GB2516979A - Predistortion in satellite signal transmission systems - Google Patents

Predistortion in satellite signal transmission systems Download PDF

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Publication number
GB2516979A
GB2516979A GB1314336.7A GB201314336A GB2516979A GB 2516979 A GB2516979 A GB 2516979A GB 201314336 A GB201314336 A GB 201314336A GB 2516979 A GB2516979 A GB 2516979A
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United Kingdom
Prior art keywords
signal
amplifier
envelope
signal transmission
distortion
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Withdrawn
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GB1314336.7A
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GB201314336D0 (en
Inventor
Ahmed Abouelenin
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University of Surrey
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University of Surrey
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Priority to GB1314336.7A priority Critical patent/GB2516979A/en
Publication of GB201314336D0 publication Critical patent/GB201314336D0/en
Priority to US14/910,799 priority patent/US9735857B2/en
Priority to JP2016532736A priority patent/JP6827613B2/en
Priority to PCT/GB2014/052414 priority patent/WO2015019091A1/en
Priority to CA2920801A priority patent/CA2920801C/en
Priority to EP14750615.8A priority patent/EP3031134A1/en
Publication of GB2516979A publication Critical patent/GB2516979A/en
Withdrawn legal-status Critical Current

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Classifications

    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B7/00Radio transmission systems, i.e. using radiation field
    • H04B7/14Relay systems
    • H04B7/15Active relay systems
    • H04B7/185Space-based or airborne stations; Stations for satellite systems
    • H04B7/1851Systems using a satellite or space-based relay
    • H04B7/18513Transmission in a satellite or space-based system
    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03FAMPLIFIERS
    • H03F1/00Details of amplifiers with only discharge tubes, only semiconductor devices or only unspecified devices as amplifying elements
    • H03F1/02Modifications of amplifiers to raise the efficiency, e.g. gliding Class A stages, use of an auxiliary oscillation
    • H03F1/0205Modifications of amplifiers to raise the efficiency, e.g. gliding Class A stages, use of an auxiliary oscillation in transistor amplifiers
    • H03F1/0211Modifications of amplifiers to raise the efficiency, e.g. gliding Class A stages, use of an auxiliary oscillation in transistor amplifiers with control of the supply voltage or current
    • H03F1/0216Continuous control
    • H03F1/0222Continuous control by using a signal derived from the input signal
    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03FAMPLIFIERS
    • H03F1/00Details of amplifiers with only discharge tubes, only semiconductor devices or only unspecified devices as amplifying elements
    • H03F1/32Modifications of amplifiers to reduce non-linear distortion
    • H03F1/3241Modifications of amplifiers to reduce non-linear distortion using predistortion circuits
    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03FAMPLIFIERS
    • H03F1/00Details of amplifiers with only discharge tubes, only semiconductor devices or only unspecified devices as amplifying elements
    • H03F1/32Modifications of amplifiers to reduce non-linear distortion
    • H03F1/3241Modifications of amplifiers to reduce non-linear distortion using predistortion circuits
    • H03F1/3247Modifications of amplifiers to reduce non-linear distortion using predistortion circuits using feedback acting on predistortion circuits
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B1/00Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
    • H04B1/02Transmitters
    • H04B1/04Circuits
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B1/00Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
    • H04B1/62Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission for providing a predistortion of the signal in the transmitter and corresponding correction in the receiver, e.g. for improving the signal/noise ratio
    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03FAMPLIFIERS
    • H03F2200/00Indexing scheme relating to amplifiers
    • H03F2200/451Indexing scheme relating to amplifiers the amplifier being a radio frequency amplifier
    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03FAMPLIFIERS
    • H03F2201/00Indexing scheme relating to details of amplifiers with only discharge tubes, only semiconductor devices or only unspecified devices as amplifying elements covered by H03F1/00
    • H03F2201/32Indexing scheme relating to modifications of amplifiers to reduce non-linear distortion
    • H03F2201/3215To increase the output power or efficiency
    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03FAMPLIFIERS
    • H03F2201/00Indexing scheme relating to details of amplifiers with only discharge tubes, only semiconductor devices or only unspecified devices as amplifying elements covered by H03F1/00
    • H03F2201/32Indexing scheme relating to modifications of amplifiers to reduce non-linear distortion
    • H03F2201/3227Adaptive predistortion based on amplitude, envelope or power level feedback from the output of the main amplifier
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B1/00Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
    • H04B1/02Transmitters
    • H04B1/04Circuits
    • H04B1/0475Circuits with means for limiting noise, interference or distortion
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B1/00Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
    • H04B1/02Transmitters
    • H04B1/04Circuits
    • H04B2001/0408Circuits with power amplifiers
    • H04B2001/0425Circuits with power amplifiers with linearisation using predistortion
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02DCLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
    • Y02D30/00Reducing energy consumption in communication networks
    • Y02D30/70Reducing energy consumption in communication networks in wireless communication networks

Abstract

Digital predistorters DPD1 and DPD2 are used in the main and envelope paths of an envelope tracking transmitter amplifier system. The predistorter DPD2 corrects distortion at the output of the envelope amplifier EA. Envelope tracking of the driver amplifier DA, and load modulation of the power amplifier PA, improves the overall power added efficiency (PAE) when transmitting signals with a high peak to average power ration (PAPR). The power amplifier PA may be bypassed. The transmitter may be used in a satellite or an earth station.

Description

PREDISTORTION IN SATELLITE SIGNAL TRANSMISSION
SYSTEMS
The present invention relates to satellite transmission systems and in S particular to the use of pre-distortion of signals that are to be transmitted by such systems.
In satellite communications, there is an increasing demand to support higher data throughput on necessarily pre-allocated bandwidth channels.
In communication payloads, DC-to-RF power conversion efficiency is an important consideration and most of the DC power is consumed by the RE Power Amplifier (PA). The maximization of PA efficiency while maintaining low distortion is a key objective. Both power and bandwidth cfficicncy can be increased by employing digital pre-distortion (DPD).
In future satellite communications links, a huge amount of data has to be transmitted due to the increase in the accuracy of the payload, number of subscribers or the need for transmission of a large volume of data within a limited period of time (maximum visibility). This could be achieved by employing a spectrally efficient modulation technique (SEMT), e.g. M-ary QAM (Quadrature amplitude modulation), which necessarily has a non-constant envelope with increased information carrying ability per unit bandwidth. However, this leads to very high constraints on the linearity of the transmitter power amplifier (PA).
Linear PAs, although suitable for SEMTs, are the main source of power consumption in the transmitter. Their use results in low overall transmitter efficiency due to the wasted power as a heat which necessarily requires thermal management. In contrast, a high efficiency PA is rather a complex nonlinear system (e.g. switch), and is not suitable for transmission of SEMTs.
On the one hand, due to variations in the amplitude of generated SEMT and saturated (i.e. power efficient) PA nonhinearities the transmitted SEMT occupies larger bandwidth (i.e. spectral regrowth) and results in out-of-band distortion that disturbs the adjacent channels. This may cause noncompliance to relevant regulatory standards (e.g. International Telecommunications Union ITU) and may violate a predefined spectral mask constraint. On the other hand, SEMTs have a weak tolerance to amplitude disturbances that occur in the nonlinear amplification process since its information carrying ability depends on the signal amplitude.
This may cause in-band distortion in the transmitted signal (i.e. error vector magnitude EVM) which consequently deteriorates the receiver performance in terms of bit error rate (BER). In addition, the overall transmitter powcr cfficicncy significantly detcrioratcs if a high peak-to-averagc power ratio (PAPR) signal is uscd whcrc morc powcr back-off is required. Therefore, high efficiency PAs should be used which, unfortunately, suffer from strong nonlinearities.
High efficiency PAs show a dynamic nonlinear behaviour, including memory effects if a wideband fast varying envelope signal is used. In this case, the amplified signal depends on the current and past input symbols.
To satisfy PA linearity requircments as well as to improve overall system efficiency, it is necessary to undertake some linearization.
Traditionally, PA static nonlinearity has been mitigated by compromising the PA DC-to-RF power conversion efficiency where output power back-off is required. However, power backing-off is not suitable for battery operated (on-board payload) or high running costs (ground segment) systems. Moreover, power back-off cannot cope with distortion due to memory effects, hence the need for a linearization approach that achieves low in-band and out-of-band distortion and high power efficiency simultaneously. Several linearization techniques, which are analog in essence, have been proposed to cope with the PA nonlinear behaviour (e.g. Feedforward, RF predistortion and LINC). However, digital predistortion DPD has shown a good simultaneous efficiency and linearity improvements for a transmitter. In addition, DPD is implemented in an FPGA (field programmable gate array) or ASIC (application specific integrated circuit), and is thus immune to the components' tolerance or aging.
The present invention provides a signal transmission system for a satellite which may comprise means for producing a signal to be transmitted. A first signal channel can be provided which includes a digital pre-distortion device for applying pre-distortion to the signal.
Further, a sccond signal channel can be providcd for processing an cnvclopc of thc signal. Thc sccond signal channel can include a second digital pre-distortion device for applying pre-distortion to the envelope of the signal. The system can include output means for transmitting the signal, such as an antenna.
Advantageously, a DPD system architecture is thus proposed where envelope tracking (ET) of the driver amplifier (DA) and load modulation of the PA are used to maximize the overall PAE (power added efficiency) while high PAPR (peak to average power ratio) signals can be used.
The invention also provides a method of transmitting a signal comprising producing a signal to be transmittcd and applying a first prc-distortion to the signal. The prc-distortcd signal can then be amplified using a first amplifier. A band-limited envelope of the signal may be isolated through a second channel in which a second pre-distortion can be applied to the envelope. The distorted envelope signal can be used to control the first amplifier. An output signal can then be transmitted from the first amplifier using an antenna.
There follows a detailed description of embodiments of the invention by way of example only and with reference to the accompanying drawings in which Figure 1 is a schematic representation of the effects of digital pre-distortion; Figure 2 is a schematic representation showing the behaviour of a typical PA; Figure 3 is a schematic representation of a system in accordance with a first embodiment of the invention; Figure 4 is a schematic representation of a system in accordance with a sceond cmbodiment of thc invcntion; Figure 5 is a schematic rcprcscntation of a systcm for tcsting a DPD device; and Figures 6 to 9 show spectra produced by systems according to the invcntion.
By way of further background explanation of the principles behind the invention, Figure 1 includes three schematic graphs showing how the DPD can offset the non-linearity of the PA. The DPD has a linearization effect on the PA output. In small fractional bandwidth systems, it is not feasiblc to filtcr out out-of-band spectral rcgrowth due to the required high-Q filter. PA DPD-based linearization is achieved by digitally processing in-phase (I) and quadrature (Q) baseband data so that frequency components are generated within a bandwidth equal to that of the spectral regrowth (normally 5 times the modulated signal bandwidth) to compensate for the distortion due to PA nonlinearities. Thus, a wideband transmitter should be used. This digital "pre-processing" allows the PA to be operated up to saturation point and mitigates the in-band and out-of-band distortions due to nonlinear behaviour. 1-lence, output power back-off can be significantly reduced.
As shown in Figure 2, power back-off techniques can also be used to help achieve linearity in the output of the PA and to cope with signals having a high peak to average power ratio. To maintain linear amplification for high PAPR signals using linear PAs, two power back-offs can be utilised; the first to avoid the nonlinear part of the gain curve and the second which is to deal with the PAPR. Even if DPD is used to alleviate the 1st back-off, either supply or load modulation could only mitigate the 2nd back-off to achieve acceptable overall power added efficiency (PAE).
Figure 5 shows a block diagram for a typical DPD+PA hardware test sctup. This sctup is for implemcnting a method of modelling thc rcsponse of a transmission system that utilises DPD using a model coefficient extraction procedure. I and Q data of a test signal can be generated on a PC using Matlab then downloaded on an arbitrary waveform generator (AWG). These data modulate an RF carrier in a Vector Signal Generator (VSG) where signal upconvcrsion is achieved.
The modulated RF carrier feeds the PA and a driver amplifier (DA) may be used for high power PAs (HPA). A Vector Signal Analyzer (VSA) downeonverts then demodulates the RE modulated carrier. This allows extraction of the DPD model coefficients (in the PC) by comparing the demodulated I and Q data of the original (PA is removed) and distorted signal (i.e. signal as amplified by the PA). The DPD+PA performance can be verified by downloading the predistorter I and Q data on the AWG and measuring the PA output.
Future high throughput satellites, where a large fractional bandwidth is expected, could benefit from adopting band-limited-DPD. These benefits, compared to using a conventional DPD, could be: less hardware complexity and less processing power as a result of processing a bandwidth comparable to the original modulated signal bandwidth compared to 5 times bandwidth in conventional DPD.
Figure 3 shows a first embodiment of the signal transmission system 30.
The system 30 comprises means 31 for producing a signal that is desired to be transmitted by a satellite, eg a film or television program, and a means 34 for transmitting an amplified output signal, such as an antenna 34. A first channel 37 or electrical path of the system leads from the signal production means 31 to the antenna 34, via a first digital pre-distortion device 32 and an amplifier 33 to the antenna 34. The first digital pre-distortion device 32 produces a non-linearity in the signal that cancels out the non-linearity produced by the amplifier 33. A second channel 38 or electrical path is able to isolate an envelope of the signal.
Thc second channel includes a second digital pre-distortion device 35 which is connected to an envelope amplifier for amplifying the envelope signal. The second digital pre-distortion device 35 applies a non-linearity to the envelope signal that is cancelled out by the non-linearity of the envelope amplifier.
Figure 4 shows a more detailed version of the embodiment of the invention shown in Figure 3. The varactor-based matching network is modulating the output matching network based on the input modulated signal. The DPD+PA architecture shown in Figure 3 advantageously increases the overall average power added efficiency of the system while minimizing the distortion in the driver amplifier (DA) stage. Load modulation is applied at the PA output using a varactors-based matching network where varaetors can be placed in parallel to cope with high PA output power. The matching network can also be connected to an antenna for transmitting the output amplified signal. The bandwidth through path DPDI, upeonverter, DA, and PA is limited to the original modulated signal bandwidth. Envelope tracking is applied to the driver amplifier using an envelope amplifier (EA) with additional DPD block (DPD2) to compensate for nonlinearities at EA output. Switching between the DA and PA is possible for low input power which further improves the average power added efficiency.
Figure 6 shows a spectrum produced by a DPD modelling process, in particular, a NARMA-based (non-linear auto-regressive moving average) DPD model for 1GHz 1024-QAM ultra wideband signal modulated on a 4GHz carrier using MGA-545P8 PA model on Agilent ADS© software.
Three iterations are done to attain further adjacent channel power ratio (ACPR) improvement. Figure 6 shows the original signal spectrum (61), PA distorted output (62), and DPD+PA output for the three iteration (63, 64 and 65). The vertical and horizontal axes are set to 0 to -110 dBm and 1 to 7 GHz, rcspcctivcly. Approximatcly 12 dB improvcmcnt in ACPR is achieved while -23dB NMSE is maintained.
Figures 7 to 9 show spectra produced in a test setup as follows: A dcmonstration low noise amplificr (ZFL-SOOLN+ Mini-Circuits©) was used to demonstrate the effect of band limited DPD on the DPD+PA performance. The following equipment was used: Agilent© N5182B MXG RF Vector Signal Generator (VSG), Agilent© N9030A PXA Vector Signal Analyser (VSA), and a TTi EL3O2Tv triple power supply. The VSG and YSA are connected through a network switch for control and data exchange via a PC. Synchronization is cstablishcd by connccting a MHz reference, trigger, and event ports. Figure 7 to Figure 9 show the measured spectra of original signal, distorted PA output, and NARMA based DPD+PA for thrcc diffcrdllt modulatcd tcst signals: Figure 7: 10MHz LTE DL (QPSK) Figurc 8: 32 MHz 1024-QAM Figure 9: 50 MHz 1024-QAM The spectra shown in Figures 7 to 9 are each normalised to the level of the original signal to facilitate comparison of the signals. In Figure 7, line 71 represents the original signal, line 73 represents the amplified signal without DPD, and line 72 represents the signal as amplified and pre-distorted. In Figure 8, line 81 represents the original signal, line 83 represents the amplified signal without DPD, and line 82 represents the signal as amplified and pre-distorted. In Figure 9, line 91 represents the original signal, line 93 represents the amplified signal without DPD, and line 92 represents the signal as amplified and pre-distorted.
The adjacent channel power ratio (ACPR) and normalised mean square error (NMSE) for DPD+PA were measured for each modulated signal and are summarized in Table 1. It is to be noted that a good NMSE could be achieved in all cases while a good ACPR is achieved only for the 10 MHz BW signal. This is justified as follows; due to the limited analysis bandwidth at the PA output, i.e. 60 MHz, no sufficient information about the spectral regrowth arrives to the DPD. Thus, the ACPR gets worse as the signal bandwidth becomes larger. However, DPD still copes with the in-band distortion.
Table 1:
Measured ACPR and NMSE for DPD-{-PA ACPR (dB) NMSE (dB) MHz LTE DL -25 -36 32MHz 1024 QAM -10 -33.54 MHz 1024 QAM -4 -33.52 The data thus indicate a most optimal performance for the 10MHz LTE DL signal Spectral re-growth can be filtered out for large fractional bandwidth signals (e.g. in L-Band) and for this reason, the ACPR constraint is significantly relaxed. To allow reliable reception of the transmitted signal ovcr a satcllitc communication link a link budgct-dctcrmined ratio of the signal energy over the spectral noise density, i.e. Es/No, has to be maintained at the receiver side assuming perfect signal transmission.
EVM at the transmitter side decreases this ratio and has to be kept at minimum by employing DPD.
As a result of the heritage in space technology, nonlinear (switch) PAs, although power efficient, are not commonly used whereas linear PAs (powerinefficient) are used. Thus high spectral density modulation techniques are avoided. An advantage of the prcscnt invention is that using DPD plus load and supply modulation Oil space (aild ground) segments guarantees efficient usage of power. Moreover, a greater amount of data can be pushed into the link assuming the same power budgct for a transmittcr.
The figure of merit for the proposed DPD+PA should be achieving a lower EYM and high throughput with fixing the power consumption.
It is possible to use a training sequence to update the DPD model: in X-band payloads, the transmitter is on for a short period of timc to transfer data when the satellite is in the visibility zone of the station. However, this does not necessarily happen for each orbit. Consequently, one of the orbits can be freed to transmit a training sequence to the data reception station. This receivcd data could be comparcd, offlinc, to the idcal training sequence and an update for the DPD model coefficient could be extracted. This updated coefficient could be transmitted to the satellite through the TT&C transponder and used to configure the DPD model onboard. In other words, an offline adaptation could be made to cope with any unexpected very slow time variation of the PA.
DPD techniques for terrestrial communications as proposed ill the present invention advantageously maximize the overall PAE while high PAPR signals can be used. A further advantage of embodiments of the present invention is that it allows less expensive (in terms of volume, mass, and cost) space and ground segment transmitters.

Claims (14)

  1. CLAIMS1. A signal transmission systcm for a satellitc comprising: S means for producing a signal to be transmitted; a first signal channel which includes a digital pre-distortion device for applying pre-distortion to the signal; a second signal channel for processing an envelope of the signal, which includes a second digital pre-distortion device for applying pre-distortion to the envelope of the signal; and output means for transmitting the signal.
  2. 2. A signal transmission system according to claim 1, wherein the second channel is connected in parallel to the first channel.
  3. 3. A signal transmission system according to claim I or 2, wherein the first channel includes a driver amplifier and a power amplifier.
  4. 4. A signal transmission system according to claim 3, wherein the power amplifier can be switched off when low power output is required.
  5. S. A signal transmission system according to claim 2, wherein the second channel includes an envelope amplifier, whose output is connected to the driver amplifier and controls the power supply to the driver amplifier.
  6. 6. A signal transmission system according to any of the preceding claims, wherein the output means comprises an antenna.
  7. 7. A signal transmission system according to any of the preceding claims, further comprising means for modulating the power output by the output means.
  8. 8. A signal transmission system according to claim 6 or 7, further comprising a matching network for modulating a load on the antenna.
  9. 9. A signal transmission system according to claim 8, wherein the matching network comprises one or more varactors.
  10. 10. A method of transmitting a signal comprising: producing a signal to be transmitted; applying a first pre-distortion to the signal and amplifying the distorted signal using a first amplifier; isolating a band-limited envelope of the signal and applying a second prc-distortion to the envelope; using the distorted envelope signal to control the first amplifier; transmitting the output from the first amplifier using an antenna.
  11. 11. A method of transmitting a signal according to claim 10, wherein the envelope signal is amplified using an envelope amplifier.
  12. 12. A method of transmitting a signal according to claim 10 or 11, further comprising modulating an output load of the system.
  13. 13. A signal transmission system substantially as herein described with reference to the accompanying drawings.
  14. 14. A method of transmitting a signal substantially as herein described with reference to the accompanying drawings.
GB1314336.7A 2013-08-09 2013-08-09 Predistortion in satellite signal transmission systems Withdrawn GB2516979A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
GB1314336.7A GB2516979A (en) 2013-08-09 2013-08-09 Predistortion in satellite signal transmission systems
US14/910,799 US9735857B2 (en) 2013-08-09 2014-08-06 Predistortion in satellite signal transmission systems
JP2016532736A JP6827613B2 (en) 2013-08-09 2014-08-06 Pre-distortion in satellite signal transmission systems
PCT/GB2014/052414 WO2015019091A1 (en) 2013-08-09 2014-08-06 Predistortion in satellite signal transmission systems
CA2920801A CA2920801C (en) 2013-08-09 2014-08-06 Predistortion in satellite signal transmission systems
EP14750615.8A EP3031134A1 (en) 2013-08-09 2014-08-06 Predistortion in satellite signal transmission systems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1314336.7A GB2516979A (en) 2013-08-09 2013-08-09 Predistortion in satellite signal transmission systems

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GB201314336D0 GB201314336D0 (en) 2013-09-25
GB2516979A true GB2516979A (en) 2015-02-11

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GB1314336.7A Withdrawn GB2516979A (en) 2013-08-09 2013-08-09 Predistortion in satellite signal transmission systems

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US (1) US9735857B2 (en)
EP (1) EP3031134A1 (en)
JP (1) JP6827613B2 (en)
CA (1) CA2920801C (en)
GB (1) GB2516979A (en)
WO (1) WO2015019091A1 (en)

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