time compensation and phase compensation to the filtered signal associated with the channel from the corresponding time and phase alignment commands, developed and sent by the diversity and tilt management device.
[4" id="c-fr-0004]
4. Multi-antenna ground station according to any one of claims 1 to 3, in which the multi-channel reception and processing device (122) further comprises:
.- a battery of P automatic gain control devices AGC (152, 154, 146) for normalizing the signals received at the input of the multi-channel reception and processing device (122), and a battery of P band-pass filters (162, 164, 166) to filter normalized signals, for example SRRC filters.
[5" id="c-fr-0005]
5. Multi-antenna ground station according to any one of claims 1 to 4, in which the multi-channel reception and processing device (122) further comprises:
a battery of complex P-1 cross-correlators (172, 174) for estimating time differences, phase differences and quality differences between a normalized and filtered reference signal, taken from among the P normalized and filtered signals, and the P-1 normalized and filtered signals remaining, and supplying said deviations to the management and switching device, by seeking for each cross-correlator (172, 174) a correlation peak which makes it possible to deduce the temporal deviation between the compared signals, by exploiting the cross-correlated signal argument to determine the phase difference between the compared signals, and by exploiting the level of correlation between the compared signals to determine an indication of difference in quality.
[6" id="c-fr-0006]
6. Multi-antenna ground station according to any one of claims 1 to 5, in which the multi-channel reception and processing device (122) further comprises:
a battery of P of FIFOs delay lines (182, 184, 186) with programmable time offset, connected downstream to a battery of multipliers (192, 194, 196) with programmable phase compensation, the multipliers (192, 194, 196 ) allowing the phase compensations being connected at the input to the diversity combination device (124).
[7" id="c-fr-0007]
7. Multi-antenna ground station according to any one of claims 1 to 6, in which the multi-channel reception and processing device (122) is configured to selectively adjust the gain of each of the channels so as to be able to gradually attenuate the output level of the output signal of a search for an output chain which it is desired to remove from the diversity combination, and the diversity management and switching device (126) is configured during a switching antenna from the first satellite (32; 72) to the second satellite (34; 74); for :
controlling a declining gain ramp on the chain to be removed by the diversity combination device, and when the differential quality has exceeded a predetermined threshold commanding the diversity combination device (124) to remove said chain.
[8" id="c-fr-0008]
8. Multi-antenna ground station according to claim 7, comprising a demodulator connected at the output of the diversity combination device and a device for implementing an adaptive modulation control loop ACM, and in which the dynamics of the ramp decreasing gain is coordinated with the dynamic characteristics of the ACM adaptive modulation control loop.
[9" id="c-fr-0009]
9. Multi-antenna ground station according to any one of claims 1 to 8, in which the multi-channel reception and processing device (122) is configured to selectively adjust the gain of each of the channels so as to be able to increase gradually. the output level of the output signal of an output chain which it is desired to add in the diversity combination, and the diversity management and switching device (126) is configured for, during a unitary switching d 'antenna of the first satellite (32; 72) to the second satellite (34; 74) and of the phase of attachment of the antenna to the destination satellite, control a progressive gain ramp on the channel to be added by the combination device to diversity.
[10" id="c-fr-0010]
10. Multi-antenna ground station according to any one of claims 1 to 9, in which the diversity management and tilting device (126) is configured on detection of an absence of signal on an active channel in the combination for send a withdrawal command to the diversity combination device (124).
[11" id="c-fr-0011]
11. Multi-antenna ground station according to any one of claims 1 to 10, comprising a supply device (354) of the same source signal to be transmitted in an integer N, less than or equal to P, of supply terminals (362-I, 3622, 362 _N ), and .- a transmission and processing device (356) for generating on N channels a wavefront intended for a satellite, taken from the first satellite S1 (32 ; 72) and the second satellite S2 (34; 74), connected as an input to the N supply terminals, and having N transmission output terminals connected to N antennas among the P transmitting antennas or equal to P, for delivering in parallel N processed output signals, shifted between them in time and in phase so that the wave fronts of each antenna are aggregated in satellite reception, and .- a transmission diversity management device (358) configured to control the multichannel transmission and processing device (356) by determining and by sending it time-shift and phase-shift commands for the N signals transmitted at the output of the multi-channel transmission and processing device (356) developed as a function of measurements of calibration of the transmission chains, estimates of the contributions internal to the terminal in reception and contributions related to the difference in distance between the transmission channels.
[12" id="c-fr-0012]
12. Multi-antenna ground station according to claim 11, comprising a retroactive calibration chain (392) of the transmission chains (394-1, 394 ₂ , 394 _N ) connected to the input ports (396i, 396 ₂ , 396 _N ) N antennas in transmission mode through sampling couplers (398i, 398 ₂ , 398n), connection cables (402i, 402 ₂ , 402 _N ) and an N: 1 channel selection switch (404), calibrated for the internal contributions of the station's transmission channels in terms of differential time and phase differences.
[13" id="c-fr-0013]
13. Multi-antenna ground station according to any one of claims 11 to 12, in which the multichannel transmission and processing device (356), and the transmission diversity management device (358) are arranged and configured for implement closed-loop compensation (452) of the time and phase differences of the N transmission channels of a transmission diversity configuration in which the N antennas (454, 456) used in transmission diversity on the pointed satellite (320) are at the same time receiving diversity antennas pointing to the same satellite (320), and send N identical signals offset in time and in phase with one another to generate a coherent wavefront at the pointed satellite ( 320), and the transmission diversity management device (358) receives a measurement of the quality of the aggregation of the carriers transmitted by the N antennas in mode, the measurement of the quality of the aggregation carriers having been determined in terms of time and phase differences by a receiver (462) of a remote external ground station (464) and retransmitted via a terrestrial return channel transmission channel (466) or via a symmetrical channel channel return of the pointed satellite (320), and corrects the time and phase offset instructions, supplied to the multichannel transmission and processing device (356), from the time and phase differences measured by the external ground station (464) .
[14" id="c-fr-0014]
14. Multi-antenna ground station according to claim 13, in which .- the N identical signals, shifted between them in time and in phase to generate a coherent wavefront at the level of the pointed satellite (320), are signals of an identical reference sequence, and the differential signals of the receiver (462) of the external ground station (464) are determined by correlation, or .- the N identical signals, shifted between them in time and in phase to generate a wavefront coherent at the pointed satellite, are signals obtained from replicas of the same traffic signal, and the differential signals from the receiver of the external ground station are determined by correlation of the received signal retransmitted by the satellite (320).
[15" id="c-fr-0015]
15. Method for transparent switching of a communication link in a reception mode or a dual reception / transmission mode from a first originating satellite S1 to a second destination satellite S2, the switching method being implemented by a station soil comprising:
.- an integer P, greater than or equal to two, of antennas (22, 24; 62, 64, 66; 112, 114, 116) capable of receiving each to follow, during the same predetermined period of time, a satellite (32, 34; 72, 74) taken from a first satellite S1 (32; 72) of origin and a second satellite S2 (34; 74) of destination, both in visibility during said period, a device for receiving and multi-channel processing (122), with P input terminals (132, 14, 136), connected respectively to P output terminals of the P antennas (112, 114, 116), for receiving at input of said device and processing P antenna signals received and supplied at the output of said reception antennas, and at P output terminals (142, 144, 146) for delivering in parallel P processed output signals, aligned with each other in time and in phase, obtained respectively from the PP antenna signals received , and a configurable diversity combination device (124), co nnected as input to the multi-channel reception and processing device (122), for combining part or all of the output processed signals according to a selection instruction of the output processed and processed signals to be combined, and a management device diversity and transparent switching (126) of the communication link, the switching method of the communication link being characterized in that the switching of the communication link consists of a succession of a number k, greater than or equal to 2, of transparent and unitary Bi tilting of antennas, selected according to a predetermined sequence, each transparent and unitary Bi tilting of antenna (44, 46; 84, 86, 88) being a tilting of an antenna (22, 24; 62, 64, 66) from a first configuration of diversity in operational reception C1 (i) in which the selected antenna is pointed with tracking on the first satellite S1, towards a second diversity configuration in operational reception C2 (i) in which the selected antenna is pointed with follow-up on the second satellite S2, at least one of the first and second configurations C1 (i), C2 (i ) of diversity in reception being a configuration in which diversity in reception is implemented on the two first and second satellites S1, S2.
[16" id="c-fr-0016]
16. A method of transparent switching of a communication link according to claim 15, in which each transparent and unitary switching Bi (44, 46; 84, 86, 88) comprises steps for controlling the reception and multi-channel processing device. as well as the configurable diversity combination device by determining and sending them respectively:
. * satellite acquisition pointing commands, and. * time and phase alignment commands for the P signals received at the input of the multi-channel reception and processing device developed as a function of time and phase difference measurements of P-1 signals received at input with respect to the signal received at input taken as reference signal, and. * an instruction for selecting the processed output signals to be combined as a function of the planning for switching from the first diversity configuration C1 to the second diversity configuration C2 and as a function of quality measurements of the signals received at the input of the reception and processing device, the control steps being implemented by the diversity management device and transparent switching of the communication link.

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同族专利:

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公开号 | 公开日

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US10256900B2|2019-04-09|

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FR3066664B1|2019-05-10|

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US20180337723A1|2018-11-22|

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EP3404849B1|2019-08-28|

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ES2753764T3|2020-04-14|

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CA3004859A1|2018-11-16|

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EP3404849A1|2018-11-21|

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法律状态:
2018-05-01| PLFP| Fee payment|Year of fee payment: 2 |

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2018-11-23| PLSC| Publication of the preliminary search report|Effective date: 20181123 |

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2019-04-29| PLFP| Fee payment|Year of fee payment: 3 |

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2020-05-05| PLFP| Fee payment|Year of fee payment: 4 |

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2022-02-11| ST| Notification of lapse|Effective date: 20220105 |

优先权:

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FR1700518A|FR3066664B1|2017-05-16|2017-05-16|MULTI-ANTENNA GROUND STATION FOR IMPLEMENTING A TRANSPARENT SWITCH WITH DIVERSITY FROM A SAILING SCREEN TO A DESTINATION SATELLITE AND CORRESPONDING TILTING METHOD|

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FR1700518|2017-05-16|FR1700518A| FR3066664B1|2017-05-16|2017-05-16|MULTI-ANTENNA GROUND STATION FOR IMPLEMENTING A TRANSPARENT SWITCH WITH DIVERSITY FROM A SAILING SCREEN TO A DESTINATION SATELLITE AND CORRESPONDING TILTING METHOD|

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EP18166710.6A| EP3404849B1|2017-05-16|2018-04-11|Multi-antenna ground station for performing a seamless handover with diversity between two passing satellites and corresponding switching method.|

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ES18166710T| ES2753764T3|2017-05-16|2018-04-11|Multi-antenna ground station to implement transparent switching with diversity between two roaming satellites and corresponding switching procedure|

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US15/973,315| US10256900B2|2017-05-16|2018-05-07|Multi-antenna ground station for implementing a seamless handover with diversity from an origin moving satellite to a destination moving satellite, and corresponding handover method|

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CA3004859A| CA3004859A1|2017-05-16|2018-05-14|Multi-antenna ground station for implementing a seamless handover with diversity from an origin moving satellite to a destination moving satellite, and corresponding handover method|