• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The present invention relates to a method (200) for transmitting a signal by a transmitting device (110) to a satellite (120) traveling in orbit around the Earth, said transmitting device (110) and the satellite (120) comprising wireless telecommunication means, said method comprises steps of: reception (210) by said transmitting device (110) of a signal emitted by the satellite (120), said presence signal; - analyzing (220) a frequency shift induced by Doppler effect on the presence signal received by said transmitting device (110); estimating (230) a subsequent time evolution of said frequency offset from a predetermined subsequent start time of transmission of the signal to be transmitted by the transmitting device (110) and over a predetermined duration of said signal to be transmitted; - Pre-compensation (240) of the subsequent estimated time evolution of the frequency shift on the signal to be transmitted.
    公开号:FR3060765A1
    申请号:FR1662549
    申请日:2016-12-15
    公开日:2018-06-22
    发明作者:David Fernandez；Christophe Fourtet
    申请人:Sigfox SA；
    IPC主号:
    专利说明:

    TECHNICAL AREA
    The present invention belongs to the field of wireless telecommunications systems and relates more particularly to a method of transmitting a signal between at least one transmitting device and at least one satellite moving in orbit.
    The invention finds particular application in the field of connected objects.
    STATE OF THE ART
    The present invention finds a particularly advantageous, although in no way limiting, application in wireless telecommunications systems with ultra narrow band. By “ultra narrow band” (“Ultra Narrow Band” or UNB in Anglo-Saxon literature), it is meant that the instantaneous frequency spectrum of the radio signals emitted by a transmitting device, bound for a satellite, is of frequency width less than two kilohertz, or even less than one kilohertz.
    Such UNB wireless telecommunications systems are particularly suitable for applications of the M2M type (acronym for "Machine-to-Machine") or of the "Internet of Things" ("Internet of Things" or loT type in English literature). -saxonne).
    One of the major drawbacks of wireless telecommunications systems comprising a transmitting device and a non-geosynchronous satellite is the appearance of the Doppler effect which disturbs the transmission of signals between the transmitting device and the satellite. The Doppler effect, a function of the speed of the moving object and the angle between the speed vector of the moving object and the direction between the two objects, changes the frequency of the transmitted signals at all times. Thus, for the reception of a signal having been transmitted on a constant transmission frequency over time, the frequency of reception of the signal at the start of reception is different from the reception frequency of the signal at the end of reception . The variation in the reception frequency over time can also be significant because, for M2M or loT type applications, the data rate is generally low so that the duration of the signal can be significant. This evolution of the reception frequency over time makes the detection of such signals complex at the satellite level.
    Another drawback induced by the appearance of the Doppler effect on the signals is the reduction in the capacity of the communication channel for the same bandwidth. In addition, the Doppler effect also involves increasing the number of collisions between signals.
    STATEMENT OF THE INVENTION
    The object of the present invention is to remedy all or part of the limitations of the solutions of the prior art, in particular those set out above, by proposing a solution allowing a satellite of a telecommunications system to more easily detect transmitted signals. by transmitting devices and / or reduce collisions between signals transmitted by such transmitting devices.
    To this end, and according to a first aspect, the invention relates to a method of transmitting a signal by a transmitting device to a satellite moving in orbit around the Earth, said transmitting device and the satellite comprising telecommunication means without wire.
    By transmitting device is meant any object provided with a means of telecommunication capable of transmitting a signal. The transmitting device can for example be a connected object. By connected object is meant any device connected to a computer network for exchanging data such as the Internet, which can be interrogated or controlled remotely. The connected object is of any type. It can for example be a weather station collecting the indoor and outdoor temperature data of a dwelling, a sensor for measuring the level of liquid or gas in a tank or a tank, a detector for occupying a parking space , a sensor for measuring the flow of people entering a building, etc. The connected object can also be a relay base between a connected device and a network. This relay base can act as a repeater or buffer by storing data to be transmitted to the network in a computer memory of the relay base.
    According to the invention, said method comprises steps of:
    - reception by said transmitter device of a signal transmitted by the satellite, called presence signal;
    - Analysis of at least one frequency offset induced by Doppler effect on the presence signal received by said transmitter device, the analysis step comprising a measurement of a temporal evolution of the frequency offset induced by Doppler effect on the presence signal ;
    - estimation, as a function of the analysis of the frequency offset induced by the Doppler effect on the presence signal, of a subsequent temporal evolution of said frequency offset from a predetermined later instant of the start of emission of the signal to be emitted by the transmitter device, said instant of transmission, and over a predetermined duration of said signal to be transmitted;
    - precompensation of the estimated future time evolution of the frequency offset on the signal to be transmitted;
    - transmission of the signal by said transmitting device from the moment of transmission.
    Thus, the signal emitted by the transmitting device which can be precompensated during the major part of its emission, or even preferentially at each instant of its emission, is received by the satellite without apparent Doppler effect. In other words, taking the example of a signal comprising a constant frequency carrier before precompensation, the signal is precompensated before or at the time of transmission so that the reception frequency of the carrier of the signal received by the satellite is constant.
    During the analysis step, the temporal evolution of the frequency shift induced by the Doppler effect can be measured by measuring the temporal variation of a main frequency of the presence signal. The main frequency of the presence signal is representative for example of the frequency of a carrier of said presence signal, or also of the frequency of a subcarrier of said presence signal, of a central frequency of an instantaneous frequency spectrum of said presence signal, of a minimum or maximum frequency of said instantaneous frequency spectrum, etc. The temporal variation of the main frequency of the presence signal received is in principle similar to the temporal variation of the frequency offset, in particular when the presence signal is transmitted with a main frequency constant over time. The temporal variation of the main frequency can be measured directly by measuring the difference between the main frequency at two different respective times or indirectly by measuring the main frequency in at least two different respective times, and by calculating the difference between the main frequencies measured.
    Furthermore, the analysis of the precompensated signal received by the satellite is easier to perform, since it does not require specific processing of the received signal in order to overcome the Doppler effect, de facto reducing the number of calculations necessary to detect and possibly demodulate the received signal.
    On the other hand, given that the temporal variation of the frequency shift induced by the Doppler effect is no longer apparent, algorithms and computer programs adapted to stationary objects can be reused without requiring any particular adaptation.
    It should be emphasized that only the temporal variation of the frequency offset, or temporal drift of the frequency, due to the Doppler effect, is corrected. Precompensation takes into account only the temporal evolution of the frequency shift and not the absolute value of the frequency shift. In other words, the reception frequency of the carrier of the received signal is substantially constant if the carrier before precompensation is of constant frequency, but can nevertheless be offset from the theoretical frequency of said carrier of said signal due to the frequency offset. induced by Doppler Effect. Precompensation thus aims to obtain a frequency shift induced by the Doppler effect perceived at the satellite level as being invariant over time.
    In particular modes of implementation, the transmission method may also include one or more of the following characteristics, taken in isolation or in any technically possible combination.
    In particular modes of implementation, the step of precompensation of the subsequent temporal evolution of the frequency offset comprises a modulation of the signal to be transmitted with a frequency opposite to subsequent temporal revolution.
    In particular modes of implementation, the subsequent temporal evolution of the frequency offset is estimated by extrapolation of the temporal evolution of the frequency offset measured on the presence signal.
    In particular modes of implementation, the measured temporal evolution of the frequency offset is represented by a curve whose parameters are calculated by a curve fitting method.
    Curve fitting methods are also known as regression methods.
    In particular modes of implementation, the analysis step comprises a measurement of a main frequency of the presence signal and an estimation of a frequency offset induced by Doppler effect on the presence signal as a function of the main frequency measured and as a function of a theoretical main frequency of said presence signal, said method also comprising steps of:
    - estimation, as a function of the estimated frequency offset on the presence signal, of a subsequent frequency offset induced by Doppler effect at the time of emission of the signal to be emitted,
    - precompensation of the subsequent frequency shift on the signal to be transmitted.
    In such implementation modes, the aim of precompensation is therefore to cancel not only the temporal variation of the frequency offset induced by Doppler effect at the satellite level, but also to cancel the absolute value of said frequency offset at said satellite. Thus, the precompensation also makes it possible to obtain that the frequency of the carrier of the signal received by the satellite is substantially equal to the theoretical frequency of the carrier of the signal transmitted by the transmitting device.
    In particular modes of implementation, the analysis step implements a phase locked loop.
    In particular modes of implementation, the presence signal is transmitted continuously over a predetermined period.
    According to a second aspect, the present invention relates to a transmitter device of a wireless telecommunication system, implementing a transmission method according to any one of the embodiments of the invention.
    In particular embodiments, the transmitting device is a connected object.
    According to a third aspect, the present invention relates to a wireless telecommunications system comprising at least one transmitting device according to any one of the embodiments of the invention and at least one satellite moving in orbit around the Earth.
    PRESENTATION OF THE FIGURES
    The invention will be better understood on reading the following description, given by way of nonlimiting example, and made with reference to the figures which represent:
    - Figure 1: a schematic representation of an exemplary embodiment of a telecommunications system,
    - Figure 2: curves illustrating the variations of the frequency offset as a function of the position of a satellite relative to a transmitting device of the telecommunications system of Figure 1,
    - Figure 3: a diagram illustrating an example of implementation of a signal transmission method by a transmitting device to a satellite,
    - Figure 4: two curves illustrating a processing carried out for the detection of a presence signal emitted by the satellite,
    - Figure 5: curves illustrating the different treatments carried out on a signal emitted by a transmitting device of the telecommunication system.
    In these figures, identical references from one figure to another denote identical or analogous elements. For the sake of clarity, the elements shown are not to scale, unless otherwise stated.
    DETAILED DESCRIPTION OF EMBODIMENTS
    FIG. 1 schematically represents a wireless telecommunications system 100 comprising a plurality of transmitting devices 110 and a satellite 120 of a constellation of nanosatellites previously put into orbit around the Earth.
    The transmitting devices 110 and the satellite 120 exchange data in the form of radio signals. By "radio signal" is meant an electromagnetic wave propagating via non-wired means, the frequencies of which are included in the traditional spectrum of radio waves (a few hertz to several hundred gigahertz).
    The transmitting devices 110 are in the present nonlimiting example of embodiment of the invention of the connected objects comprising telecommunication means 111 able to transmit signals to the satellite 120. It should be emphasized that the transmitting devices 110, hereinafter called objects connected 110, can also, in particular embodiments, exchange signals between them.
    For example, the connected objects 110 further comprise an electronic card 112 provided with a microprocessor capable of processing data, or even of a computer memory capable of storing data before their transmission by means of signals.
    The signals transmitted by the connected objects 110, and / or the signals transmitted by the satellite 120, are for example ultra narrow band signals (UNB, acronym for “Ultra Narrow Band”).
    The UNB signals exchanged within the telecommunications system 100 include a carrier whose frequency is for example of the order of a hundred MHz, or even GHz. The bandwidth of UNB signals is less than 2 kHz or even less than 1 kHz.
    The telecommunication means 111 connected to the electronic card 112 of said connected object 110 include in the present nonlimiting example of the invention an antenna capable of transmitting and receiving UNB signals, a phase locked loop and a super-reaction receiver.
    The satellite 120 is in the present example, a nanosatellite of the CubeSat type formed by a cubic structure of ten centimeters on a side. Two photovoltaic panels 121 deployed on either side of the cubic structure supply the satellite 120 with energy. The mass of satellite 120 is approximately equal to five kilos. An antenna 122 directed towards the earth's surface makes it possible to transmit or receive UNB signals to or from connected objects 110. It should be emphasized that the satellite
    120 is placed in an orbit of around five hundred kilometers around the Earth. The satellite 120 thus travels around the Earth at a speed of the order of seven kilometers per second, and makes a complete revolution around the planet in a duration of the order of ninety minutes. More generally, satellite 120 is in non-geosynchronous orbit, for example in LEO (“Low Earth Orbit”) or MEO (“Medium Earth Orbit”) orbit.
    The satellite 120 also comprises a beacon 125, also known by the English term "beacon", transmitting a UNB signal continuously, hereinafter called the presence signal. The presence signal emitted by the beacon 125 comprises, for example, a carrier whose frequency, at the time of remission, is for example constant over time.
    In a variant of this particular embodiment of the invention, the beacon 125 transmits presence signals in a discontinuous manner, preferably at regular intervals. The presence signals transmitted are for example of limited duration, for example of the order of a few hundred milliseconds, a few seconds, or even a few minutes.
    It should be emphasized that for the sake of energy saving, the connected object 110 is generally, but not limited to, in standby mode for most of the time and that it comes out of this standby mode at regular intervals to listen and / or transmit signals.
    FIG. 2 represents an example of curves 150 of the temporal evolution of the frequency offset undergone by signals received by the connected object 110 from the satellite 120, as a function of the position of the satellite relative to the connected object. FIG. 2 comprises five curves, each of which corresponds to a different maximum elevation angle from the satellite 120 seen by the connected object 110. The term “maximum elevation angle”, also known by the English term “cross-track angle”, is understood , the angle between the ground and the direction of the satellite 120, measured at the level of the object when the satellite 120 is closest to the connected object 110. The abscissa of the curves 150 corresponds in the present example to the difference between the latitude of the satellite 110 and the latitude of the connected object 110. When the maximum elevation angle is small, as in the case of the curve 150i, the satellite 120 is seen by the connected object 110 as being close of the horizon, while when the maximum elevation angle is of the order of ninety degrees, as in the case of curve 1502, the connected object 110 is located substantially below the trajectory of satellite 120.
    FIG. 3 shows in the form of a block diagram a method 200 of transmitting a signal between one of the connected objects 110 and the satellite 120 moving in orbit.
    The method 200 comprises a step 210 of reception by the connected object 110 of the presence signal transmitted by the satellite 120.
    In preferred embodiments, the presence signal comprises a carrier of frequency f c _ sa t and at least one modulated subcarrier having a predetermined frequency deviation fs from the frequency f c _ sa t in order to be able to differentiate the signals from the beacons from the signals from the connected objects 110, which do not have this particular shape or which otherwise have a predetermined frequency difference different from the frequency difference fs of the presence signal.
    In other words, the presence signal of the satellite 120 includes information making it possible to identify the source of the presence signal, that is to say in the present case of the beacon 125 of the satellite 120, via of the presence of the modulated subcarrier having a predetermined frequency deviation fs from the frequency f c sa t. More generally, the identification information of the presence signal can be coded in the presence signal emitted by the beacon 125 by any technique known to those skilled in the art.
    It should be emphasized that such a presence signal comprising a carrier and at least one subcarrier is of the self-synchronous type.
    The presence signal emitted by the beacon 125 with a carrier of frequency f c _ sa t is received by the connected object 110 with a carrier of frequency f ' c _sat = f c _sat + ûf (t) where Af (t) represents the frequency shift induced by the Doppler effect which varies during the transmission of the presence signal of the beacon 125 from the satellite 120 to the connected object 110.
    A V * cos (0 (t)) * cos (<jo (t) + F (t)) * fc
    - c where v represents the standard of the satellite speed vector, f c the carrier of the transmitted signal, here equal to f c _sat, c the speed of light,
    Θ the angle between the speed vector of satellite 120 and the plane defined by satellite 120, object 110 and the center of the Earth,
    E the angle of elevation between the horizon and the satellite 120 at the level of the object 110, φ the angle, also called coverage angle, between the sub-satellite point, i.e. the point of the satellite projected onto the earth's surface and object 110.
    It should be emphasized that the frequency offset varies over time because the angles θ, E and φ vary as a function of the movement of the satellite 120 relative to the connected object 110.
    The recognition of the presence signals by virtue of the presence of a subcarrier having a predetermined frequency deviation from the carrier is advantageously used in the case of a telecommunication network, called a hydride, comprising a plurality of connected objects and a plurality of satellites, in which a connected object can receive signals from both a satellite and another connected object.
    Step 210 includes, for example, a sub-step 211 of detecting the signal of the beacon 125 from among a plurality of received signals. To this end, the super-reaction receiver included in the connected object 110 makes it possible to detect the presence signal emitted by the beacon 125 by virtue of the presence of the subcarrier in the presence signal, including the frequency deviation from the carrier frequency of the presence signal is advantageously predetermined. It should be emphasized that the super-reaction receiver advantageously has a very low energy consumption of the order of one hundred microwatts in active reception. The consumption of the super-reaction receiver can be reduced by performing recurrent, non-contiguous detections, through detection cycles. Increasing the latency between two consecutive detections notably makes it possible to reduce the consumption of this receiver.
    Furthermore, it should be emphasized that the super-reaction receiver is advantageously insensitive to frequency variations if the carrier and the subcarriers vary in a similar manner, as is the case when the presence signal undergoes the Doppler effect.
    An example of the result obtained by this detection mechanism is illustrated in FIG. 4 which includes a curve 310 before detection and a curve 320 after detection. The curve 310 comprises a carrier 311 of frequency f'c_sat θΐ a modulated subcarrier 312 of frequency f 2 . The frequency difference between the carrier and the subcarrier is equal to fs. The detection makes it possible to extract a signal 321 of frequency fs, a signal 322 of frequency 2f ' c _ sa t, a signal 323 of frequency f' c _ S at + f2 and a signal 324 of frequency 2f 2 .
    An analysis of at least one frequency offset induced by Doppler effect on the presence signal received by the connected object 110 is carried out during a step 220 of the method 200.
    During this analysis step 220, a measurement of a temporal evolution of the frequency offset Δί induced by Doppler effect on the presence signal received by the connected object 110 is carried out.
    This measurement is for example carried out by means of the phase-locked loop included in the connected object 110 by measuring the main frequency of the presence signal received by the connected object 110 at at least two distinct times, preferably at each moment of reception of the presence signal. The temporal evolution of the frequency offset Δί is in fact equal to the temporal variation of the main frequency of the presence signal received.
    From the analysis of the frequency shift induced by Doppler effect on the presence signal, an estimate of a subsequent time change in the frequency shift is carried out during a step 230 of the method 200. This subsequent time change in the frequency shift is notably calculated in order to predict the frequency offset undergone by the signal to be emitted by the connected object 110 during its transmission to the satellite 120. The subsequent temporal evolution of the frequency offset is thus estimated from a predetermined later instant of the start of transmission of the signal to be transmitted by the device 110, said instant of transmission, and over a predetermined duration of this signal to be transmitted. This predetermined duration corresponds in particular to the duration of emission of the signal.
    In preferred modes of the invention, the subsequent temporal evolution of the offset is estimated by extrapolation of the temporal evolution of the frequency offset previously measured during step 220.
    The temporal evolution of the frequency offset previously measured can be represented by the intermediary of the theoretical curve Af (t) whose parameters are adjusted for example via methods of regression of curves, also called methods of curve adjustment (in English "Curve fitting").
    The estimation of the subsequent temporal evolution of the frequency offset can be carried out from this theoretical curve, the parameters of which have been adjusted.
    Once the subsequent temporal evolution is estimated, a precompensation of the subsequent temporal evolution on the presence signal is carried out during a step 240 of the method 200.
    In preferred embodiments of the invention, the step of precompensation 240 of the subsequent temporal evolution of the frequency offset comprises a modulation of the signal to be transmitted with a frequency opposite to the subsequent temporal evolution. The precompensation can be carried out for example by means of an FM modulation (English acronym of "Frequency Modulation") whose modulated frequency is equal to the opposite of the variation to be precompensated.
    It should be emphasized that this FM modulation is applied over a conventional modulation of encoding of the binary data contained in the signal emitted by the connected object 110. The conventional modulation of encoding of the binary data is, in the present example non-limiting of the invention, a modulation of the DBPSK type (English acronym for "Digital Binary Phase-Shift Keying") comprising a bit rate of 100 bits per second.
    The precompensated signal is then transmitted, from the time of transmission, during a step 250 of the method 200.
    It should be emphasized that precompensation makes it possible in particular to obtain at the time of reception by the satellite 120 of the signal emitted by the connected object 110, that the frequency of reception of the signal carrier by the satellite 120 is substantially constant throughout along the reception.
    The satellite 120 can therefore process the received signal without the need to apply to it a complex processing for correcting the temporal drift of the frequency due to the Doppler effect. It is thus possible to reuse the algorithms developed for communication between immobile objects. The computing power of the satellite is then used only to demodulate signals that have apparently not undergone a Doppler effect.
    Furthermore, it should be emphasized that the precompensation proposed in the present example does not take into account the absolute value of the frequency offset. The frequency of the carrier of the signal received by the satellite 120 is certainly constant but is generally different from the frequency of the carrier of the signal at the time of its emission by the connected object 110.
    For this purpose, it can optionally be provided for the analysis step to further comprise a measurement of a main frequency of the presence signal and an estimation of a frequency offset induced by Doppler effect on the presence signal in as a function of the main frequency measured and as a function of a theoretical main frequency of the presence signal. The theoretical frequency of the presence signal, which corresponds to the frequency of the carrier at the time of the transmission of the presence signal by the beacon 125, is in certain cases known in advance, in which case the beacon 125 transmits on a frequency predetermined corresponding for example to a previously established standard. When the carrier transmission frequency is a priori unknown, the value of said transmission frequency can for example be coded in the presence signal, and for example modulates the modulated subcarrier of said presence signal. The measurement of the main frequency can in particular be carried out using the phase-locked loop included in the connected object 110.
    Thus, the method 200 can also include a step 235 of estimation, as a function of the frequency offset estimated on the presence signal, of a frequency offset induced by Doppler effect at the instant of transmission of the signal to be transmitted, called offset subsequent frequency. A precompensation of the subsequent frequency offset can also be carried out on the signal to be emitted by the connected object 110, during a step 245 of the method 200, before or after the precompensation of the estimated subsequent temporal evolution of the frequency offset.
    In this case, the frequency of reception of the signal carrier by the satellite 120 is substantially equal to the transmission frequency of the carrier of said signal by the connected object 110, with the two precompensations by the connected object 110.
    FIG. 5 illustrates the temporal evolution of the transmission frequency of a carrier of a signal 510 transmitted by the connected object 110 without precompensation of the Doppler effect, of the same signal 520 transmitted with precompensation of the temporal evolution of the frequency offset and of the same signal 525 transmitted with also the optional precompensation of the frequency offset.
    The frequency of transmission of the carrier of the signal 510 without precompensation is constant during the transmission of the signal 510. The frequency of reception of the carrier of the signal 510 by the satellite 120 is represented in FIG. 5 by the signal 530. The difference between signal 510 and signal 530 corresponds to the frequency shift induced by Doppler effect on the frequency of the carrier of signal 510 during its transmission. It should be emphasized that this frequency offset being a function of the speed and of the relative position of the satellite 120 with respect to the connected object 110 evolves over time. In order to counterbalance the temporal frequency drift of the by the Doppler effect, a precompensation of the temporal evolution of the frequency offset is carried out on the signal 510. The result obtained by this precompensation is the signal 520 which is seen by the satellite 120 at the time of its reception as a signal 540 having a reception frequency of the carrier constant but generally different from the transmission frequency of the carrier of the signal 510.
    In order to obtain a reception frequency which is constant but also identical to the transmission frequency of said signal carrier 510, a frequency offset precompensation can be applied to signal 520, so that the transmission frequency of the carrier corresponds to that illustrated by the signal 525. When the signal 525 is transmitted by the connected object 110, it is received by the satellite as a signal 550 whose frequency of reception of the carrier by said satellite 120 is constant and identical to the transmission frequency of the signal carrier 510.
    Optionally, the method 200 can also comprise a step of identifying the signals intended for the satellite 120 among a plurality of signals received by the satellite 120. Since the signals intended for the satellite 120 are precompensated, they are easy to identify because they do not require prior treatment to correct the Doppler effect. This step is particularly useful in the case of a hybrid telecommunications system.
    权利要求:
    Claims (8)
    [1" id="c-fr-0001]
    1 - Method (200) of transmitting a signal by a transmitting device (110) to a satellite (120) moving in orbit around the Earth, said transmitting device (110) and the satellite (120) comprising means for wireless telecommunications,
    5 characterized in that said method comprises steps of:
    - Reception (210) by said transmitting device (110) of a signal transmitted by the satellite (120), said presence signal;
    - analysis (220) of a frequency offset induced by Doppler effect on the presence signal received by said transmitter device (110), the step
    10 analysis (220) comprising a measurement of a temporal evolution of the frequency shift induced by Doppler effect on the presence signal;
    - estimate (230), based on the analysis of the frequency shift induced by the Doppler effect on the presence signal, of an evolution
    15 subsequent time of said frequency offset from a predetermined later instant of the start of emission of the signal to be transmitted by the transmitter device (110), said instant of transmission, and over a predetermined duration of said signal to be transmitted;
    - precompensation (240) of the estimated future temporal evolution
    20 of the frequency shift on the signal to be transmitted;
    - transmission (250) of the signal by said transmitting device (110) from the moment of transmission.
    [2" id="c-fr-0002]
    2 - Method (200) according to claim 1, characterized in that the step of precompensation (240) of the subsequent time evolution of the offset
    25 frequency includes modulation of the signal to be transmitted with a frequency opposite to the subsequent time course.
    [3" id="c-fr-0003]
    3 - Method (200) according to any one of claims 1 to 2, characterized in that the subsequent temporal evolution of the frequency offset is estimated by extrapolation of the temporal evolution of the
    30 frequency offset measured on the presence signal.
    [4" id="c-fr-0004]
    4 - Method (200) according to any one of claims 1 to 3, characterized in that the measured time evolution of the frequency offset is represented by a theoretical curve whose parameters are calculated by a curve adjustment method.
    [5" id="c-fr-0005]
    5 - Method (200) according to any one of claims 1 to 4, characterized in that the analysis step (230) comprises a measurement of a main frequency of the presence signal and an estimation of a frequency offset induced by Doppler effect on the presence signal as a function of the measured main frequency and as a function of a theoretical main frequency of said presence signal, said method also comprising steps of:
    - estimation (235), as a function of the frequency offset estimated on the presence signal, of a subsequent frequency offset induced by Doppler effect at the time of emission of the signal to be transmitted,
    - precompensation (245) of the subsequent frequency shift on the signal to be transmitted.
    6 - Method (200) according to any one of claims 1 to 5, characterized in that the analysis step puts implement a loop at phase lock. 7 - Method (200) according to any one of claims 1 to 6,
    characterized in that the presence signal is transmitted continuously over a predetermined period.
    [6" id="c-fr-0006]
    8 - Transmitter device (110) of a wireless telecommunications system (100), characterized in that it implements the transmission method (200) according to any one of claims 1 to 7.
    [7" id="c-fr-0007]
    9 - Transmitter device (110) according to claim 8, characterized in that said transmitter device is a connected object.
    [8" id="c-fr-0008]
    10-wireless telecommunications system (100) characterized in that it comprises at least one transmitting device (110) according to any one of claims 8 to 9, and at least one satellite (120) moving in orbit around Earth.
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    EP3556028A1|2019-10-23|
    CN110226296B|2021-10-29|
    EP3556028B1|2020-09-02|
    RU2019121629A|2021-01-15|
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    法律状态:
    2017-12-29| PLFP| Fee payment|Year of fee payment: 2 |
    2018-06-22| PLSC| Publication of the preliminary search report|Effective date: 20180622 |
    2019-12-27| PLFP| Fee payment|Year of fee payment: 4 |
    2020-12-31| PLFP| Fee payment|Year of fee payment: 5 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1662549|2016-12-15|
    FR1662549A|FR3060765B1|2016-12-15|2016-12-15|METHOD OF PROCESSING THE DOPPLER EFFECT OF A SIGNAL TRANSMITTED BY A TRANSMITTING DEVICE TO A NON-GEOSYNCHRONOUS SATELLITE|FR1662549A| FR3060765B1|2016-12-15|2016-12-15|METHOD OF PROCESSING THE DOPPLER EFFECT OF A SIGNAL TRANSMITTED BY A TRANSMITTING DEVICE TO A NON-GEOSYNCHRONOUS SATELLITE|
    US16/469,362| US10505624B2|2016-12-15|2017-12-14|Method for processing the doppler effect of a signal transmitted by a transmitter device to a non-geosynchronous satellite|
    CN201780084696.2A| CN110226296B|2016-12-15|2017-12-14|Method for processing the Doppler effect of signals transmitted by a transmitter device to a non-geostationary satellite|
    PCT/FR2017/053591| WO2018109411A1|2016-12-15|2017-12-14|Method for processing the doppler effect of a signal transmitted by a transmitter device to a non-geosynchronous satellite|
    EP17825577.4A| EP3556028B1|2016-12-15|2017-12-14|Method for processing the doppler effect of a signal transmitted by a transmitter device to a non-geosynchronous satellite|
    AU2017374685A| AU2017374685A1|2016-12-15|2017-12-14|Method for processing the doppler effect of a signal transmitted by a transmitter device to a non-geosynchronous satellite|
    RU2019121629A| RU2747850C2|2016-12-15|2017-12-14|Method for processing effect of doppler signal transmitted by transmitting device to non-geostationary satellite|
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