EP4616530A1 - Transmitter signal processor - Google Patents

Transmitter signal processor

Info

Publication number
EP4616530A1
EP4616530A1 EP23805491.0A EP23805491A EP4616530A1 EP 4616530 A1 EP4616530 A1 EP 4616530A1 EP 23805491 A EP23805491 A EP 23805491A EP 4616530 A1 EP4616530 A1 EP 4616530A1
Authority
EP
European Patent Office
Prior art keywords
signal
input
output
transmitter
sum
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
EP23805491.0A
Other languages
German (de)
French (fr)
Inventor
Malcolm David Macleod
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Qinetiq Ltd
Original Assignee
Qinetiq Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Qinetiq Ltd filed Critical Qinetiq Ltd
Publication of EP4616530A1 publication Critical patent/EP4616530A1/en
Pending legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03FAMPLIFIERS
    • H03F3/00Amplifiers with only discharge tubes or only semiconductor devices as amplifying elements
    • H03F3/20Power amplifiers, e.g. Class B amplifiers, Class C amplifiers
    • H03F3/24Power amplifiers, e.g. Class B amplifiers, Class C amplifiers of transmitter output stages
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/02Details of the space or ground control segments
    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03FAMPLIFIERS
    • H03F1/00Details of amplifiers with only discharge tubes, only semiconductor devices or only unspecified devices as amplifying elements
    • H03F1/34Negative-feedback-circuit arrangements with or without positive feedback
    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03FAMPLIFIERS
    • H03F3/00Amplifiers with only discharge tubes or only semiconductor devices as amplifying elements
    • H03F3/189High-frequency amplifiers, e.g. radio frequency amplifiers
    • 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
    • H03F2201/3206Multiple channels are combined and amplified by only one 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
    • H04B2001/0408Circuits with power amplifiers
    • H04B2001/0416Circuits with power amplifiers having gain or transmission power control
    • 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
    • H04B2001/0433Circuits with power amplifiers with linearisation using feedback

Definitions

  • the present invention relates to electronic amplifiers, and more particularly amplifiers used to amplify signals for transmission, where a plurality of signals are required to be transmitted together in an efficient manner.
  • amplifiers are used in applications where the power efficiency of the amplifier is critical.
  • One such application is in satellite systems, where there is often a very limited power budget available to supply all the electronic systems on board.
  • the power supply which generally comprises solar panels
  • the power supply cost a lot of money, but as a result of increased size and weight it adversely affects satellite performance in many ways, such as launch rocket size, manoeuvrability, vulnerability to damage etc.
  • dissipating waste heat which results from amplifier inefficiency is a serious challenge for a satellite in space, again resulting in extra cost and weight.
  • GNSSs Global navigation satellite systems
  • GPS Global Positioning System
  • European Galileo system European Galileo system
  • Beidou systems each comprise of a number of satellites (typically 15-30) in orbit around the earth.
  • the trend in modern GNSS is to transmit a greater number of signals from one satellite.
  • These signals may support multiple different GNSS “services” with, for the purposes of this application, each service being associated with one or more signals.
  • Each of the individual signals may be a constant envelope signal, but it is very difficult to maintain a constant envelope when the signals are combined together, particularly where the combined signal is subsequently filtered.
  • the result can be the production of undesired intermodulation signals which are wasteful of energy, compared to the ideal solution of producing a combined signal of constant envelope that can then be fed into a constant envelope amplifier.
  • One way of processing the multiple signals in a satellite signal transmitter is to use a separate transmit amplifier for each one, with each signal being a constant envelope signal, for maximum efficiency, and then combining these amplified signals before sending them to a transmit antenna. This therefore provides Constant Envelope High Power Amplification.
  • the step of combining the high power signals for transmission through one antenna is an engineering challenge, and overall this solution has size, cost and weight penalties.
  • a constant envelope signal is one where the amplitude of the signal is not modulated. It may synonymously be known as a constant amplitude signal.
  • PCET Phase Optimised Constant Envelope Transmission
  • a transmitter having a transmitter signal processor (TSP) for processing a plurality of signals for transmission to produce an output signal of constant envelope, the transmitter signal processor having a sum input comprising a sum of the plurality of signals for transmission, and further inputs comprising of each signal for transmission, and an output, the TSP being arranged to compute an error signal between the sum input and the output of the TSP, and for each input signal, to model the effect of the error in a receiver by correlating the error signal with the input signal and to use the sum of the effects for each input signal to generate a correction signal that is fed back, in a feedback loop, to an input of the TSP.
  • TSP transmitter signal processor
  • Embodiments of the invention thus employ a feedback approach to ameliorating distortion caused by the amplification of multiple signals where a constant envelope is desired.
  • Some embodiments of the invention may comprise a transmitter wherein the feedback loop generates a combined feedback signal that is subtracted from the sum input to produce a “constant envelope input signal”, the feedback loop comprising, for each input signal, a) a correlator arranged to generate a correlation between (i) said input signal and (ii) an error signal comprising a measurement of a difference between the sum input and an output of a constant envelope process or within the TSP; and b) a multiplier arranged to multiply the result of the correlation at step (a) with said input signal, to produce a multiplier output; the signal processor being further arranged to sum the output of the multiplier at step (b) for each input signal to produce a combined feedback signal and to feed back the combined feedback signal to the sum input of the signal processor wherein the constant envelope process comprises either of a normalisation function, or an analogue signal processing chain or a digital model thereof.
  • Embodiments may provide a transmitter that is able to process multiple (e.g. 2, 3, 4, 5 or more inputs) digital input signals for transmission, generating an output signal for transmission that has a substantially constant envelope.
  • multiple e.g. 2, 3, 4, 5 or more inputs
  • the correlator at (a), is carrying out a similar process to that which would occur in a receiver of the signal transmitted by the transmitter.
  • the sum input signal of (a) is of similar form to that of a reference signal used in a correlator in a well-designed receiver, and the transmitted signal is (in part) that received at the receiver.
  • the output of the correlator therefore gives a representation as to the effects of distortion caused by the constant envelope process, as it would be seen at a receiver.
  • This correlator output is, at (b), multiplied by the input signal to form (along with contributions from similar signals produced for each of the other input signals) the combined feedback signal that is subtracted from the sum input signal to the TSP.
  • the output signal may in some embodiments be a digital signal that is then converted to an analogue signal in a digital to analogue converter (DAC), and amplified and, if necessary, up-converted in frequency before being transmitted.
  • DAC digital to analogue converter
  • the constant envelope process comprises an analogue signal processing chain having at least one of an amplifier or a frequency up-converter, or comprising a digital model thereof.
  • the feedback loop further comprises a digital to analogue converter, along with a frequency down-converter where an up-converter is present in the constant envelope process.
  • the processing within the TSP occurs entirely within the digital domain
  • the correlator comprises a multiplier arranged to multiply the complex conjugate of signal (i) with signal (ii), and to accumulate the result in an accumulator.
  • a high pass filter may be included in the correlator between the multiplier and the accumulator, to remove a low frequency component from an output of the multiplier. This prevents any such low frequency components (including DC, or near-DC signals) from accumulating and causing errors.
  • the transmitter may further include scaling means for scaling the input signals prior to their being summed at the sum input.
  • the scaling means may comprise one or more multipliers.
  • the multi plier(s) may preferably be implemented digitally.
  • the multipliers may be arranged to scale each input signal independently.
  • the scaling provided by the scaling means may be adjustable in operation of the TSP. The adjustment to the scaling may be determined by measurement of a DC component removed by the high pass filter.
  • a method of combining a plurality of digital input signals for transmission by a transmitter the method acting to produce an output signal of constant envelope, and the transmitter having a transmitter signal processor (TSP) configured to sum the digital inputs to produce a sum input, and to compute an error signal between the sum input and the output of the TSP, and to, for each digital input signal, model the effect of the error as would occur in a receiver by correlating the error signal with the digital input signal, and to use the sum of the modelled effects for each digital input signal to generate a correction signal, and to feed back the correction signal, in a feedback loop, and to subtract the feedback signal from the sum input of the TSP.
  • TSP transmitter signal processor
  • the method may further comprise a method wherein the sum signal is fed into a constant envelope processor in the TSP that comprises at least a normalisation function or an analogue signal processing chain, or a digital model thereof, and which produces an output; wherein the feedback signal is produced by the following steps: i) measuring an instantaneous error signal by taking the difference between the sum input and the output; ii) for each input signal, modelling the effect of the instantaneous error signal, by correlating the instantaneous error signal with the input signal, and multiplying the output of the correlation with the input signal; iii) summing the results of the multiplication in step (ii) produced for each input signal, with the result of this summation comprising the feedback signal; wherein the constant envelope process comprises either of a normalisation function, or an analogue signal processing chain.
  • the constant envelope processor may be arranged to normalise, using a normaliser, the constant envelope input signal.
  • the constant envelope process comprises a digital to analogue converter, and at least one of a frequency upconverter and an RF amplifier, and wherein the output for the purposes of (i) of this second aspect is derived from a downconverted and digitised version of an output from the RF amplifier and/or upconverter.
  • the constant envelope process comprises a digital model of at least a part of an analogue processing chain, including at least a power amplifier, of a transmitter in which the method is implemented.
  • the digital model may have inputs from the analogue processing chain, and may be adapted to change parameters of the digital model based upon these inputs.
  • Figure 1 shows a high level representation of a transmitter arranged to transmit multiple independent signals through a common up-conversion and amplification process
  • Figure 2 shows a high level representation of a prior art process for achieving a constant envelope output signal
  • Figure 3 shows a high level representation of an improved prior art process for achieving a constant envelope output signal
  • Figure 4 shows a high level architecture of an embodiment of the present invention
  • Figure 5 shows a more detailed architecture of an embodiment of the present invention, operable completely in the digital domain
  • Figure 6 shows partial detail of an alternative embodiment of the present invention, where some elements are operable in the analogue domain; and Figure 7 shows partial detail of an alternative embodiment of the present invention, where a digital model of analogue components are used.
  • Figure 1 shows a simple transmitter architecture 100, where three independent digital input signals Si(t)- S3(t) are scaled in multipliers ai -a 3 before being summed in summer 102 to produce a combined digital signal w(t). This is then converted to analogue form in digital-to- analogue converter (DAC) 104 before being up-converted by mixing with a local oscillator signal (not shown) in mixer 106, and amplified in amplifier 108. It is then fed to an antenna (not shown) for transmission.
  • DAC digital-to- analogue converter
  • a typical application may comprise a GNSS satellite, and the signals s,(t) may comprise different navigation signals, such as an open navigation signal, along with commercial, public regulated service, and safety of life navigation signals, and pilot signals, which may be at different frequencies, bandwidths or phases to each other.
  • different navigation signals such as an open navigation signal, along with commercial, public regulated service, and safety of life navigation signals, and pilot signals, which may be at different frequencies, bandwidths or phases to each other.
  • the signal w(t) is the wanted signal for transmission.
  • the envelope of w(t) can vary, for example as each signal itself varies in amplitude or phase.
  • the variation of the envelope of w(t) leads to inefficiencies, particularly within the RF amplifier, such as the generation of intermodulation signals as mentioned earlier which, when the amplifier is in a challenging environment such as a satellite, can be costly in terms of additional cooling requirements, or excess power input required to achieve a given performance.
  • Figure 2 shows a simple prior art technique 200 for generating a constant envelope signal. It is similar to the architecture of Figure 1 , but with the addition of new blocks in the signal path between the summer 102 and the DAC 104.
  • CE constant envelope
  • Measurement of the error produced by the approach can be done by subtraction, in subtractor 202 of the output signal of the CE block from the input signal, to produce instantaneous error signal eo(t).
  • the power of the error eo(t) would generally be minimised by design by adjusting the scaling factor %, such that the mean squared value of w(t) equals the mean squared value of o(t), which is p 2 .
  • FIG. 3 An improved prior art technique 300 is shown in Figure 3. This is the technique used by prior art document US8774315 which, as stated above, uses precomputed tables to generate an output signal, based upon the individual input signals as presented to the CE component by the dotted line connections 302. These tables take possible combinations of input signals, such as a discrete number of different phases for each (for phase modulated signals), and precompute an ideal output signal for each possible input combination.
  • Figure 4 shows at a top level a system 400 according to an embodiment of the present invention.
  • the basic principle of this embodiment, and all embodiments of the invention, is the use of negative feedback of the error signal e 0 (t) to correct for errors introduced by the constant envelope process.
  • the error signal e 0 (t) is equivalent to the error signal as shown in Figure 2, but in this embodiment the error signal is used as explained below, to produce the feedback signal.
  • Signals Si(t)- S3(t) are the input signals which need to be combined, and transmitted from a power amplifier. They are scaled by corresponding scaling factors ai- 03 and summed in summer 402, providing a summation output.
  • a further combined scaling may be performed on the summation output at 404, or alternatively this scaling may be done by incorporating an appropriate common factor to the individual scaling factors 01-03.
  • the output of this is signal wi(t), which provides a first input to a summation node 406, to calculate the error signal e 0 (t).
  • the instantaneous error caused by the conversion to constant envelope (CE) is thus computed.
  • Signal wi(t) is also provided to a further summation node 408 in the transmit path at which point a feedback signal is subtracted from it to produce signal w 2 (t)
  • the signal o(t) is fed to the summation node 406 as its second input, where it is subtracted from signal wi(t) to produce e 0 (t).
  • Signal o(t)) is the constant envelope (digital) signal in this embodiment, which is then converted to an analogue signal and up- converted in frequency and amplified in a power amplifier for transmission, as required.
  • the feedback signal is produced by taking the error signal and, for each individual input signal Si(t), applying it to a correlator 410 that correlates it with s,(t) to model the effect that the error has on a correlation process that would happen in a receiver, which of course has (in GNSS and other Direct Sequence Spread Spectrum applications), its own locally stored reference copy of signal Si(t).
  • Figure 4 only shows the correlation and feedback process associated with signal Si(t), and in practice each signal s,(t) will have its own correlator to provide its own contribution to the feedback signal as is explained later.
  • the correlator output is then multiplied by the signal s,(t) in multiplier 412 to become si(t)’s contribution to the feedback correction signal.
  • the corrections themselves, due to their being subtracted from signal wi(t), are distorted by the CE process, but the continuous negative feedback still reduces the cumulative error effect.
  • FIG. 5 shows in more detail the generation of the feedback signal.
  • the embodiment 500 shown is the same as that of Figure 4, but with additional elements shown that further clarify the operation of the system.
  • Like reference numbers indicate like functional blocks.
  • the instantaneous transmitter error e 0 (t) is computed, and correlated with each reference signal. This is only shown for signal si(t) in the figure; the processing for the other signals uses duplicated blocks.
  • Arrow 502 indicates, for example, a feed to correlators for the other signals s t (t) and arrow 504 indicates the summation of the results of the processing of those signals to create the overall feedback signal.
  • the correlator 410 comprises a conjugator 506 for conjugating the reference signal before it is multiplied by the error signal in multiplier 508. It is then accumulated in accumulator 510 to produce, error signal ei(t).
  • the distorting operation of the CE block means that the corrections are also distorted, so the level of correction actually achieved on the next sample is reduced. However, a significant degree of correction does survive the CE block, and modelled performance better than the prior art techniques has been achieved.
  • the above embodiments all operate in the digital domain throughout, in that all the processing, and the CE process also, operate in this domain, and provides its output to a DAC which then feeds any required up-conversion and amplification for transmission.
  • Other embodiments may use a CE process that operates at least in part in the analogue domain, with a feedback path coming from an element within the analogue path, typically after an amplification stage. This allows imperfections within the amplifier to be directly taken into account by the processing occurring in the feedback path. These imperfections may include any soft-clipping that occur in the amplifier, and/or any AM to AM, and AM to PM distortion that may occur, where AM is amplitude modulation, and PM is phase modulation.
  • Figure 6 shows in top level form part 600 of an embodiment of the invention that has the CE process in analogue form, this comprising part of the transmit chain of a transmitter. Note that the details of the feedback processing are the same as that for the embodiments above, and will not be described in detail further in relation to this figure.
  • this figure just shows the analogue equivalent of the (digital) CE block in figure 5, along with the error summer 406.
  • the connections to the summer 406 from w-i(t) and o(t), along with the output from summer 406 show the paths to the feedback circuit, this comprising e.g. the feedback circuit as explained in relation to Figure 4.
  • the signal wi(t) is presented to a DAC and the resulting analogue signal is up- converted to the transmit frequency in up-conversion mixer 604, before being passed to an RF amplifier 606 for amplification to a desired transmit output power, to produce an analogue power signal 608 for subsequent transmission via an antenna.
  • a coupler 610 takes a small amount of this transmit energy from the output of the RF amplifier, and brings it back to a baseband signal in downconversion mixer 612, and converts this back to a digital signal in analogue to digital converter 614. It is then fed to the feedback loop to generate the error signal e 0 (t) as for previous embodiments.
  • this embodiment may introduce a small delay in the signal path.
  • the signals s t (t) comprise a sequence of chips
  • any added delay is small compared to one chip duration (which, in the higher GNSS chip rates is about 0.1 ps) this delay can be ignored without any significant problem occurring.
  • the delay is measured at the design and test stage of system production. Then that amount of delay is inserted into the digital correction circuits, at the conjugate box 506 in Figure 5 (albeit that is shown in an all- digital scenario, but the feedback signal generation will be the same in this embodiment as previously stated).
  • FIG. 6 A further potential issue with the embodiment of Figure 6 is that the RF measurement process, of splitting a signal from an output of the amplifier (in coupler 610), downconverting it in frequency and converting it to digital form may introduce noise.
  • Figure 7 shows an alternative embodiment that aims to reduce the effects of any such noise that may be present.
  • This embodiment has similarities to that of Figure 6, in that an output of an analogue transmit chain is used to influence the feedback process.
  • the analogue transmit chain, and the coupler, down-converter and digitiser are similar to that shown in Figure 6, and hence has the same reference numbers.
  • the digitiser 614 output is not directly used, but is instead fed to a digital amplifier model 616.
  • This digital amplifier model is a model of the RF amplifier.
  • the adjustable parameters may take the form of an input-envelope to output-envelope mapping function and an input-envelope to output-phase-error mapping function. Alternatively they may be the parameters of a Volterra function model of the power amplifier. Such models are mentioned in “The Evolution of PA Linearization” by Allen Katz, John Wood, and Daniel Chokola, IEEE Microwave Magazine, Feb 2016, p. 32.
  • This embodiment provides the advantage that any noise or error in the coupled output (o(t) is not fed directly into the feedback process described earlier, but is smoothed by the long term adaptation within the model.
  • the model itself being digital, operates with low output noise.
  • Embodiments of the invention will typically be implemented in software, for example in one or more digital signal processors or microprocessors - the processor or processors being programmable hardware controlled by computer code, or may be operated in firmware/hardware, such as in one or more Application Specific Integrated Circuits (ASIC), or a Field Programmable Gate Arrays (FPGA).
  • ASIC Application Specific Integrated Circuit
  • FPGA Field Programmable Gate Arrays
  • Such devices will typically include, or be connected with, a suitable memory and storage, as would be appreciated by a normally skilled person.
  • the invention may extend therefore to a software program arranged to be storable in computer memory and comprising of instructions that cause a processor to implement the various elements described herein.
  • the transmitter signal processor may comprise a combination of analogue and digital circuitry arranged to process signals in both the analogue and digital domains.
  • analogue circuitry forming part of the transmitter signal processor may comprise of one or more amplifiers (including power amplifiers), frequency shifters, filters etc. that form part of a signal processing chain of a signal to be transmitted by an antenna.
  • Embodiments of the invention have utility in many areas of signal transmission, typically in space or airborne application, such as in GNSS satellites, and may also be used more widely for terrestrial radio receivers (where increased power efficiency gives longer battery life and reduced waste heat).

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Transmitters (AREA)
  • Amplifiers (AREA)
  • Complex Calculations (AREA)
  • Feedback Control In General (AREA)

Abstract

A transmitter signal processor (TSP) for use where multiple independent signals are to be combined, amplified and transmitted whilst maintaining a substantially constant envelope, the processor comprising a feedback network, whereby an error signal between a sum of the signals and an output of a constant envelope process within the TSP is computed, and, for each input signal this error signal correlated with the input signal to model the effect of the error in a receiver, and to produce a feedback signal by multiplying each error signal by its corresponding input signal, and summing the result for each such input signal, and then subtracting the feedback signal from the sum input. The constant envelope process may be all-digital, such as a normalisation process, and/or may comprise a part of the analogue transmit chain, such as amplifiers, frequency convertors or filters.

Description

Transmitter Signal processor
The present invention relates to electronic amplifiers, and more particularly amplifiers used to amplify signals for transmission, where a plurality of signals are required to be transmitted together in an efficient manner.
Often amplifiers are used in applications where the power efficiency of the amplifier is critical. One such application is in satellite systems, where there is often a very limited power budget available to supply all the electronic systems on board. Not only does the power supply (which generally comprises solar panels) cost a lot of money, but as a result of increased size and weight it adversely affects satellite performance in many ways, such as launch rocket size, manoeuvrability, vulnerability to damage etc. Furthermore, dissipating waste heat which results from amplifier inefficiency is a serious challenge for a satellite in space, again resulting in extra cost and weight.
Global navigation satellite systems (GNSSs), such as the US Global Positioning System (GPS), the European Galileo system, or the Chinese Beidou systems each comprise of a number of satellites (typically 15-30) in orbit around the earth. The trend in modern GNSS is to transmit a greater number of signals from one satellite. These signals may support multiple different GNSS “services” with, for the purposes of this application, each service being associated with one or more signals.
Each of the individual signals may be a constant envelope signal, but it is very difficult to maintain a constant envelope when the signals are combined together, particularly where the combined signal is subsequently filtered. The result can be the production of undesired intermodulation signals which are wasteful of energy, compared to the ideal solution of producing a combined signal of constant envelope that can then be fed into a constant envelope amplifier.
One way of processing the multiple signals in a satellite signal transmitter is to use a separate transmit amplifier for each one, with each signal being a constant envelope signal, for maximum efficiency, and then combining these amplified signals before sending them to a transmit antenna. This therefore provides Constant Envelope High Power Amplification. However, the step of combining the high power signals for transmission through one antenna is an engineering challenge, and overall this solution has size, cost and weight penalties. Note that a constant envelope signal is one where the amplitude of the signal is not modulated. It may synonymously be known as a constant amplitude signal.
Solutions to these problems have been sought which take non-constant-amplitude multiplexes of signals and modify them before they are passed through the amplifier, with the aim of maximising the fraction of output power which carries the desired signals, which correspondingly means minimising the fraction of output power which goes into useless erroneous signals known as intermodulation signals.
An alternative approach is to use a single, power-efficient, constant envelope amplifier. A known technique that works on this basis is called Phase Optimised Constant Envelope Transmission (POCET), and is described in US patent No. US8774315. It works by using pre-computed tables of composite signal phase values, with a value from the table being chosen through an optimisation process that minimises or reduces envelope variation for a phase modulated carrier subject to intra-signal constraints for the multiple input signals.
International patent application W001/058026 discloses an approach whereby signals from individual sources in a transmission system are combined and amplified in a power amplifier, whilst simultaneously the signals are combined and subtracted from a part of the amplified combined signal to provide an error signal that is a measure of the distortion produced by the amplification process. The error signal is then adjusted in phase and amplitude before being combined with the power-amplified signal to compensate for the distortion, in a feedforward system.
It is an object of the present invention to provide an alternative approach to the efficient generation of transmission signals.
According to a first aspect of the present invention there is provided a transmitter having a transmitter signal processor (TSP) for processing a plurality of signals for transmission to produce an output signal of constant envelope, the transmitter signal processor having a sum input comprising a sum of the plurality of signals for transmission, and further inputs comprising of each signal for transmission, and an output, the TSP being arranged to compute an error signal between the sum input and the output of the TSP, and for each input signal, to model the effect of the error in a receiver by correlating the error signal with the input signal and to use the sum of the effects for each input signal to generate a correction signal that is fed back, in a feedback loop, to an input of the TSP.
Embodiments of the invention thus employ a feedback approach to ameliorating distortion caused by the amplification of multiple signals where a constant envelope is desired.
Some embodiments of the invention may comprise a transmitter wherein the feedback loop generates a combined feedback signal that is subtracted from the sum input to produce a “constant envelope input signal”, the feedback loop comprising, for each input signal, a) a correlator arranged to generate a correlation between (i) said input signal and (ii) an error signal comprising a measurement of a difference between the sum input and an output of a constant envelope process or within the TSP; and b) a multiplier arranged to multiply the result of the correlation at step (a) with said input signal, to produce a multiplier output; the signal processor being further arranged to sum the output of the multiplier at step (b) for each input signal to produce a combined feedback signal and to feed back the combined feedback signal to the sum input of the signal processor wherein the constant envelope process comprises either of a normalisation function, or an analogue signal processing chain or a digital model thereof.
Embodiments may provide a transmitter that is able to process multiple (e.g. 2, 3, 4, 5 or more inputs) digital input signals for transmission, generating an output signal for transmission that has a substantially constant envelope.
It will be appreciated by the normally skilled person that the correlator, at (a), is carrying out a similar process to that which would occur in a receiver of the signal transmitted by the transmitter. This is evident because the sum input signal of (a) is of similar form to that of a reference signal used in a correlator in a well-designed receiver, and the transmitted signal is (in part) that received at the receiver. The output of the correlator therefore gives a representation as to the effects of distortion caused by the constant envelope process, as it would be seen at a receiver. This correlator output is, at (b), multiplied by the input signal to form (along with contributions from similar signals produced for each of the other input signals) the combined feedback signal that is subtracted from the sum input signal to the TSP. Thus, in effect, the distortion error caused by the constant envelope process is continuously subtracted from the input, which at least partially counters said distortion. The output signal may in some embodiments be a digital signal that is then converted to an analogue signal in a digital to analogue converter (DAC), and amplified and, if necessary, up-converted in frequency before being transmitted.
Other embodiments may include outputs of a DAC and an amplifier and/or up-converter as a part of a feedback loop of the transmitter signal processor (TSP), which enables the TSP to take into account distortions added by these components, and so lead to an improved, more constant envelope, signal that is transmitted by the transmitter. Alternatively, a digital model of one or more components, such as a DAC, and up-converter and/or an amplifier may be used in the feedback loop of the TSP, rather than the corresponding analogue components. Accordingly, in some embodiments of the invention, the constant envelope process comprises an analogue signal processing chain having at least one of an amplifier or a frequency up-converter, or comprising a digital model thereof.
In those embodiments that incorporate analogue elements such as a frequency up-converter and/or an amplifier, the feedback loop further comprises a digital to analogue converter, along with a frequency down-converter where an up-converter is present in the constant envelope process. This enables an analogue signal, which may be at a different frequency to that of the different signals provided to the input of the TSP, to be brought to the same frequency as those input signals and be more conveniently processed in the feedback loop.
In some embodiments the processing within the TSP occurs entirely within the digital domain, and the constant envelope process may comprise a normaliser arranged to compute an output o(t) = p w(t)/|w(t)|, where p is the desired constant amplitude and w(t) is the sum input, or a scaled version thereof.
Advantageously, in some embodiments the correlator comprises a multiplier arranged to multiply the complex conjugate of signal (i) with signal (ii), and to accumulate the result in an accumulator.
Advantageously, a high pass filter may be included in the correlator between the multiplier and the accumulator, to remove a low frequency component from an output of the multiplier. This prevents any such low frequency components (including DC, or near-DC signals) from accumulating and causing errors. Advantageously, the transmitter may further include scaling means for scaling the input signals prior to their being summed at the sum input. The scaling means may comprise one or more multipliers. The multi plier(s) may preferably be implemented digitally. The multipliers may be arranged to scale each input signal independently. The scaling provided by the scaling means may be adjustable in operation of the TSP. The adjustment to the scaling may be determined by measurement of a DC component removed by the high pass filter.
According to a second aspect of the invention there is provided a method of combining a plurality of digital input signals for transmission by a transmitter, the method acting to produce an output signal of constant envelope, and the transmitter having a transmitter signal processor (TSP) configured to sum the digital inputs to produce a sum input, and to compute an error signal between the sum input and the output of the TSP, and to, for each digital input signal, model the effect of the error as would occur in a receiver by correlating the error signal with the digital input signal, and to use the sum of the modelled effects for each digital input signal to generate a correction signal, and to feed back the correction signal, in a feedback loop, and to subtract the feedback signal from the sum input of the TSP.
Advantageously, in some embodiments, the method may further comprise a method wherein the sum signal is fed into a constant envelope processor in the TSP that comprises at least a normalisation function or an analogue signal processing chain, or a digital model thereof, and which produces an output; wherein the feedback signal is produced by the following steps: i) measuring an instantaneous error signal by taking the difference between the sum input and the output; ii) for each input signal, modelling the effect of the instantaneous error signal, by correlating the instantaneous error signal with the input signal, and multiplying the output of the correlation with the input signal; iii) summing the results of the multiplication in step (ii) produced for each input signal, with the result of this summation comprising the feedback signal; wherein the constant envelope process comprises either of a normalisation function, or an analogue signal processing chain. Advantageously, the constant envelope processor may be arranged to normalise, using a normaliser, the constant envelope input signal.
In some embodiments the constant envelope process comprises a digital to analogue converter, and at least one of a frequency upconverter and an RF amplifier, and wherein the output for the purposes of (i) of this second aspect is derived from a downconverted and digitised version of an output from the RF amplifier and/or upconverter.
In some embodiments the constant envelope process comprises a digital model of at least a part of an analogue processing chain, including at least a power amplifier, of a transmitter in which the method is implemented. Advantageously, the digital model may have inputs from the analogue processing chain, and may be adapted to change parameters of the digital model based upon these inputs.
Embodiments of the invention will now be described in more detail, by way of example only, and with reference to the following Figures, of which:
Figure 1 shows a high level representation of a transmitter arranged to transmit multiple independent signals through a common up-conversion and amplification process;
Figure 2 shows a high level representation of a prior art process for achieving a constant envelope output signal;
Figure 3 shows a high level representation of an improved prior art process for achieving a constant envelope output signal;
Figure 4 shows a high level architecture of an embodiment of the present invention;
Figure 5 shows a more detailed architecture of an embodiment of the present invention, operable completely in the digital domain;
Figure 6 shows partial detail of an alternative embodiment of the present invention, where some elements are operable in the analogue domain; and Figure 7 shows partial detail of an alternative embodiment of the present invention, where a digital model of analogue components are used.
Figure 1 shows a simple transmitter architecture 100, where three independent digital input signals Si(t)- S3(t) are scaled in multipliers ai -a3 before being summed in summer 102 to produce a combined digital signal w(t). This is then converted to analogue form in digital-to- analogue converter (DAC) 104 before being up-converted by mixing with a local oscillator signal (not shown) in mixer 106, and amplified in amplifier 108. It is then fed to an antenna (not shown) for transmission. In general, there may of course be a different number of input signals s,(t) in a given system. A typical application may comprise a GNSS satellite, and the signals s,(t) may comprise different navigation signals, such as an open navigation signal, along with commercial, public regulated service, and safety of life navigation signals, and pilot signals, which may be at different frequencies, bandwidths or phases to each other.
The signal w(t) is the wanted signal for transmission. However, due to the independence of the signals s,(t) the envelope of w(t) can vary, for example as each signal itself varies in amplitude or phase. The variation of the envelope of w(t) leads to inefficiencies, particularly within the RF amplifier, such as the generation of intermodulation signals as mentioned earlier which, when the amplifier is in a challenging environment such as a satellite, can be costly in terms of additional cooling requirements, or excess power input required to achieve a given performance.
Figure 2 shows a simple prior art technique 200 for generating a constant envelope signal. It is similar to the architecture of Figure 1 , but with the addition of new blocks in the signal path between the summer 102 and the DAC 104. The new blocks comprise a scaling means % (which can be ignored for the purposes of this paragraph), and the “constant envelope” (CE) block, which takes signal w(t) and produces an output o(t) = w(t)/|w(t)|) of constant (or more constant than its input) envelope. Thus, it acts to normalise the input signal to an amplitude /3, All known techniques for producing a constant envelope distort the output signal to a degree, but this simple approach performs badly compared to other techniques, including embodiments of the current invention.
Measurement of the error produced by the approach can be done by subtraction, in subtractor 202 of the output signal of the CE block from the input signal, to produce instantaneous error signal eo(t). When implementing a technique as shown in Figure 2, the power of the error eo(t) would generally be minimised by design by adjusting the scaling factor %, such that the mean squared value of w(t) equals the mean squared value of o(t), which is p2.
Alternatively, and equivalently, the three scale factors ai, a2 and as could be adjusted by a common scale factor of %. Assuming the scale factors are fixed, this is all set up once only. It should be noted that known implementations of any system of the type shown in Figure 2 do not actually use the error signal eo(t) in any real-time correction process - it is illustrated here simply to show where the error would be measured.
This simple prior art approach has two limitations:
• There is no control over the power density spectrum of noise added by the action of the CE block; and
• There is no control over the actual signal power which is seen by receivers matched to the individual signals
An improved prior art technique 300 is shown in Figure 3. This is the technique used by prior art document US8774315 which, as stated above, uses precomputed tables to generate an output signal, based upon the individual input signals as presented to the CE component by the dotted line connections 302. These tables take possible combinations of input signals, such as a discrete number of different phases for each (for phase modulated signals), and precompute an ideal output signal for each possible input combination.
Figure 4 shows at a top level a system 400 according to an embodiment of the present invention. The basic principle of this embodiment, and all embodiments of the invention, is the use of negative feedback of the error signal e0(t) to correct for errors introduced by the constant envelope process. The error signal e0(t) is equivalent to the error signal as shown in Figure 2, but in this embodiment the error signal is used as explained below, to produce the feedback signal. Signals Si(t)- S3(t) are the input signals which need to be combined, and transmitted from a power amplifier. They are scaled by corresponding scaling factors ai- 03 and summed in summer 402, providing a summation output. A further combined scaling may performed on the summation output at 404, or alternatively this scaling may be done by incorporating an appropriate common factor to the individual scaling factors 01-03. The output of this is signal wi(t), which provides a first input to a summation node 406, to calculate the error signal e0(t). The instantaneous error caused by the conversion to constant envelope (CE) is thus computed.
Signal wi(t) is also provided to a further summation node 408 in the transmit path at which point a feedback signal is subtracted from it to produce signal w2(t) This signal then feeds the CE process to produce an output o(t), the CE process in this embodiment being given by o(f) = w2(t) / |w2(t) | ). The signal o(t) is fed to the summation node 406 as its second input, where it is subtracted from signal wi(t) to produce e0(t). Signal o(t)) is the constant envelope (digital) signal in this embodiment, which is then converted to an analogue signal and up- converted in frequency and amplified in a power amplifier for transmission, as required.
The feedback signal is produced by taking the error signal and, for each individual input signal Si(t), applying it to a correlator 410 that correlates it with s,(t) to model the effect that the error has on a correlation process that would happen in a receiver, which of course has (in GNSS and other Direct Sequence Spread Spectrum applications), its own locally stored reference copy of signal Si(t). Note that Figure 4 only shows the correlation and feedback process associated with signal Si(t), and in practice each signal s,(t) will have its own correlator to provide its own contribution to the feedback signal as is explained later. The correlator output is then multiplied by the signal s,(t) in multiplier 412 to become si(t)’s contribution to the feedback correction signal. The corrections themselves, due to their being subtracted from signal wi(t), are distorted by the CE process, but the continuous negative feedback still reduces the cumulative error effect.
Figure 5 shows in more detail the generation of the feedback signal. The embodiment 500 shown is the same as that of Figure 4, but with additional elements shown that further clarify the operation of the system. Like reference numbers indicate like functional blocks. As explained earlier, the instantaneous transmitter error e0(t) is computed, and correlated with each reference signal. This is only shown for signal si(t) in the figure; the processing for the other signals uses duplicated blocks. Arrow 502 indicates, for example, a feed to correlators for the other signals st(t) and arrow 504 indicates the summation of the results of the processing of those signals to create the overall feedback signal. The correlator 410 comprises a conjugator 506 for conjugating the reference signal before it is multiplied by the error signal in multiplier 508. It is then accumulated in accumulator 510 to produce, error signal ei(t).
An ideal system would add to output signal o(t) a correction to the next sample which, when demodulated by the relevant receiver correlator, would equal the negative of the accumulated error for that signal. This would make the accumulated error on that signal zero after the next sample. This is purpose of multiplier 412 which multiplies the accumulated error from accumulator 510 by the reference signal Si(t) before summing the result at summer 504 with results from similar processes occurring for other input signals st(t), and then in adder 406 subtracting the result of the summation from the wanted signal wi(t), giving a modified wanted signal w2(t).
The distorting operation of the CE block means that the corrections are also distorted, so the level of correction actually achieved on the next sample is reduced. However, a significant degree of correction does survive the CE block, and modelled performance better than the prior art techniques has been achieved.
A detail to note is that unless the scale factor at 404 (or equivalent adjustments made to ai .as) can be simultaneously optimally adjusted, the output amplitude which can actually be achieved for signal component s, may not equal (/_ cq si). Therefore the error associated with that signal component can grow without limit. This problem is solved by including a high pass filter at the point indicated by star 0 in the correlator 410. By measuring a DC component removed by the high pass filter, the source signal scale factors (a;) can be adjusted by a slow adaptive algorithm (e.g. an LMS steepest gradient algorithm).
The above embodiments all operate in the digital domain throughout, in that all the processing, and the CE process also, operate in this domain, and provides its output to a DAC which then feeds any required up-conversion and amplification for transmission. Other embodiments may use a CE process that operates at least in part in the analogue domain, with a feedback path coming from an element within the analogue path, typically after an amplification stage. This allows imperfections within the amplifier to be directly taken into account by the processing occurring in the feedback path. These imperfections may include any soft-clipping that occur in the amplifier, and/or any AM to AM, and AM to PM distortion that may occur, where AM is amplitude modulation, and PM is phase modulation.
Figure 6 shows in top level form part 600 of an embodiment of the invention that has the CE process in analogue form, this comprising part of the transmit chain of a transmitter. Note that the details of the feedback processing are the same as that for the embodiments above, and will not be described in detail further in relation to this figure.
Thus, this figure just shows the analogue equivalent of the (digital) CE block in figure 5, along with the error summer 406. The connections to the summer 406 from w-i(t) and o(t), along with the output from summer 406 show the paths to the feedback circuit, this comprising e.g. the feedback circuit as explained in relation to Figure 4.
Here, the signal wi(t) is presented to a DAC and the resulting analogue signal is up- converted to the transmit frequency in up-conversion mixer 604, before being passed to an RF amplifier 606 for amplification to a desired transmit output power, to produce an analogue power signal 608 for subsequent transmission via an antenna. This is the step where much of the distortion being corrected for by the method of the invention takes place. A coupler 610 takes a small amount of this transmit energy from the output of the RF amplifier, and brings it back to a baseband signal in downconversion mixer 612, and converts this back to a digital signal in analogue to digital converter 614. It is then fed to the feedback loop to generate the error signal e0(t) as for previous embodiments.
Unlike the all-digital approach of previous embodiments, this embodiment may introduce a small delay in the signal path. In a GNSS application, where the signals st(t) comprise a sequence of chips, then provided that any added delay is small compared to one chip duration (which, in the higher GNSS chip rates is about 0.1 ps) this delay can be ignored without any significant problem occurring. However it is not difficult to compensate for such a delay, especially if it is approximately constant. To do this, the delay is measured at the design and test stage of system production. Then that amount of delay is inserted into the digital correction circuits, at the conjugate box 506 in Figure 5 (albeit that is shown in an all- digital scenario, but the feedback signal generation will be the same in this embodiment as previously stated). A further potential issue with the embodiment of Figure 6 is that the RF measurement process, of splitting a signal from an output of the amplifier (in coupler 610), downconverting it in frequency and converting it to digital form may introduce noise. Figure 7 shows an alternative embodiment that aims to reduce the effects of any such noise that may be present. This embodiment has similarities to that of Figure 6, in that an output of an analogue transmit chain is used to influence the feedback process. The analogue transmit chain, and the coupler, down-converter and digitiser are similar to that shown in Figure 6, and hence has the same reference numbers. However, in this embodiment the digitiser 614 output is not directly used, but is instead fed to a digital amplifier model 616. This digital amplifier model is a model of the RF amplifier. It has adjustable parameters that are adapted slowly over a “relatively long” time period, based upon the input from the downconverted and digitised signal from the actual power amplifier, since the characteristics of the RF amplifier will not vary rapidly. This time period may be for example measured in tens or hundreds of milliseconds, or seconds. Their adaptation is controlled by feedback of the error which is the difference between the (downconverted and digitised) amplifier output p(t) and the model output o(t).
The adjustable parameters may take the form of an input-envelope to output-envelope mapping function and an input-envelope to output-phase-error mapping function. Alternatively they may be the parameters of a Volterra function model of the power amplifier. Such models are mentioned in “The Evolution of PA Linearization” by Allen Katz, John Wood, and Daniel Chokola, IEEE Microwave Magazine, Feb 2016, p. 32.
This embodiment provides the advantage that any noise or error in the coupled output (o(t) is not fed directly into the feedback process described earlier, but is smoothed by the long term adaptation within the model. The model itself, being digital, operates with low output noise.
It will be appreciated by the normally skilled person that the novel techniques described herein are completely different from the existing methods because, whereas they use precomputed tables, the new method uses real-time feedback of errors.
Embodiments of the invention will typically be implemented in software, for example in one or more digital signal processors or microprocessors - the processor or processors being programmable hardware controlled by computer code, or may be operated in firmware/hardware, such as in one or more Application Specific Integrated Circuits (ASIC), or a Field Programmable Gate Arrays (FPGA). Such devices will typically include, or be connected with, a suitable memory and storage, as would be appreciated by a normally skilled person. The invention may extend therefore to a software program arranged to be storable in computer memory and comprising of instructions that cause a processor to implement the various elements described herein. Some embodiments may be implemented in a combination of hardware or software, and the transmitter signal processor may comprise a combination of analogue and digital circuitry arranged to process signals in both the analogue and digital domains. In particular, analogue circuitry forming part of the transmitter signal processor may comprise of one or more amplifiers (including power amplifiers), frequency shifters, filters etc. that form part of a signal processing chain of a signal to be transmitted by an antenna. Embodiments of the invention have utility in many areas of signal transmission, typically in space or airborne application, such as in GNSS satellites, and may also be used more widely for terrestrial radio receivers (where increased power efficiency gives longer battery life and reduced waste heat).

Claims

Claims
1. A transmitter having a transmitter signal processor (TSP) for processing a plurality of signals for transmission to produce an output signal of constant envelope, the transmitter signal processor having a sum input comprising a sum of the plurality of signals for transmission, and further inputs comprising of each signal for transmission, and an output, the TSP being arranged to compute an error signal between the sum input and the output of the TSP, and for each input signal, to model the effect of the error in a receiver by correlating the error signal with the input signal and to use the sum of the effects for each input signal to generate a correction signal that is fed back, in a feedback loop, to an input of the TSP.
2. A transmitter as claimed in claim 1 wherein the feedback loop generates a combined feedback signal that is subtracted from the sum input to produce a “constant envelope input signal”, the feedback loop comprising, for each input signal, a) a correlator arranged to generate a correlation between (i) said input signal and (ii) an error signal comprising a measurement of a difference between the sum input and an output of a constant envelope processor within the TSP; and b) a multiplier arranged to multiply the result of the correlation at step (a) with said input signal, to produce a multiplier output; the signal processor being further arranged to sum the output of the multiplier at step (b) for each input signal to produce a combined feedback signal and to feed back the combined feedback signal to the sum input of the signal processor; wherein the constant envelope processor comprises either of a normalisation function, or an analogue signal processing chain or a digital model thereof.
3. A transmitter as claimed in claim 2 wherein, when the constant envelope processor comprises of an analogue signal processing chain, having at least one of an amplifier or a frequency up-converter, or comprises a digital model thereof.
4. A transmitter as claimed in claim 3 wherein the feedback loop further comprises a digital to analogue converter, along with a frequency down-converter where an up-converter is present in the constant envelope process.
5. A transmitter as claimed in claim 1 or claim 2 wherein the processing within the signal processor occurs entirely within the digital domain, and the constant envelope process comprises of a normaliser arranged to compute an output o(t) = w(t)/|w(t)|, where is the desired constant amplitude and w(t) is the sum input, or a scaled version thereof.
6. A transmitter as claimed in any of the above claims wherein the correlator comprises a multiplier arranged to multiply the complex conjugate of signal (i) with signal (ii), and to accumulate the result in an accumulator.
7. A transmitter as claimed in claim 6 wherein a high pass filter is included in the correlator between the multiplier and the accumulator, to remove a low frequency component from an output of the multiplier.
8. A transmitter as claimed in any of the above claims wherein the transmitter further includes scaling means for scaling the input signals prior to their being summed at the sum input.
9. A method of combining a plurality of digital input signals for transmission by a transmitter, the method acting to produce an output signal of constant envelope, and the transmitter having a transmitter signal processor (TSP) configured to sum the digital inputs to produce a sum input, and to compute an error signal between the sum input and the output of the TSP, and to, for each digital input signal, model the effect of the error as would occur in a receiver by correlating the error signal with the digital input signal, and to use the sum of the modelled effects for each digital input signal to generate a correction signal, and to feed back the correction signal, in a feedback loop, and to subtract the feedback signal from the sum input of the TSP.
10. A method as claimed in claim 9 wherein the sum input signal is fed into a constant envelope processor in the TSP that comprises at least a normalisation function or an analogue signal processing chain, or a digital model thereof, and which produces an output; wherein the feedback signal is produced by the following steps: i) measuring an instantaneous error signal by taking the difference between the sum input and the output; ii) for each input signal, modelling the effect of the instantaneous error signal, by correlating the instantaneous error signal with the input signal, and multiplying the output of the correlation with the input signal; iii) summing the results of the multiplication in step (ii) produced for each input signal, with the result of this summation comprising the feedback signal.
11. The method of claim 10 wherein the constant envelope processor comprises a normaliser for normalising the constant envelope input signal.
12. The method of claim 10 or claim 11 wherein the constant envelope process further comprises a digital to analogue converter, and at least one of a frequency upconverter and an RF amplifier, and wherein the output for the purposes of claim 9(i) is derived from a downconverted and digitised version of an output from the RF amplifier and/or upconverter.
13 The method of claim 10 or claim 11 wherein the constant envelope process further comprises a digital model of at least a part of an analogue processing chain, including at least a power amplifier, of a transmitter in which the method is implemented.
EP23805491.0A 2022-11-09 2023-11-07 Transmitter signal processor Pending EP4616530A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB2216710.0A GB2624195A (en) 2022-11-09 2022-11-09 Signal processor
PCT/EP2023/080925 WO2024100005A1 (en) 2022-11-09 2023-11-07 Transmitter signal processor

Publications (1)

Publication Number Publication Date
EP4616530A1 true EP4616530A1 (en) 2025-09-17

Family

ID=84839824

Family Applications (1)

Application Number Title Priority Date Filing Date
EP23805491.0A Pending EP4616530A1 (en) 2022-11-09 2023-11-07 Transmitter signal processor

Country Status (5)

Country Link
EP (1) EP4616530A1 (en)
JP (1) JP2025537241A (en)
CN (1) CN120226263A (en)
GB (1) GB2624195A (en)
WO (1) WO2024100005A1 (en)

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4560945A (en) * 1984-09-04 1985-12-24 Westinghouse Electric Corp. Adaptive feedforward cancellation technique that is effective in reducing amplifier harmonic distortion products as well as intermodulation distortion products
US6570444B2 (en) * 2000-01-26 2003-05-27 Pmc-Sierra, Inc. Low noise wideband digital predistortion amplifier
AU2000223178A1 (en) * 2000-02-03 2001-08-14 Wiseband Communications Ltd. Super-linear multi-carrier power amplifier
US8031804B2 (en) * 2006-04-24 2011-10-04 Parkervision, Inc. Systems and methods of RF tower transmission, modulation, and amplification, including embodiments for compensating for waveform distortion
KR20100059974A (en) * 2007-09-27 2010-06-04 교세라 가부시키가이샤 Power amplifying circuit, and transmitter and wireless communication device using the same
US8774315B2 (en) 2009-08-25 2014-07-08 The Aerospace Corporation Phase-optimized constant envelope transmission (POCET) method, apparatus and system
CN102694569B (en) * 2012-06-07 2014-05-14 清华大学 Constant envelop multiplexing method, generating device and receiving method for navigation signal
CN103023598B (en) * 2012-11-23 2016-03-30 清华大学 The permanent envelope multiplex method of double frequency four component spread-spectrum signal, device and method of reseptance

Also Published As

Publication number Publication date
GB2624195A (en) 2024-05-15
CN120226263A (en) 2025-06-27
WO2024100005A1 (en) 2024-05-16
JP2025537241A (en) 2025-11-14
GB202216710D0 (en) 2022-12-21

Similar Documents

Publication Publication Date Title
US11129076B2 (en) Method and system for baseband predistortion linearization in multi-channel wideband communication systems
US7330517B2 (en) Amplifier linearization using non-linear predistortion
US9209841B2 (en) Adaptively controlled digital pre-distortion in an RF power amplifier using an integrated signal analyzer with enhanced analog-to-digital conversion
US5959500A (en) Model-based adaptive feedforward amplifier linearizer
US7555057B2 (en) Predistortion calibration in a transceiver assembly
US7471739B1 (en) Advanced adaptive pre-distortion in a radio frequency transmitter
US7206356B2 (en) Wireless transmitter with reduced power consumption
US7542518B2 (en) Predistortion apparatus and method for compensating for a nonlinear distortion characteristic of a power amplifier using a look-up table
US8121560B1 (en) Pre-distortion with enhanced convergence for linearization
US8224266B2 (en) Power amplifier predistortion methods and apparatus using envelope and phase detector
US6956433B2 (en) Polynomial predistorter using complex vector multiplication
US20050180527A1 (en) Digital predistorter using power series model
EP0890218A1 (en) Adaptive amplifier distortion compensation circuit
WO2001008293A1 (en) Feed forward distortion reduction system
US20100327932A1 (en) Feedback system with improved stability
CN102231620A (en) Power amplifier linearization method and device based on baseband digital predistortion technology
US7804359B1 (en) Linearization with memory compensation
GB2400996A (en) Signal sample acquisition techniques in a distortion controller for an RF PA
CN105978500A (en) Analog predistortion system, transceiver and communication device
WO2024100005A1 (en) Transmitter signal processor
WO1999045638A1 (en) Predistorter
US20050157813A1 (en) Methods and apparatus for signal distortion correction
US6919764B2 (en) Amplifier control system with statistical enhancement of resolution of digital control signals
US8295394B1 (en) Error signal formation for linearization
JP2003078451A (en) Amplifier

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: UNKNOWN

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20250430

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC ME MK MT NL NO PL PT RO RS SE SI SK SM TR

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)