The present disclosure relates to an impedance detection circuit, an impedance control circuit, and a Doherty amplifier circuit.
Patent Document 1 describes an amplification device that adjusts the phase or the amplitude of a second signal input to a second amplification part, by using the reflection coefficient of each of an output from the first amplification part and an output from the second amplification part.
However, the amplification device described in Patent Document 1 detects the reflection coefficient of each of the output from the first amplification part and the output from the second amplification part and thus requires two directional couplers. Directional couplers are large due to the structure thereof and are not usable for, for example, mobile communication terminals.
The present disclosure prevents a circuit from being upsized and also to detect impedance.
An impedance detection circuit according to an aspect of the present disclosure includes: a first detector that detects a first voltage amplitude at an end of an inverter circuit having the end to which a radio frequency signal is input and having a different end from which a signal is output; a second detector that detects a second voltage amplitude of the different end of the inverter circuit; and a phase difference detector that detects a phase difference between a phase of a voltage across the end of the inverter circuit and a phase of a voltage across the different end of the inverter circuit. An absolute value of a product of diagonal elements of a dependent parameter for the inverter circuit is smaller than an absolute value of a product of off-diagonal elements.
An impedance control circuit according to an aspect of the present disclosure includes: the impedance detection circuit of the present disclosure; and at least one of a first transistor and a second transistor, the first transistor having a base or a gate to which a first signal based on the first voltage amplitude and the second voltage amplitude is input and having a collector from which first current is output to the end of the inverter circuit, a second transistor having a base or a gate to which a second signal based on the first voltage amplitude and the second voltage amplitude is input and having a collector from which second current is output to the different end of the inverter circuit.
A Doherty amplifier circuit according to an aspect of the present disclosure includes: a carrier amplifier that amplifies an input radio frequency signal; a peaking amplifier that amplifies an input radio frequency signal; and the impedance control circuit of the present disclosure. The inverter circuit serves as a Doherty combiner that combines a signal output by the carrier amplifier and a signal output by the peaking amplifier.
According to the present disclosure, the circuit may be prevented from being upsized and may also detect impedance.
Hereinafter, embodiments of an impedance detection circuit, an impedance control circuit, and a Doherty amplifier circuit of the present disclosure will be described in detail based on the drawings. The embodiments do not limit the present disclosure. It goes without necessarily saying that each embodiment is exemplification and configurations illustrated in different embodiments can be partially replaced or combined. After a second embodiment, the description of a matter common to that in a first embodiment is omitted, and one or more different points will only be described. In particular, the same advantageous effects and operations of the same configuration are not referred to in each embodiment.
An amplifier circuit 1 includes an amplifier 2, an inverter circuit 3, a 90-degree shift circuit 4, and an impedance control circuit 10.
The amplifier 2 amplifies a radio frequency signal RFIN and outputs a radio frequency signal RF1 to an end 3a of the inverter circuit 3. The inverter circuit 3 receives the radio frequency signal RF1 at the end 3a and outputs a radio frequency signal RF2 from a different end 3b to a load 150.
The amplifier 2 assumes that impedance ZL′ seen from the output terminal thereof to the load 150 has a value assumed in designing. A general emitter-grounded or source-grounded single-ended amplifier, a differential amplifier, a Doherty amplifier, an envelope tracking amplifier, and the like are exemplified as the amplifier 2; however, the present disclosure is not limited to these.
An output voltage of the amplifier 2 is a voltage VL′, and output current is current IL′.
The inverter circuit 3 converts the value of the impedance ZL for the load 150 to a reciprocal thereof (admittance). The inverter circuit 3 is a ¼ wavelength line of characteristic impedance Z0; however, the present disclosure is not limited to this.
A voltage input to the end 3a of the inverter circuit 3 is a voltage VI1, and input current thereof is current II1. A voltage output from the different end 3b of the inverter circuit 3 is a voltage VI2, and output current is current II2.
A voltage input to the load 150 is a voltage VL, and current input to the load 150 is current IL.
The impedance control circuit 10 controls the impedance ZL′. The impedance ZL′ is also the input impedance of the inverter circuit 3.
The impedance control circuit 10 includes transistors Q1 and Q2, variable phase control circuits 11 and 15, variable gain control circuits 12 and 16, capacitors 13 and 17, resistors 14 and 18, a control circuit 19, and an impedance detection circuit 20.
Each transistor is a bipolar transistor in the present disclosure; however, the present disclosure is not limited to this. A heterojunction bipolar transistor (HBT) is exemplified as the bipolar transistor; however, the present disclosure is not limited to this. The transistor may be, for example, a field effect transistor (FET). The transistor may be a multi-finger transistor in which a plurality of unit transistors are electrically connected in parallel. A unit transistor denotes a minimum configuration of a transistor.
If the transistor is a FET, the drain of the FET corresponds to the collector of the bipolar transistor, the gate thereof corresponds to the base, and the source thereof corresponds to the emitter.
The transistor Q1 corresponds to an example of “first transistor” of the present disclosure. The transistor Q2 corresponds to an example of “second transistor” of the present disclosure. The variable gain control circuit 12 corresponds to an example of “first variable gain control circuit” of the present disclosure. The variable gain control circuit 16 corresponds to an example of “second variable gain control circuit” of the present disclosure. The variable phase control circuit 11 corresponds to an example of “first variable phase control circuit” of the present disclosure. The variable phase control circuit 15 corresponds to an example of “second variable phase control circuit” of the present disclosure.
The impedance detection circuit 20 includes detectors 21 and 22 and a phase difference detector 23.
The detector 21 corresponds to an example of “first detector” of the present disclosure. The detector 22 corresponds to an example of “second detector” of the present disclosure.
The detector 21 detects the voltage VI1 across the end 3a of the inverter circuit 3 and outputs a voltage amplitude |VI1| to the control circuit 19.
The voltage amplitude |VI1| corresponds to an example of “first voltage amplitude” of the present disclosure.
The detector 22 detects the voltage VI2 across the different end 3b of the inverter circuit 3 and outputs a voltage amplitude |VI2| to the control circuit 19.
The voltage amplitude |VI2| corresponds to an example of “second voltage amplitude” of the present disclosure.
The phase difference detector 23 detects a phase difference (arg(VI1)−arg(VI2)) between the voltage VI1 and the voltage VI2 and outputs the phase difference (arg(VI1)−arg(VI2)) to the control circuit 19.
Based on the voltage amplitudes |VI1| and |VI2| and the phase difference (arg(VI1)−arg(VI2)), the control circuit 19 outputs a phase control signal S1 to the variable phase control circuit 11, outputs a gain control signal S2 to the variable gain control circuit 12, and outputs a bias control signal S3 to an end of the resistor 14. Alternatively, based on the voltage amplitudes |VI1| and |VI2| and the phase difference (arg(VI1)−arg(VI2)), the control circuit 19 outputs a phase control signal S4 to the variable phase control circuit 15, outputs a gain control signal S5 to the variable gain control circuit 16, and outputs a bias control signal S6 to an end of the resistor 18.
The variable phase control circuit 11 changes the phase of the radio frequency signal RFIN by a phase θ1 based on the phase control signal S1 and outputs a radio frequency signal RF11 to the variable gain control circuit 12.
The variable gain control circuit 12 changes the amplitude of the radio frequency signal RF11 by using a gain G1 based on the gain control signal S2 and outputs a radio frequency signal RF12 via the capacitor 13 that is a DC blocking capacitor to the base of the transistor Q1.
A different end of the resistor 14 is electrically connected to the base of the transistor Q1. A bias voltage B1 is input from the different end of the resistor 14 to the base of the transistor Q1.
The emitter of the transistor Q1 is electrically connected to the reference potential. A voltage for substrate and source is exemplified as the reference potential; however, the present disclosure is not limited to this. The collector of the transistor Q1 is electrically connected to a power supply voltage VCC with a choke coil 31 interposed therebetween, and power is supplied.
The transistor Q1 outputs current Iadd1 according to the radio frequency signal RF12 and the bias voltage B1 from the collector to the end 3a of the inverter circuit 3. In other words, the transistor Q1 outputs a radio frequency signal from the collector to the end 3a of the inverter circuit 3, the radio frequency signal being obtained by amplifying the radio frequency signal RF12.
The current Iadd1 corresponds to an example of “first current” of the present disclosure.
If a reactance component (imaginary component) of the impedance ZL′ is not required to be compensated, the variable phase control circuit 11 does not have to be provided. That is, the variable gain control circuit 12 may change the amplitude of the radio frequency signal RFIN by using the gain G1 based on the gain control signal S2 and may output the radio frequency signal RF12 to the base of the transistor Q1 via the capacitor 13 that is the DC blocking capacitor.
Both or only one of the variable gain control circuit 12 and the resistor 14 may be provided. That is, both or only one of the radio frequency signal RF12 and the bias voltage B1 may be input to the base of the transistor Q1.
One or both of the radio frequency signal RF12 and the bias voltage B1 correspond to an example of “first signal” of the present disclosure. Specifically, the radio frequency signal RF12 is a signal the phase or the gain of which is controlled in accordance with the phase control signal S1 based on the voltage amplitudes |VI1| and |VI2| and the gain control signal S2 and is “first signal” based on the voltage amplitudes |VI1| and |VI2|. The bias voltage B1 is a signal controlled in accordance with the bias control signal S3 based on the voltage amplitudes |VI1| and |VI2| as described above and is “first signal” based on the voltage amplitudes |VI1| and |VI2|.
The 90-degree shift circuit 4 shifts the phase of the radio frequency signal RFIN by 90 degrees and outputs a radio frequency signal RF3 to the variable phase control circuit 15.
The variable phase control circuit 15 changes the phase of the radio frequency signal RF3 by a phase θ2 based on the phase control signal S4 and outputs a radio frequency signal RF13 to the variable gain control circuit 16.
If the control circuit 19 is designed to add 90-degree offset to the phase control signal S4, the 90-degree shift circuit 4 does not have to be provided.
The variable gain control circuit 16 changes the amplitude of the radio frequency signal RF13 by using a gain G2 based on the gain control signal S5 and outputs a radio frequency signal RF14 to the base of the transistor Q2 via the capacitor 17 that is the DC blocking capacitor.
A different end of the resistor 18 is electrically connected to the base of the transistor Q2. A bias voltage B2 is input from the different end of the resistor 18 to the base of the transistor Q2.
The emitter of the transistor Q2 is electrically connected to the reference potential. The collector of the transistor Q2 is electrically connected to the power supply voltage VCC with a choke coil 32 interposed therebetween, and power is supplied.
The transistor Q2 outputs current Iadd2 according to the radio frequency signal RF14 and the bias voltage B2 from the collector to the different end 3b of the inverter circuit 3.
The current Iadd2 corresponds to an example of “second current” of the present disclosure.
If the reactance component (imaginary component) of the impedance ZL′ is not required to be compensated, the variable phase control circuit 15 does not have to be provided. That is, the variable gain control circuit 16 may change the amplitude of the radio frequency signal RF3 by using the gain G2 based on the gain control signal S5 and output the radio frequency signal RF14 to the base of the transistor Q2 via the capacitor 17 that is the DC blocking capacitor.
Both or only one of the variable gain control circuit 16 and the resistor 18 may be provided. That is, both or only one of the radio frequency signal RF14 and the bias voltage B2 may be input to the base of the transistor Q2.
One or both of the radio frequency signal RF14 and the bias voltage B2 correspond to an example of “second signal” of the present disclosure.
If the impedance ZL′ deviates from the value assumed in designing in the amplifier 2, characteristics are deteriorated on occasions. For example, substantial deviation of the impedance ZL′ from the value assumed in designing in the amplifier 2 causes substantial distortion in the radio frequency signals RF1 and RF2 and thus misoperation in communication apparatus nearby in some cases. In particular, the amplifier 2 that is a Doherty amplifier is typically less resistant to change in the impedance ZL′.
Hence, the impedance control circuit 10 performs control to cause the impedance ZL′ to have a value close to the value assumed in designing. This enables the impedance control circuit 10 to prevent the distortion in the radio frequency signals RF1 and RF2.
(1)
The inverter circuit 3 has a relationship that the voltage VI2 is proportional to the current II1 in a carrier frequency. That is, Formula (1) below holds true.
VI2=−j*ZINV*II1 (1)
In Formula (1), ZINV is referred to as inverter impedance and is a positive or negative real number. The inverter impedance corresponds to mirror impedance of two-terminal pair network.
The inverter circuit 3 also has a relationship that the current II2 is proportional to the voltage VI1 in the carrier frequency. That is, Formula (2) below holds true.
The control circuit 19 detects the voltage amplitudes |VI1| and |VI2| of the respective voltages VI1 and VI2 and the phase difference (arg(VI1)−arg(VI2)) between the voltage VI1 and the voltage VI2 by using Formula (1) and Formula (2) and may thereby calculate the impedance ZINV. Specifically, by using the detectors 21 and 22, the control circuit 19 detects the voltage amplitudes |VI1| and |VI2| of the respective voltages VI1 and VI2 derived according to Formula (1) and Formula (2). By using the phase difference detector 23, the control circuit 19 also detects the phase difference (arg(VI1)−arg(VI2)) between the voltage VI1 and the voltage VI2 derived according to Formula (1) and Formula (2). The control circuit 19 calculates the impedance ZINV by using the detected voltage amplitudes |VI1| and |VI2| and the phase difference (arg(VI1)−arg(VI2)).
Further, the impedance control circuit 10 outputs the high frequency current Iadd1 or Iadd2 to an end portion of the inverter circuit 3 and may thereby control the impedance ZL′ seen from the amplifier 2.
Specifically, if the impedance ZL′ is low, the impedance control circuit 10 outputs the current Iadd1 to the end 3a of the inverter circuit 3. The current Iadd1 flows to the inverter circuit 3. Accordingly, the current IL′ is decreased by an amount corresponding to the current Iadd1. That is, the impedance control circuit 10 may decrease the current IL′ output by the amplifier 2. This enables the impedance control circuit 10 to increase the impedance ZL′ seen from the amplifier 2 to the load 150 and prevent the impedance ZL′ from varying.
If the impedance ZL′ is high, the impedance control circuit 10 outputs the current Iadd2 to the different end 3b of the inverter circuit 3. The current Iadd2 flows to the load 150. Accordingly, the current II2 is decreased by an amount corresponding to the current Iadd2. That is, the impedance control circuit 10 may decrease the current II2 output by the inverter circuit 3. The decreased current II2 causes the voltage VL′ output by the amplifier 2 to be low due to the characteristics of the inverter circuit 3. The impedance control circuit 10 may thereby decrease the impedance ZL′ seen from the amplifier 2 to the load 150 and prevent the impedance ZL′ from varying.
Further, if the impedance control circuit 10 includes the variable phase control circuits 11 and 15, the following actions are provided. That is, if the impedance control circuit 10 controls the phase of the current Iadd1 and Iadd2 based on the phase difference (arg(VI1)−arg(VI2)), the control of the impedance ZL′ described above may also be act on the reactance component (imaginary component). This enables the impedance control circuit 10 to further prevent the impedance ZL′ from varying.
(2)
In
As a known circuit for which Formula (1) and (2) hold true, a circuit composed of lumped elements, a circuit obtained by combining a transmission line and lumped elements, a circuit using a transducer are exemplified. These circuits will be described for other embodiments.
According to Formula (1) and (2), the inverter circuit 3 is a circuit for which Formula (3) below holds true near the carrier frequency.
For example, the amplifier 2 is designed on the assumption of the impedance ZL′ of 50Ω (ohm) and the characteristic impedance Z0 of 50Ω; however, the present disclosure is not limited to these. If the characteristic impedance Z0 is different from the assumed impedance (50Ω) of the impedance ZL′, the following processing may be performed in such a manner that the voltage amplitude |VI1| or |VI2| is multiplied by the constant.
(3)
First, control performed for lower impedance ZL′ by the impedance control circuit 10 will be described. If the impedance ZL′ is lower than the assumed impedance (for example, 50Ω), the voltage amplitude |VI1| lower than the voltage amplitude |VI2| is observed.
In this case, the impedance control circuit 10 outputs the high frequency current Iadd1 to the end 3a of the inverter circuit 3 and thereby decreases the current IL′. This enables the impedance control circuit 10 to increase the impedance ZL′.
For example, the control circuit 19 controls the gain G1 of the variable gain control circuit 12 by using Formula (4) below. In Formula (4), α1 is sensitivity (a coefficient or a constant) for controlling the gain G1 and is determined in consideration of the gain of the transistor Q1.
As represented by Formula (4), with the increase of a difference between the voltage amplitude |VI2| and the voltage amplitude |VI1|, the impedance control circuit 10 increases the amplitude of the radio frequency signal RF12 to be input to the base of the transistor Q1 and thereby increases the high frequency current Iadd1 to be output from the collector of the transistor Q1.
Formula (4) is the simplest expression for the impedance control circuit 10 to achieve the control goal, and the present disclosure is not limited to this. The impedance control circuit 10 may use a ratio between the voltage amplitude |VI2| and the voltage amplitude |VI1| instead of the difference between the voltage amplitude |VI2| and the voltage amplitude |VI1|. The impedance control circuit 10 may also use combination of these or a high-order function such as a quadric.
If the impedance ZL′ seen from the amplifier 2 is about to be low because the output impedance of the amplifier circuit 1 deviates from the assumed value, the impedance control circuit 10 may automatically increase the impedance ZL′ by performing the control represented by Formula (4). The amplifier 2 thereby exists from the low impedance state.
Further, if a reactance component (imaginary component) is generated in the inverter circuit 3, the phase difference (arg(VI1)−arg(VI2)) is shifted from 90 degrees. The control circuit 19 controls the phase θ1 based on a shift amount of the phase difference (arg(VI1)−arg(VI2)) from 90 degrees. This enables the impedance control circuit 10 to control the phase of the radio frequency signal RF12 to be input to the base of the transistor Q1. The impedance control circuit 10 may thus compensate the reactance component of the impedance ZL′.
For example, the control circuit 19 controls the phase θ1 by using Formula (5) below. In Formula (5), B1 is sensitivity (a coefficient or a constant) for controlling the phase.
Control performed for higher impedance ZL′ by the impedance control circuit 10 will then be described. If the impedance ZL′ is higher than the assumed impedance (for example, 5002), the voltage amplitude |VI1| higher than the voltage amplitude |VI2| is observed.
In this case, the impedance control circuit 10 outputs the high frequency current Iadd2 to the different end 3b of the inverter circuit 3 and thereby decreases the current I12. The decreased current I12 causes the voltage VI1 to be low due to the characteristics of the inverter circuit 3. As the result, the impedance control circuit 10 may decrease the voltage Vi′ and thus decrease the impedance ZL′.
For example, the control circuit 19 controls the gain G2 of the variable gain control circuit 16 by using Formula (6) below. In Formula (6), α2 is sensitivity (a coefficient or a constant) for controlling the gain G2 and is determined in consideration of the gain of the transistor Q2.
As represented by Formula (6), with the increase of a difference between the voltage amplitude |VI1| and the voltage amplitude |VI2|, the impedance control circuit 10 increases the amplitude of the radio frequency signal RF14 to be input to the base of the transistor Q2 and thereby increases the high frequency current Iadd2 to be output from the collector of the transistor Q2.
Formula (6) is the simplest expression for the impedance control circuit 10 to achieve the control goal, and the present disclosure is not limited to this. The impedance control circuit 10 may use a ratio between the voltage amplitude |VI1| and the voltage amplitude |VI2|, instead of the difference between the voltage amplitude |VI1| and the voltage amplitude |VI2|. The impedance control circuit 10 may also use combination of these or a high-order function such as a quadric.
If the impedance ZL′ seen from the amplifier 2 is about to be high because the output impedance of the amplifier circuit 1 deviates from the assumed value, the impedance control circuit 10 may automatically decrease the impedance ZL′ by performing the control represented by Formula (6). The amplifier 2 thereby exists from the high impedance state.
Further, if a reactance component (imaginary component) is generated in the inverter circuit 3, the phase difference (arg(VI1)−arg(VI2)) is shifted from 90 degrees. The control circuit 19 controls the phase θ2 based on a shift amount of the phase difference (arg(VI1)−arg(VI2)) from 90 degrees. This enables the impedance control circuit 10 to control the phase of the radio frequency signal RF14 to be input to the base of the transistor Q2. The impedance control circuit 10 may thus compensate the reactance component of the impedance ZL′.
For example, the control circuit 19 controls the phase θ2 by using Formula (7) below. In Formula (7), β2 is sensitivity (a coefficient or a constant) for controlling the phase.
In the circuit simulation in
The waveform 201 is inward of the waveform 200. The waveform 211 is downward of the waveform 210. That is, it is understood that the return loss is decreased. It is thus understood that the impedance ZL′ approaches the value assumed in designing.
However, a point 212 and a point 213 where the load phases are respectively 90 degrees and 270 degrees represent |VI1|=|VI2|, and the gain G1 of the variable gain control circuit 12 and the gain G2 of the variable gain control circuit 16 are each 0. That is, it is not possible for the impedance control circuit 10 to control the impedance ZL′ sufficiently. However, if the load phase is 90 degrees or 270 degrees, performance is not remarkably deteriorated in the amplifier 2 on occasions, which is acceptable.
As described above, the impedance detection circuit 20 detects the voltage amplitudes |VI1| and |VI2| and the phase difference (arg(VI1)−arg(VI2)) and may thereby prevent the circuit from being upsized and also detect the impedance of the inverter circuit 3.
If the impedance ZL′ becomes low, the impedance control circuit 10 may perform control to increase the impedance ZL′ to have the value assumed in designing by outputting the current Iadd1 to the end 3a of the inverter circuit 3.
If the impedance ZL′ becomes high, the impedance control circuit 10 may perform control to decrease the impedance ZL′ to have the value assumed in designing by outputting the current Iadd2 to the different end 3b of the inverter circuit 3.
As described above, in the amplifier circuit 1, the impedance ZL′ seen from the amplifier 2 to the load 150 is controlled to have the value assumed in designing, and thus the distortion of the radio frequency signals RF1 and RF2 may be prevented.
Among components in the second embodiment, the same components as those in the first embodiment are denoted by the same reference numerals, and description thereof is omitted.
For the first embodiment, the case of controlling all of the gain G1 of the path for compensating low impedance and the phase θ1 as well as the gain G2 of the path for compensating high impedance and the phase θ2 has heretofore been described. However, if one or more of these are controlled, a partial effect may be provided.
If only the impedance ZL′ is required to be compensated, the 90-degree shift circuit 4, the transistor Q2, the variable phase control circuit 15, the variable gain control circuit 16, the capacitor 17, and the resistor 18 may be omitted.
An amplifier circuit 1A does not include the 90-degree shift circuit 4, as compared with the amplifier circuit 1 (see
The impedance control circuit 10A does not include the transistor Q2, the variable phase control circuit 15, the variable gain control circuit 16, the capacitor 17, and the resistor 18, as compared with the impedance control circuit 10.
If the impedance ZL′ becomes low, the impedance control circuit 10A outputs the current Iadd1 to the end 3a of the inverter circuit 3. The impedance control circuit 10A may thereby increase the impedance ZL′ and perform control to have the value assumed in designing.
If only a high impedance ZL′ is required to be compensated, the transistor Q1, the variable phase control circuit 11, the variable gain control circuit 12, the capacitor 13, and the resistor 14 may be omitted.
An amplifier circuit 1B includes an impedance control circuit 10B instead of the impedance control circuit 10, as compared with the amplifier circuit 1 (see
The impedance control circuit 10B does not include the transistor Q1, the variable phase control circuit 11, the variable gain control circuit 12, the capacitor 13, and the resistor 14, as compared with the impedance control circuit 10.
If the impedance ZL′ becomes high, the impedance control circuit 10B outputs the current Iadd2 to the different end 3b of the inverter circuit 3. The impedance control circuit 10B may thereby decrease the impedance ZL′ and perform control to have the value assumed in designing.
An amplifier circuit 1C includes an impedance control circuit 10C instead of the impedance control circuit 10, as compared with the amplifier circuit 1 (see
In the circuit simulation in
The waveform 221 is inward of the waveform 200 on the whole. The waveform 221 is downward of the waveform 210 on the whole. That is, it is understood that the return loss is decreased. It is thus understood that the impedance ZL′ approaches the value assumed in designing.
However, near a point 223 and a point 224 where the load phases are respectively 90 degrees and 270 degrees, impedance mismatching in the real part is not decreased, but impedance mismatching in the imaginary part is increased. As the result, the return loss of the inverter circuit 3 is higher than the return loss of the load 150. However, impedance mismatching in a real axis direction (real part) is sufficiently low, and thus it is understood that it is sufficiently practical.
Among components in a third embodiment, the same components as those in any one of the other embodiments are denoted by the same reference numerals, and description thereof is omitted.
In the first and second embodiments, the inverter circuit 3 is the ¼ wavelength line. However, it suffices that in the inverter circuit 3, the diagonal elements of a dependent parameter (see the right side of Formula (3)) is 0 at the operating frequency, and various variations are considered. The diagonal elements is ideally 0 in discussion, and the absolute value of the product of the diagonal elements is only required to be smaller than the absolute value of the product of off-diagonal elements at the used frequency. Circuits having the characteristics as described above will be exemplified and enumerated.
An inverter circuit 3A includes inductors 41 and 42 and a capacitor 43.
An end of the inductor 41 is electrically connected to the end 3a of the inverter circuit 3A. A different end of the inductor 41 is electrically connected to an end of the inductor 42 and an end of the capacitor 43.
A different end of the capacitor 43 is electrically connected to the reference potential.
A different end of the inductor 42 is electrically connected to the different end 3b of the inverter circuit 3A.
The inverter circuit 3A may be considered as a T-type low pass filter.
An inverter circuit 3B includes an inductor 44 and capacitors 45 and 46.
An end of the inductor 44 is electrically connected to the end 3a of the inverter circuit 3B and an end of the capacitor 45. A different end of the inductor 44 is electrically connected to the different end 3b of the inverter circuit 3B and an end of the capacitor 46.
A different end of the capacitor 45 and a different end of the capacitor 46 are electrically connected to the reference potential.
The inverter circuit 3B may be considered as a π-type low pass filter.
An inverter circuit 3C includes capacitors 47 and 48 and an inductor 49.
An end of the capacitor 47 is electrically connected to the end 3a of the inverter circuit 3C. A different end of the capacitor 47 is electrically connected to an end of the capacitor 48 and an end of the inductor 49.
A different end of the inductor 49 is electrically connected to the reference potential.
A different end 3b of the capacitor 48 is electrically connected to the different end of the inverter circuit 3C.
The inverter circuit 3C may be considered as a T-type high pass filter.
An inverter circuit 3D includes a capacitor 50 and inductors 51 and 52.
An end of the capacitor 50 is electrically connected to the end 3a of the inverter circuit 3D and an end of the inductor 51. A different end of the capacitor 50 is electrically connected to the different end 3b of the inverter circuit 3D and an end of the inductor 52.
A different end of the inductor 51 and a different end of the inductor 52 are electrically connected to the reference potential.
The inverter circuit 3D may be considered as a π-type high pass filter.
An inverter circuit 3E includes a first winding 53, a second winding 54, and capacitors 55 and 56.
The first winding 53 and the second winding 54 are electromagnetically coupled.
The capacitor 55 is electrically connected in parallel to the first winding 53.
The capacitor 56 is electrically connected in parallel to the second winding 54.
An end of the first winding 53 and an end of the capacitor 55 are electrically connected to the end 3a of the inverter circuit 3E. A different end of the first winding 53 and a different end of the capacitor 55 are electrically connected to the reference potential.
An end of the second winding 54 and an end of the capacitor 56 are electrically connected to the different end 3b of the inverter circuit 3E. A different end of the second winding 54 and a different end of the capacitor 56 are electrically connected to the reference potential.
The inverter circuit 3E may be considered as a transducer.
As described above, the inverter circuit 3 may be replaced with one of various circuits, and band widening and downsizing are expectable.
Among components in a fourth embodiment, the same components as those in any one of the other embodiments are denoted by the same reference numerals, and description thereof is omitted.
AS long as an inverter circuit is configured to be used as a balun such as the inverter circuit 3E (see
An amplifier circuit 1D includes the inverter circuit 3E instead of the inverter circuit 3, as compared with the amplifier circuit 1 (see
The end of the first winding 53 and the end of the capacitor 55 of the inverter circuit 3E are electrically connected to a first terminal 3c of the inverter circuit 3E. The different end of the first winding 53 and the different end of the capacitor 55 are electrically connected to a second terminal 3d of the inverter circuit 3E.
The end of the second winding 54 of the inverter circuit 3E and the end of the capacitor 56 are electrically connected to a third terminal 3e of the inverter circuit 3E. The different end of the second winding 54 and the different end of the capacitor 56 are electrically connected to a fourth terminal 3f of the inverter circuit 3E.
The first terminal 3c of the inverter circuit 3E is electrically connected to the output terminal of the amplifier 2, and the radio frequency signal RF1 is input thereto. The second terminal 3d of the inverter circuit 3E is electrically connected to the load 150, and the radio frequency signal RF2 is output therefrom.
The third terminal 3e of the inverter circuit 3E is electrically connected to the reference potential. The fourth terminal 3f of the inverter circuit 3E is electrically connected to the collector of the transistor Q2, and the current Iadd2 is input thereto.
A voltage between the third terminal 3e and the fourth terminal 3f of the inverter circuit 3E is the voltage VI2.
The scaler circuit 5 includes a first winding 61, a second winding 62, and capacitors 63 and 64.
An end of the first winding 61 is electrically connected to a first terminal 5a of the scaler circuit 5. A different end of the first winding 61 is electrically connected to an end of the capacitor 63 serving as a DC blocking capacitor.
A different end of the capacitor 63 is electrically connected to a second terminal 5b of the scaler circuit 5.
The end of the second winding 62 and the end of the capacitor 64 are electrically connected to a third terminal 5c of the scaler circuit 5. A different end of the second winding 62 and a different end of the capacitor 64 are electrically connected to a fourth terminal 5d of the scaler circuit 5.
The first terminal 5a and the third terminal 5c of the scaler circuit 5 are electrically connected to the reference potential.
The fourth terminal 5d of the scaler circuit 5 is electrically connected to the collector of the transistor Q1, and the current Iadd1 is input thereto. The second terminal 5b of the scaler circuit 5 is electrically connected to the output terminal of the amplifier 2 and the first terminal 3c of the inverter circuit 3E, and current Iadd1′ is output therefrom.
A voltage between the third terminal 5c and the fourth terminal 5d of the scaler circuit 5 is the voltage VI1.
On the contrary to the inverter circuit 3E, the scaler circuit 5 is a circuit having a larger absolute value of the product of the diagonal elements of the dependent parameter than the absolute value of the product of the off-diagonal elements.
The scaler circuit 5 may be included in the impedance detection circuit 20.
If the current Iadd1 is not high, the scaler circuit 5 may output the current Iadd1′ obtained by multiplying the current Iadd1 by the constant (for example, once or twice) to the first terminal 3c of the inverter circuit 3E.
If the current Iadd1 is sufficiently high, the scaler circuit 5 is not required. It suffices that the collector of the transistor Q1 is electrically connected to the output terminal of the amplifier 2 and the first terminal 3c of the inverter circuit 3E to cause the current Iadd1 to be directly output from the collector of the transistor Q1 to the first terminal 3c of the inverter circuit 3E.
If the voltage VL′ is high, the scaler circuit 5 may decrease the voltage VL′ to one over constant (for example, one second) and output the voltage VL′ to the collector of the transistor Q1 and the detector 21. The scaler circuit 5 may thereby prevent the transistor Q1 from being damaged and change the detectable range of the detector 21.
In the circuit simulation in
With the configuration of the amplifier circuit 1D, it is possible to freely select whether to inject the current Iadd1 and to detect the voltage VI1 on the load 150 side or the amplifier 2 side with respect to the inverter circuit 3E.
Among components in a fifth embodiment, the same components as those in any one of the other embodiments are denoted by the same reference numerals, and description thereof is omitted.
For the first, second, and fourth embodiments, the case where one of the inverter circuit 3 to the inverter circuit 3E is additionally provided closer to the load 150 than to the amplifier 2 has heretofore been described. However, if the amplifier 2 is a Doherty amplifier, one of the inverter circuit 3 to the inverter circuit 3E is included in the Doherty combiner, and the Doherty combiner may also be used for the impedance control.
The amplifier circuit 1E includes a carrier amplifier 6, a peaking amplifier 7, and a Doherty combiner 8 instead of the amplifier 2, as compared with the amplifier circuit 1 (see
The Doherty combiner 8 includes the inverter circuit 3.
Each of the carrier amplifier 6 and the peaking amplifier 7 has two stages; however, the present disclosure is not limited to this. Each of the carrier amplifier 6 and the peaking amplifier 7 may have one stage and may have three or more stages.
The carrier amplifier 6 amplifies the radio frequency signal RFIN and outputs a radio frequency signal RF21 to the end 3a of the inverter circuit 3.
Impedance seen from the carrier amplifier 6 to the load 150 is impedance ZC. An output voltage of the carrier amplifier 6 is a voltage VC, and output current is current IC.
A connection relationship among the carrier amplifier 6, the variable phase control circuit 11, the variable gain control circuit 12, the capacitor 13, the resistor 14, and the transistor Q1 is the same as the connection relationship (see
The inverter circuit 3 receives the radio frequency signal RF21 at the end 3a and outputs a radio frequency signal RF22 from the different end 3b to a node N1.
The peaking amplifier 7 amplifies the radio frequency signal RF3 and outputs a radio frequency signal RF23 to the node N1.
Impedance seen from the peaking amplifier 7 to the load 150 is impedance ZP. An output voltage of the peaking amplifier 7 is a voltage VP, and output current thereof is current IP.
A connection relationship among the peaking amplifier 7, the variable phase control circuit 15, the variable gain control circuit 16, the capacitor 17, the resistor 18, and the transistor Q2 is the same as the connection relationship (see
At the node N1, the radio frequency signal RF22 and the radio frequency signal RF23 are combined, and a radio frequency signal RF24 is generated. The combined radio frequency signal RF24 is output to the load 150.
The inverter circuit 3 is used for combining the radio frequency signal RF22 and the radio frequency signal RF23 and also for controlling impedance, and thereby downsizing may be achieved.
However, in achieving high efficiency, the Doherty amplifier circuit is characterized by variation of the impedance ZC seen from the carrier amplifier 6 to the load 150 due to input power (power of the radio frequency signal RFIN). Accordingly, if the technology in the first, second, and fourth embodiments is simply used for the amplifier circuit 1E, control is performed to have a constant impedance ZC, and thus the efficiency is likely to be deteriorated.
Hence, the control circuit 19 may change the control of the gains G1 and G2 and the control of the bias voltages B1 and B2 according to input power (power of the radio frequency signal RFIN or the radio frequency signal RF3) or output power (power of the radio frequency signals RF21, RF22, or RF24).
Specifically, control as in Formula (8) and Formula (9) below is conceivable as the control of the gains G1 and G2
In Formula (8) and (9), Voffset is a parameter varying with the input power or the output power.
The amplifier circuit 1E may thereby match the impedance ZC seen from the carrier amplifier 6 to the load 150 with different impedance according to the input power or the output power.
Among components in a sixth embodiment, the same components as those in any one of the other embodiments are denoted by the same reference numerals, and description thereof is omitted.
For the fifth embodiment, the case where each of the carrier amplifier 6 and the peaking amplifier 7 has a single-ended output configuration and where the Doherty combiner 8 combines the radio frequency signal RF21 and the radio frequency signal RF23 in parallel has heretofore been described. However, the present disclosure is not limited to this. Each of the carrier amplifier and the peaking amplifier may have a differential output configuration, and the Doherty combiner may combine two differential signals in series.
The amplifier circuit 1F includes carrier amplifiers 6-1 and 6-2 instead of the carrier amplifier 6, as compared with the amplifier circuit 1E (see
The carrier amplifier 6-1 and the carrier amplifier 6-2 form a differential carrier amplifier. The carrier amplifier 6-1 is a positive polarity carrier amplifier. The carrier amplifier 6-2 is a negative polarity carrier amplifier.
The peaking amplifier 7-1 and the peaking amplifier 7-2 form a differential peaking amplifier 7-2. The peaking amplifier 7-1 is a positive polarity peaking amplifier. The peaking amplifier 7-2 is a negative polarity peaking amplifier.
Each of the carrier amplifiers 6-1 and 6-2 as well as the peaking amplifiers 7-1 and 7-2 has two stages; however, the present disclosure is not limited to this. Each of the carrier amplifiers 6-1 and 6-2 as well as the peaking amplifiers 7-1 and 7-2 may have one stage and may have three or more stages.
The balun 71 outputs radio frequency signals RF31 and RF32 constituting a differential signal, based on the radio frequency signal RF3.
The carrier amplifier 6-1 amplifies the radio frequency signal RF31 and outputs a radio frequency signal RF33 to the end of the second winding 62 of the scaler circuit 5.
Impedance seen from the carrier amplifier 6-1 to the load 150 is the impedance ZC. An output voltage of the carrier amplifier 6-1 is the voltage VC, and output current thereof is the current IC.
A connection relationship among the carrier amplifier 6-1, a variable phase control circuit 11-1, a variable gain control circuit 12-1, a capacitor 13-1, a resistor 14-1, and the transistor Q1 is the same as the connection relationship (see
The carrier amplifier 6-2 amplifies a radio frequency signal RF32 and outputs a radio frequency signal RF34 to the different end of the second winding 62 of the scaler circuit 5.
Impedance seen from the carrier amplifier 6-2 to the load 150 is impedance ZC′. An output voltage of the carrier amplifier 6-2 is a voltage VC′, and output current thereof is current IC′.
A connection relationship among the carrier amplifier 6-2, a variable phase control circuit 11-2, a variable gain control circuit 12-2, a capacitor 13-2, a resistor 14-2, and a transistor Q1′ is the same as the connection relationship (see
The balun 72 outputs radio frequency signals RF35 and RF36 constituting a differential signal, based on the radio frequency signal RFIN.
The peaking amplifier 7-1 amplifies the radio frequency signal RF35 and outputs a radio frequency signal RF37 to the end of the first winding 53 of the inverter circuit 3E.
Impedance seen from the peaking amplifier 7-1 to the load 150 is the impedance ZP. An output voltage of the peaking amplifier 7-1 is the voltage VP, and output current thereof is the current IP.
A connection relationship among the peaking amplifier 7-1, a variable phase control circuit 15-1, a variable gain control circuit 16-1, a capacitor 17-1, a resistor 18-1, and the transistor Q2 is the same as the connection relationship (see
The peaking amplifier 7-2 amplifies the radio frequency signal RF36 and outputs a radio frequency signal RF38 to the different end of the first winding 53 of the inverter circuit 3E.
Impedance seen from the peaking amplifier 7-2 to the load 150 is impedance ZP′. An output voltage of the peaking amplifier 7-2 is a voltage VP′, and output current thereof is current IP′.
A connection relationship among the peaking amplifier 7-2, a variable phase control circuit 15-2, a variable gain control circuit 16-2, a capacitor 17-2, a resistor 18-2, and a transistor Q2′ is the same as the connection relationship (see
The end of the second winding 54 of the inverter circuit 3E is electrically connected to the reference potential. The different end of the second winding 54 of the inverter circuit 3E is electrically connected to the end of the first winding 61 of the scaler circuit 5. A radio frequency signal RF39 obtained by combining the differential signal (radio frequency signals RF33 and RF34) and the differential signal (radio frequency signals RF37 and RF38) in series is output from the capacitor 63 of the scaler circuit 5 to the load 150.
In this embodiment, the phase difference detector 23 detects a phase difference (arg(VC)−arg(VP)) between the radio frequency signal RF33 that is an output signal of the positive polarity carrier amplifier 6-1 and the radio frequency signal RF37 that is an output signal of the positive polarity peaking amplifier 7-1; however, the present disclosure is not limited to this. The phase difference detector 23 may detect a phase difference between the radio frequency signal RF34 that is an output signal of the negative polarity carrier amplifier 6-2 and the radio frequency signal RF38 that is an output signal of the negative polarity peaking amplifier 7-2. The phase difference detector 23 may also detect a phase difference between the radio frequency signal RF33 that is the output signal of the positive polarity carrier amplifier 6-1 and the radio frequency signal RF38 that is the output signal of the negative polarity peaking amplifier 7-2. The phase difference detector 23 may also detect a phase difference between the radio frequency signal RF34 that is the output signal of the negative polarity carrier amplifier 6-2 and the radio frequency signal RF37 that is the output signal of the positive polarity peaking amplifier 7-1. The phase difference detector 23 may also average two or more of the phases described above.
Further, the phase difference detector 23 may calculate a phase difference between the carrier side and the peak side by using the amplitude, the phase, or the like of the differential signal (radio frequency signals RF33 and RF34) on the carrier side and the differential signal (radio frequency signals RF37 and RF38) on the peak side.
A phase control signal S1-2 input to the variable phase control circuit 11-2 on the negative polarity side, a gain control signal S2-2 input to the variable gain control circuit 12-2, and a bias control signal S3-2 input to the resistor 14-2 may be respectively same as a phase control signal S1-1 input to the variable phase control circuit 11-1 on the positive polarity side, a gain control signal S2-1 input to the variable gain control circuit 12-1, and a bias control signal S3-1 input to the resistor 14-1; however, the present disclosure is not limited to this.
A gain, a phase difference, and a bias point may be controlled by using a result of comparison between the radio frequency signal RF33 and the radio frequency signal RF34 (for example, comparison between |VC| and |VC′| such as arg(VC)−arg(VC′)). The amplifier circuit 1F may thereby reduce an influence on the differential pair caused by the load variation.
A phase control signal S4-2 input to the variable phase control circuit 15-2, a gain control signal S5-2 input to the variable gain control circuit 16-2, and a bias control signal S6-2 input to the resistor 18-2 are the same as described above.
Among components in a seventh embodiment, the same components as those in any one of the other embodiments are denoted by the same reference numerals, and description thereof is omitted.
The load detection technology in the first to sixth embodiments may be combined with another control technology. For example, a case where a target amplifier is a Doherty amplifier will be described. There is typically a possibility that the characteristics of the Doherty amplifier largely vary (performance deterioration) in response to the load variation, as described above. The amplifier circuit 1F of the sixth embodiment described above may improve the characteristic variation described above but may improve the characteristic variation described above also in the seventh embodiment.
The amplifier circuit 1G includes a first bias circuit 81, as compared with the amplifier circuit 1E (see
Based on the voltage amplitude |VI1| and the voltage amplitude |VI2|, the first bias circuit 81 outputs a bias signal BCD to the base (or the gate) of a first stage amplifier 6a of the carrier amplifier 6 and outputs a bias signal BCF to the base (or the gate) of a final stage amplifier 6b.
Based on the voltage amplitude |VI1| and the voltage amplitude |VI2|, the second bias circuit 82 outputs a bias signal BPD to the base (or the gate) of a first stage amplifier 7a of the peaking amplifier 7 and outputs a bias signal BPF to the base (or the gate) of a final stage amplifier 7b.
Typically, it is known that the characteristic variation in response to the load variation in the Doherty amplifier may be improved by controlling a bias of the base (or the gate) of one or more of amplifiers in respective stages of the carrier amplifier and amplifiers in respective stages of the peaking amplifier. The amplifier circuit 1G controls, in accordance with the load condition, a bias of one or more of the first stage amplifier 6a and the final stage amplifier 6b of the carrier amplifier 6 and the first stage amplifier 7a and the final stage amplifier 7b of the peaking amplifier 7 and thereby may provide a high performance Doherty amplifier even if the load variation occurs.
Hereinafter, control of the amplifier circuit 1G, for example, in a case of low impedance will be described. In a case of high impedance, similar effects are provided by performing control for reverse operations.
Low impedance of the load 150 leads to, for example, |VI2|>|VI1|. In this case, the impedance ZC seen from the carrier amplifier 6 to the load 150 becomes high. If the impedance ZC becomes high, the gain of the carrier amplifier 6 changes to be higher, and saturation power changes to be lower. The amplifier circuit 1G performs control to compensate for this and thereby may prevent the characteristic variation due to the load variation.
Specifically, the first bias circuit 81 decreases the impedance of the bias signals BCD and BCF to have impedance lower than in the case of the assumed impedance (for example, in the case of |VI2|=|VI1|) and prevents the gain of the carrier amplifier 6 from increasing. In addition, the second bias circuit 82 increases the bias signals BPD and BPE to have impedance higher than in the case of the assumed impedance. This causes the peaking amplifier 7 to start, and thus early saturation in the carrier amplifier 6 due to low saturation power of the carrier amplifier 6 may be compensated.
For the seventh embodiment, the case where the amplifier circuit 1G combines the radio frequency signal RF21 and the radio frequency signal RF23 in parallel has heretofore been described; however, the present disclosure is not limited to this. If the amplifier circuit 1G combines the radio frequency signal RF21 and the radio frequency signal RF23 in series, the polarity of a detected voltage and the polarity for bias control are opposite polarities from those in the case of the parallel combination described above.
For a bias point of the peaking amplifier 7, control technology in, for example, U.S. Patent Application Publication No. 2021/0036661 Specification and U.S. Patent Application Publication No. 2016/0241209 Specification may be used. A voltage amplitude comparison result or a voltage phase comparison result is reflected on a bias point of the peaking amplifier 7, and thereby a Doherty amplifier compensated for the load variation may be provided.
An amplifier 91 in
It is understood that the amplifier 91 for impedance control (transistor Q1) is connected in parallel to the final stage amplifier 6b of the carrier amplifier 6.
It is understood that the amplifier 92 for impedance control (transistor Q2) is connected in parallel to the final stage amplifier 7b of the peaking amplifier 7.
Among components in an eighth embodiment, the same components as those in any one of the other embodiments are denoted by the same reference numerals, and description thereof is omitted.
The amplifier circuit 1H includes a variable attenuator 101 and a detector 102 instead of the second bias circuit 82, as compared with the amplifier circuit 1G (see
The variable attenuator 101 attenuates the radio frequency signal RF3 based on a signal S7 and outputs the radio frequency signal RF3 to the detector 102. The signal S7 is a signal representing the drive level of the final stage amplifier 6b of the carrier amplifier 6, and a saturation signal or a load detection signal is exemplified; however, the present disclosure is not limited to this. The signal S7 is also a signal representing the level of the input power (power of the radio frequency signal RFIN). The detector 102 detects a radio frequency signal attenuated by the variable attenuator 101 and outputs the bias signals BPD and BPF respectively to the first stage amplifier 7a and the final stage amplifier 7b.
Even if input power (power of the radio frequency signal RFIN) is not high, the amplifier circuit 1H may perform circuit operations on which the load status is reflected and thus prevent control delay.
An amplifier circuit 1I further includes a drive level detector 111 and an envelope modulation circuit 112, as compared with the amplifier circuit 1H (see
The drive level detector 111 detects the drive level of the final stage amplifier 6b of the carrier amplifier 6 and outputs a signal SDL representing the drive level to the envelope modulation circuit 112. In an example, the drive level detector 111 detects the drive level of the final stage amplifier 6b based on a voltage or current of an amplifying transistor in the final stage amplifier 6b or a voltage or current of the transistor in the first bias circuit 81; however, the present disclosure is not limited to this. The signal SDL is also a signal representing the level of input power (power of the radio frequency signal RFIN).
The envelope modulation circuit 112 outputs the signal S7 to the variable attenuator 101 based on the voltage amplitude |VI1|, the voltage amplitude |VI2|, the phase difference (arg(VI1)−arg(VI2)), and the signal SDL.
With the amplifier circuit 1I, an adaptive Doherty amplifier capable of impedance control may be achieved.
The embodiments described above have been provided for easier understanding of the present disclosure and are not intended to limit the interpretation of the present disclosure. The present disclosure may be changed/improved without necessarily departing from the spirit thereof and includes its equivalents.
Number | Date | Country | Kind |
---|---|---|---|
2022-059840 | Mar 2022 | JP | national |
This is a continuation of International Application No. PCT/JP2023/013286 filed on Mar. 30, 2023 which claims priority from Japanese Patent Application No. 2022-059840 filed on Mar. 31, 2022. The contents of these applications are incorporated herein by reference in their entireties.
Number | Date | Country | |
---|---|---|---|
Parent | PCT/JP2023/013286 | Mar 2023 | WO |
Child | 18888758 | US |