A system using modulated signals to compensate for frequency errors in LTE signals

Abstract

In satellite communication systems, the carrier offset detection function of the demodulator included in the on-board modem of the M&C channel is used. This modem analyzes the baseband signal in the baseband converter to detect the frequency error Δf that occurs in the signal path from the output of the terrestrial base station to the baseband conversion output of the satellite, and converts it to the received carrier f ’ c and calculate the expected frequency (f c ) and detect it by subtracting it from

Description

[Technical field]

[0001] Related Applications This application claims the benefit of priority to Indian Patent Application No. 202011001814, filed on January 15, 2020, and U.S. Provisional Application No. 63 / 033087, filed on June 1, 2020, the contents of which are incorporated by reference in their entireties and relied upon herein. [Background technology]

[0002] U.S. Patent No. 9,973,266 discloses a system for assembling a large number of small satellite antenna assemblies in space to form a large array. The entire contents of the '266 patent are incorporated herein by reference. As disclosed in the '266 patent, FIGS. 1(a) and 1(b) show a satellite communication system 100 having an array 300 of a plurality of small satellites 302 and a central or control satellite 200. The small satellites 302 communicate with end users 500 in a footprint 400 on Earth and with the control satellite 200, which further communicates with a gateway 600 at a base station. Each of the plurality of small satellites 302 can include, for example, a processing unit (e.g., a processor or controller) and one or more antenna elements. And the control satellite 200 can include a processing unit and one or more antennas or antenna elements.

[0003] Terrestrial mobile phone base stations must comply with current specifications for radio transmission and reception, such as 3GPP TS 36.104 V12.10.0 (2016-01). In particular, this specification mentions requirements for frequency accuracy and stability of signals transmitted by the base station. Terrestrial base stations can meet this demand by using a highly accurate and stable clock source.

[0004] To provide economically efficient connectivity to sparsely populated remote areas and ships on the high seas, the earth station equipment (see FIG. 2) radiates (to space) from the base station processor 13 multiple signals that are upconverted to a higher spectral band by the Q / V band interface 16 for spectrum utilization and antenna size reasons, and then frequency multiplexed by a multiplexer, typically in the MUX / DE-MUX 15.

[0005] In space, these signals are received by the satellite equipment (see Figure 3), downconverted to baseband signals by the Q / V band interface 26, demultiplexed by a demultiplexer in the MUX / DE-MUX compensator 25, upconverted back to the mobile spectrum, and relayed by the transmitter / receiver 27 to the user equipment on the ground over a wide field of view (FoV) that mimics the range of a wide area base station. Summary of the Invention

[0006] In such cases, it is very difficult to ensure the accuracy of the signal frequency due to the difference in frequency between the earth station clock source 14 and the satellite device clock source 24, and the Doppler effect due to the motion of the non-geostationary satellite relative to the earth station. These can be addressed to some extent by using highly accurate stable clocks and Doppler compensation of the signal, but the uncorrected frequency error due to the prediction error of the satellite position (and motion) and the short-term (unstable) stability of the clock oscillator can easily exceed the allowable error (currently + / - 0.05 ppm for wide area base stations). For example, the '266 patent discloses that the array 300 forms multiple beams, each of which is pre-compensated for the Doppler frequency shift caused by a satellite based on the satellite ephemeris and the latitude and longitude of the beam center.

[0007] The radio communication link between the earth station and the satellite typically carries signals for the purpose of monitoring and controlling (Monitor and Control, M&C) the satellite's subsystems, in addition to transmitting signals that are relayed to the user equipment (UE) via the satellite and receiving signals from the UE via the satellite. [Brief description of the drawings]

[0008] [Figure 1(a)] FIG. 1(a) is a diagram showing a known phased array. [Figure 1(b)] FIG. 1(b) is a diagram showing a known phased array.

[0009] [Diagram 2] FIG. 2 is a block diagram illustrating an earth station apparatus and a transmitted baseband spectrum in one embodiment of the present disclosure.

[0010] [Diagram 3] FIG. 3 is a block diagram illustrating an apparatus and received baseband spectrum of a non-geostationary satellite in accordance with one embodiment of the present disclosure.

[0011] [Figure 4] FIG. 4 is a flow diagram illustrating an uplink signal flow from a UE to an eNodeB; and

[0012] [Diagram 5] FIG. 5 is a flow diagram illustrating the flow of downlink signals from an eNodeB to a UE. Detailed Description

[0013] In describing non-limiting embodiments, specific terms will be used for clarity in illustrating the present disclosure as depicted in the drawings. However, the present disclosure is not intended to be limited to the specific terms so selected, and each specific term is understood to include all technical equivalents that operate in a similar manner to achieve a similar purpose. Although several embodiments of the present disclosure have been described for illustrative purposes, it is understood that the present disclosure may be embodied in other forms not specifically shown in the drawings.

[0014] Referring to the drawings, Figures 2 and 3 show a system and method in one non-limiting exemplary embodiment of the present disclosure. Figure 2 shows a ground station with a ground station system, which includes a processing unit 13 for a base station (similar to that used in a cell tower), a signal delay and Doppler compensator 15, a Q / V band interface 16, a stable clock source 14, and a modem 11. The processing unit 13 may be an eNodeB or a bank of eNodeBs, etc., and communicates signals with the compensator 15, which then conveys the signals to the interface 16. The eNodeB 13 transmits signals to the compensator 15, which performs delay and Doppler compensation and further includes a multiplexer for combining the signals. The compensated signals are then up-converted in the interface 16 and transmitted to the satellite. The clock source 14 communicates with the eNodeB 13, the compensator 15, and the interface 16 and provides a stable and accurate clocking signal to power the eNodeB 13, the compensator 15, and the interface 16.

[0015] The satellite equipment (FIG. 3) has a satellite system including a Q / V band interface 26, a processor compensator 25 for multiplexing, demultiplexing and frequency correction, a Tx / Rx transceiver 27, and a modem 21. Signals from the ground station are downconverted in the interface 26 and demultiplexed in the satellite compensator 25. The transceiver 27 relays the frequency corrected signals to terrestrial user equipment (e.g., mobile terminals such as smartphones) over a wide field of view (FoV) that mimics the coverage of a wide-area base station. A clock source 24 communicates with the interface 26, the satellite compensator 25, and the transceiver 27 and provides clock signals to operate the interface 26, the compensator 25, and the transceiver 27. On the return (uplink) path, signals from end users 500 are received by transceiver 27, multiplexed in compensator 25 and retransmitted via interface 26 to the gateway.

[0016] In the satellite system, a satellite modem 21 is connected to a satellite compensator 25. The satellite modem 21 receives monitor and control (M&C) data 23 from the multiplexer-demultiplexer of the compensator 25, some of which is fed to a frequency shifter in the satellite compensator 25 as a frequency error 22 with the ground station. The M&C data 23 may include data such as the number of beams, beam frequencies, spectrum allocation, bandwidth, etc., and may be obtained from the control center, eNodeB 13 or compensator 15. The frequency error occurs due to relative frequency errors of the clock sources 14, 24 in the gateway and the satellite, and errors in prediction of the satellite's position and dynamics (which leads to inaccurate Doppler frequency compensation in the gateway). The satellite system utilizes the carrier offset detection function of the demodulator included in the on-board modem 21 of the M&C channel 23. The modem 21 detects a frequency error Δf 22, which is the difference between the expected frequency (based on the spectrum allocation of the M&C channel) and the frequency observed at the satellite. This is caused in the signal path from the output of the base station 13 on the ground to the output of the baseband converter 26 on the satellite. The modem 21 analyzes the baseband signal using the carrier frequency estimation function of the demodulation section of the modem and estimates the received carrier f of the M&C channel 23 at the baseband converter 26. c and convert it to the expected frequency of M&C channel 23 (f c ) to similarly correct for frequency errors in the downlink beam signals.

[0017] The demultiplexer (demultiplexing function, separation function) of the compensator 25 separates the signals for each downlink beam, applies a frequency shift equal to the negative of Δf, and then converts the signals to the LTE band in a phased array 27 (e.g., a digital phased array) and transmits the signals for radiation to a ground user equipment (UE). The phased array 27 can be, for example, a phased array having multiple small satellites and a control satellite as shown in FIG. 1 and disclosed in U.S. Pat. No. 9,973,266.

[0018] Similarly, in the reverse direction, the ground station modem 11 receives the M&C channel data from the control satellite via interfaces 16 and 15. The demodulator in the ground station host modem 11 for the M&C channel analyzes the baseband signal at MUX / DE-MUX (multiplexer / demultiplexer) 15 to generate the receive carrier f c and convert it to the expected frequency (expected frequency, f c ) to estimate the frequency error 12 of the M&C channel. The expected frequency can be obtained from the M&C data. The demultiplexer 15 separates the signals received from each beam and then applies a frequency shift equal to the negative of Δf before transmitting them to the eNodeB 13 (the base station side of the normal terrestrial link). In this way, the base station and the UE receive at their inputs signals with the same frequency accuracy as they would be received in a normal 3GPP-compliant terrestrial mobile network.

[0019] Frequency errors in the carrier signal (both directions, from ground to satellite and from satellite to ground) violate the 3GPP standard and can cause communication degradation or interruption. Frequency errors are mainly caused by two factors. The received carrier frequency f i ' is "f i '=f i+Δf, for i=0...n, where Δf is the frequency offset due to the sum of (a) the difference (divergence) between the clock source 14 used for the up / down conversion at the earth station and the clock source 24 used for the up / down conversion at the satellite, and (b) the residual Doppler after Doppler compensation at the earth station compensator 15. The carrier frequency f i is the carrier frequency of the i-th signal transmitted to the UE. i is the expected frequency f c The Doppler correction must be based on the error detected at the satellite. As the satellite moves in orbit, the signal delay changes at the ground station, resulting in a Doppler shift. The system precompensates the signal sent to the satellite by shifting the signal in time and frequency to account for the delay and Doppler based on a prediction of the satellite's position. However, there may still be errors when the signal reaches the satellite. Thus, the Doppler correction is based on a predicted Doppler, but the prediction may be inaccurate and there may be residual errors detected by the demodulator of modem 11. In one embodiment, frequency correction is done in addition to or after the delay and Doppler correction.

[0020] This Δf is the same for the M&C channel (monitoring and control channel) and the eNodeB / UE carrier. Therefore, once estimated by the satellite / earth station M&C demodulator, it is used to correct the center frequency of all base station signals received from the terrestrial eNodeB and signals from the UE received via the satellite. This error can be different in each direction, from the gateway to the satellite and from the satellite to the gateway.

[0021] Referring to the drawings, Figures 4 and 5 show the above described process in the form of signal flow diagrams for the uplink 30 and downlink 70 signal paths, respectively. Referring to Figures 3 and 4, the uplink operation 30 starts at step 32, where the satellite equipment, e.g., beamforming phased array 27, forms beams and collects uplink signals from user equipment. These are multiplexed by the multiplexer in the compensator 25 with M&C signals (supervisory and control signals) from the modulator in the modem 21 (step 33) at intermediate frequency IF (step 34), upconverted by the interface 26 to V-band frequencies (step 36), amplified by the HPA and antenna and radiated towards the gateway (step 38).

[0022] 2 and 4, the interface 16 of the gateway device 10 includes an antenna and a low noise amplifier (LNA) that collects the signal emitted from the satellite interface 26 in step 38 (step 52) and downconverts it from the V-band to an IF frequency (step 54). The compensator 15 then demultiplexes the uplink and M&C signals (step 56) and compensates for delay and Doppler variations (step 58). The M&C signal is received from the satellite 20 (step 33). The M&C signal is sent to the demodulator of the modem 11 (step 57) to correct the carrier offset or frequency error Δf u is estimated (e.g., depending on the spectrum analysis resolution, this can be as little as 1 percent). The uplink signal is then corrected by compensator 15 for the estimated frequency error determined based on the M&C signal (step 59) and then sent to eNodeBs 13 (step 64) for processing of the user equipment (UE) originated uplink signal.

[0023] The operation of the downlink signal is shown in Figures 2 and 5. Here, the gateway device 10 including the eNodeB 13 provides the downlink signal to the UE in step 72. In parallel with this, M&C (Monitoring and Control) data is transmitted from the network control center (step 74) and modulated by the modulator of the modem 11 (step 75). The compensator 15 compensates for the delay and Doppler variations of the uplink signal and the M&C signal (step 73). Then, the multiplexer of the compensator 15 multiplexes the signal to an intermediate frequency (IF) (step 76). Then, the interface 16 upconverts the signal to a Q-band frequency (step 77), and the HPA and antenna amplify the signal and radiate it towards the satellite (step 78).

[0024] The satellite device 20 has an antenna and an LNA for receiving the signal radiated by the interface 16 in step 78. The phased array converts the Q-band signal to IF (step 83). The signal is demultiplexed (demultiplexed, separated) by the demultiplexer of the compensator 25 (step 84). The M&C signal is received from the ground station 10 (step 75) and then fed to a demodulator in the modem 21 (step 85), which corrects for the carrier offset or frequency error Δf d 22 is estimated (e.g., depending on the spectrum analysis resolution, this may be as little as one percent). Next, in compensator 25, the downlink signal is compensated for delay and Doppler, and then the estimated frequency error in the monitor and control signals is corrected (step 86), before being radiated by beamforming phased array 27 to the UE (step 88).

[0025] This system can also be used in other communication systems where multiple channels are multiplexed and communicated over a common radio link, and the baseband signal of only one of the channels can be analyzed to estimate its frequency error, which is common to all channels, so that the frequency error of the signal at the receiver can be corrected.

[0026] In the illustrated embodiment, the plurality of small satellites 302 and / or the central satellite 200 may include a processor or processing components for performing various functions and operations according to the present disclosure, such as the operations illustrated in Figs. 4, 5. Additionally, the ground station may have a processor 13 and processing components, and the satellite may have a processing component and a processor. The processor may be, for example, a computing device, a processor, an ASIC (Application Specific Integrated Circuits), or a controller. The processor may comprise at least one of a wide variety of components or subsystems, including, for example, a wired or wireless communication link, and / or one or more storage devices, such as analog or digital memories or databases. All or a portion of the systems, processes, and / or data utilized in the disclosed systems and methods may be stored on or read from a storage device. The processor may execute software that may be stored on the storage device. Unless otherwise indicated, the processes are preferably performed automatically by the processor in substantially real time without delay.

[0027] In the embodiment of Figs. 2-3, the system includes a demodulator for determining a frequency error and a compensator for applying an error correction to the received signal. However, any suitable components may be provided, such as a device, e.g., a comparator, for determining the frequency error and a subtractor for applying the error correction. It is further noted that the system includes common processing and communication components, such as a Q / V band interface, an eNodeB, a multiplexer, and a demultiplexer. It should be clear that any other suitable components may be utilized and the above components and operations are not required. For example, the estimation of the frequency error may be implemented in a system that does not include a multiplexer, a demultiplexer, or a Q / V band interface.

[0028] The foregoing description and drawings should be considered merely as illustrative of the principles of the present disclosure, which may be configured in various ways and is not intended to be limited by the embodiments described herein. Numerous applications of the present disclosure will readily occur to those skilled in the art. Thus, it is not desired to limit the present disclosure to the specific examples disclosed or to the exact construction and operation shown and described. Rather, all suitable modifications and equivalents are intended to be within the scope of the present disclosure.

Claims

1. An antenna configured to receive a transmission signal and a supervisory and control signal; a demultiplexer configured to demultiplex the transmit signal and the supervisory and control signal to provide a demultiplexed transmit signal and a demultiplexed supervisory and control signal; a compensator configured to compensate for delay and Doppler variations in the demultiplexed transmit signals and the demultiplexed monitor and control signals to provide delay- and Doppler-compensated transmit signals and delay- and Doppler-compensated monitor and control signals; a modem including a demodulator configured to receive the delay and Doppler compensated monitor and control signals, the demodulator configured to determine a residual frequency error in the delay and Doppler compensated monitor and control signals; The compensator is further configured to compensate the delay and Doppler compensated transmit signal for the residual frequency error to provide a residual frequency error compensated transmit signal.

2. In claim 1, The ground station further comprises a processor configured to process the residual frequency error compensated transmission signal.

3. In claim 1 or 2, The transmission signal includes an uplink signal.

4. In claim 2, The processing device is a ground station, including an eNodeB.

5. In any one of claims 1 to 4, The demodulator is configured to determine the residual frequency error by determining a frequency offset relative to the delay and Doppler compensated monitor and control signal carrier signal.

6. In any one of claims 1 to 4, the demodulator is configured to determine the residual frequency error by subtracting an expected frequency of the delay- and Doppler-compensated monitoring and control signals from a received carrier frequency of the delay- and Doppler-compensated monitoring and control signals, the earth station.

7. In claim 6, The demodulator is configured to determine the received carrier frequency.

8. In any one of claims 1 to 7, The antenna is configured to receive the transmitted signals from user equipment via a satellite, at a ground station.

9. an antenna configured to receive the transmission signal and the monitoring and control signal; a demodulator configured to determine a residual frequency error of said monitor and control signals that has been compensated for delay and Doppler variations; a compensator configured to compensate the transmit signal for the residual frequency error to provide a transmit signal compensated for residual frequency error.

10. In claim 9, The demodulator is configured to determine the residual frequency error by determining a frequency offset of the supervisory and control signal relative to a carrier signal.

11. In claim 9, The earth station, wherein the demodulator is configured to determine the residual frequency error by subtracting an expected frequency of the supervisory and control signals from a received carrier frequency of the supervisory and control signals.

12. In claim 11, The demodulator is configured to determine the received carrier frequency.

13. a receiving antenna configured to receive the transmission signal and the supervisory and control signal from the ground station; a demultiplexer configured to demultiplex the transmit signal and the supervisory and control signal to provide a demultiplexed transmit signal and a demultiplexed supervisory and control signal; a modem including a demodulator configured to receive the demultiplexed monitor and control signals, the demodulator configured to determine a residual frequency error in the demultiplexed monitor and control signals, the monitor and control signals being compensated for delay and Doppler variations; a compensator configured to compensate the demultiplexed transmit signal for the residual frequency error and provide a transmit signal compensated for residual frequency error.

14. In claim 13, The system further comprises a transmit antenna configured to transmit the residual frequency error compensated transmit signal to a user equipment.

15. In claim 14, The system, wherein the transmit antenna comprises a phased array.

16. In any one of claims 13 to 15, The system, wherein the demodulator is configured to determine the residual frequency error by determining a frequency offset relative to the delay and Doppler compensated monitor and control signal carrier signal.

17. In any one of claims 13 to 15, the demodulator is configured to determine the residual frequency error by subtracting an expected frequency of the delay- and Doppler-compensated monitoring and control signals from a received carrier frequency of the delay- and Doppler-compensated monitoring and control signals.

18. In claim 17, The system, wherein the demodulator is configured to determine the received carrier frequency.

19. In any one of claims 13 to 17, The system for communication includes a satellite system.

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