CA2279031C - Sweep pilot technique for a control system that reduces distortion produced by electrical circuits - Google Patents
Sweep pilot technique for a control system that reduces distortion produced by electrical circuits Download PDFInfo
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- CA2279031C CA2279031C CA002279031A CA2279031A CA2279031C CA 2279031 C CA2279031 C CA 2279031C CA 002279031 A CA002279031 A CA 002279031A CA 2279031 A CA2279031 A CA 2279031A CA 2279031 C CA2279031 C CA 2279031C
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- pilot
- electrical circuit
- control system
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Classifications
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- H—ELECTRICITY
- H03—ELECTRONIC CIRCUITRY
- H03L—AUTOMATIC CONTROL, STARTING, SYNCHRONISATION, OR STABILISATION OF GENERATORS OF ELECTRONIC OSCILLATIONS OR PULSES
- H03L7/00—Automatic control of frequency or phase; Synchronisation
-
- H—ELECTRICITY
- H03—ELECTRONIC CIRCUITRY
- H03F—AMPLIFIERS
- H03F1/00—Details of amplifiers with only discharge tubes, only semiconductor devices or only unspecified devices as amplifying elements
- H03F1/32—Modifications of amplifiers to reduce non-linear distortion
- H03F1/3223—Modifications of amplifiers to reduce non-linear distortion using feed-forward
- H03F1/3229—Modifications of amplifiers to reduce non-linear distortion using feed-forward using a loop for error extraction and another loop for error subtraction
- H03F1/3235—Modifications of amplifiers to reduce non-linear distortion using feed-forward using a loop for error extraction and another loop for error subtraction using a pilot signal
Abstract
A control system comprising an electrical circuit that produces distortion where the electrical circuit has a frequency band of operation. A pilot modulated carrier signal is generated and is cause to traverse across the frequency band of operation of the electrical circuit. Information obtained from the traversing pilot modulated carrier signal when it is determined that there is no interference between any signal applied to or generated by the electrical circuit. The information is used by the control system to substantially cancel the distortion.
Description
SWEEP PILOT TECHNIQUE FOR A CONTROL SYSTEM THAT REDUCES
DISTORTION PRODUCED BY ELECTRICAL CIRCUITS
Background of the Invention Field of the Invention The present invention is directed to a control system comprising an electrical circuit that uses a pilot signal to substantially cancel distortion produced by the electrical circuit and more particularly to a technique of traversing or sweeping the pilot signal to across the band of operation of the electrical circuit.
Description of the Related Art Electrical signals when applied to electrical circuits are often distorted as a result of being processed by the circuits. Also electrical circuits generate signals for various useful purposes. The distortion comprises any undesired signals produced by the electrical circuits which are added to or are somehow combined with the applied or generated signals. A well known technique for substantially canceling distortion produced by an electrical circuit uses a control system coupled to the electrical circuit to 2o which a pilot signal is applied. The applied pilot signal is detected by the control system.
The applied pilot signal can have a single spectral component (i.e., one frequency) of a certain amplitude or the applied pilot signal can comprise a plurality of spectral components of various amplitudes. Typically, the applied pilot signal has an amplitude that is at least 60 dB lower than signals applied to or generated by the electrical circuit.
The control system obtains information from the detected pilot signal and uses that information to substantially cancel the distortion produced by the electrical circuit.
A control system comprises at least one circuit which uses external signals or signals generated by the at least one circuit to process signals applied to the at least one 3o circuit. A particular implementation of the technique discussed above is shown in FIG. 1.
FIG. 1 depicts a control system, comprising two feed forward loops (loop l and loop 2) and detection circuit 132. A pilot signal is applied to electrical circuit 108 via coupler 105. Electrical circuit 108 can be any electrical and/or electronic (e.g., Radio Frequency (RF) linear amplifier, power amplifier) circuit. Loop 1 comprises coupler 105, Gain &
Phase circuit 104, splitter 102 and delay circuit 126. Coupler 105 is typically a device which combines two or more input signals and allows access to all or a portion of the combined signal. A coupler is also used to obtain a portion of a signal appearing at its input and output. Gain & Phase circuit 104 is typically a circuit which modifies the amplitude and phase of signals applied to its input based on the values of control signals applied to its control inputs (not shown). Splitter 102 is a circuit with one input and at least two outputs where a signal applied to the input is substantially replicated at the outputs. Delay circuit 126 is typically a circuit which applies a certain amount of delay to a signal applied to its input.
When a signal is applied to the input of the control system (i.e., to sputter 102), the distortion experienced by the applied signal due to electrical circuit 108 is isolated at point A (i.e., path 123). In particular, an input signal is applied to splitter 102. Sputter 102 substantially replicates the input signal on paths 103 and 127. In path 103 the input signal is applied to Gain & Phase circuit 104, coupler 105 and electrical circuit 108. In path 127, the input signal is delayed by delay circuit 126 and then fed to cancellation circuit 124 via path 125. Although not shown, it will be readily understood to those 2o skilled in the art that the amplitude and phase of the input signal on path 125 can be detected (using well known detection circuitry) and converted to control signals that are applied to the control inputs (not shown) of Gain and Phase circuit 104. Using coupler 112, a portion of the input signal (plus any distortion produced by electrical circuit 108) appearing at the output of electrical circuit 108 is fed to cancellation circuit 124 via path 113. Cancellation circuit 124 can be implemented as a combiner circuit which has at least two inputs and one output. A combiner circuit combines signals applied to its inputs and transfers the combined signal to its output. Gain and Phase circuit 104 is adjusted such that the amplitude and phase of the input signal on path 113 are modified resulting in that signal being substantially 180° out of phase (+/- 1 ° ) and relatively the same 3o amplitude (i.e., substantially the inverse) with the input signal on path 125 such that when the two signals are combined by cancellation circuit 124 they substantially cancel each other leaving the distortion (produced by electrical circuit 108) at point A
(path 123).
Thus Loop 1 is designed to isolate the distortion produced by electrical circuit 108.
Loop 2, which comprises delay circuit 114, coupler 116, Gain & Phase circuit 122, and amplifier 120, is designed to use information obtained by Detection circuit 132 from a pilot signal applied to electrical circuit 108 to substantially cancel the distortion produced by electrical circuit 108. In particular, a pilot signal is applied to electrical circuit 108 via coupler 105. The pilot signal (processed by electrical circuit 108) appears on path 115 and at the output of coupler 116, i.e., on path 117. The pilot signal also 1o appears at point A on path 123 after having propagated through path 113 via coupler 112.
A portion of the pilot signal processed by electrical circuit 108 is fed to detection circuit 132 via coupler 130 and path 128. Detection circuit 132 comprises well known circuits (e.g., Log detector/amplifier, Sample & Hold circuit, Null circuit) to detect signal -characteristics (e.g., amplitude) of the pilot signal. Detection circuit 132 detects the amplitude of the input and uses this information to generate control signals on path 131 to cause Gain & Phase circuit 122 to modify the pilot signal. The pilot signal at point A is modified such that the pilot signal appearing on path 118 is substantially the inverse (relatively same amplitude, 180° out of phase, +/- 1 ° ) of the pilot signal appearing on path 115. Amplifier 120 provides additional gain to the output of Gain & Phase circuit 122. The additional gain is calculated such that the signal appearing on path 118 has an amplitude substantially equal to the amplitude of the signal on path 115.
Delay circuit 114 is designed such that the two pilot signals arrive at coupler 116 at substantially the same moment; that is, the two pilot signals are substantially synchronized (aligned in time) to each other. When the two pilot signals are combined by coupler 116 they cancel each other.
Detection circuit 132 now has the information that allows Gain & Phase circuit 122 to modify distortion appearing at point A and thus cancel distortion appearing at the output of electrical circuit 108. When an input signal is applied to the control system, 3o any distortion produced by electrical circuit 108 is isolated at point A
(on path 123) as discussed above. The signal on path 115 is the input signal (processed by electrical circuit 108) plus any distortion produced by electrical circuit 108. The distortion at point A is modified by Gain and Phase circuit 122 based on the information (i.e., signal characteristics) obtained from the previously applied pilot signal so that the distortion on path 129 is substantially the inverse of the distortion on path 115. The distortions on path 115 and path 118 are combined at coupler 116 causing the distortions to substantially cancel each other resulting in an output signal that is substantially free of distortion.
Electrical circuit 108 has a bandwidth that defines a frequency band of operation.
It is desirable that the pilot signal be spectrally located substantially in the middle of the 1o frequency band of operation of electrical circuit 108. However, placing the pilot signal anywhere in the band of operation of electrical circuit 108 causes interference to occur between the input signal and the pilot signal adding more distortion to the input signal.
The interference is any interaction between the pilot signal and an applied or generated signal that adversely affects one or more characteristic (e.g., amplitude, frequency, phase) of the applied or generated signal and/or the pilot signal. Thus, interference not only distorts any signal that is applied or generated by the electrical circuit, but also affects the pilot signal. As discussed above, the pilot signal is typically 60 dB lower than the applied or generated signals and thus would be interfered with by such signals. A
distorted pilot signal provides inaccurate information about the distortion and thus the very purpose of 2o such a pilot signal is defeated. Also, even when the pilot signal is located in the middle of the frequency band of operation, it does not experience the distortions located in other parts (e.g., lower band or upper band) of the frequency band of operation.
What is therefore needed is to use a pilot signal that obtains information about the entire frequency band of operation of the electrical circuit and does so without interfering with any signals applied to or generated by the electrical circuit.
Summary of the Invention The present invention is a control system comprising an electrical circuit that 3o produces distortion where the electrical circuit has a frequency band of operation. A
carrier signal modulated by a pilot signal is applied to the electrical circuit and is traversed across at least a portion of the frequency band of operation of the electrical circuit. As the pilot modulated carrier signal traverses the at least portion of the frequency band of operation of the electrical circuit information about the distortion produced by the electrical circuit is selectively obtained from the pilot signal.
Information about the distortion is not obtained during periods of time when the control system has determined that there is interference between the traversing pilot modulated carrier signal and signals applied to or created by the electrical circuit.
The information obtained is used by the control system to substantially cancel the distortion produced by the electrical circuit.
1o The control system of the present invention also comprises a first feed forward loop and a second feed forward loop coupled to the electrical circuit. The control system of the present invention further comprises a Carrier circuit coupled to a Single Side Band (SSB) modulator which is coupled to the electrical circuit. The control system of the 15 present invention still further comprises a Detection circuit coupled to the carrier circuit and the second feed forward loop. The Carrier circuit is configured to generate a traversable carrier signal. The SSB modulator is configured to generate a single side band pilot signal and to modulate the carrier with the single side band pilot.
The Carrier circuit is further configured to cause the pilot modulated carrier signal to traverse at least 2o a portion of the frequency band of operation of the electrical circuit without interference from any signal applied to or generated by the electrical circuit. As the pilot modulated carrier signal traverses the at least portion of the frequency band of operation, the Detection circuit selectively obtains information about the distortion produced by the electrical circuit and provides the information to the second feed forward loop. The first 25 feed forward loop is configured to isolate the distortion produced by the electrical circuit.
The second feed forward loop is configured to use the information obtained by the Detection circuit to substantially cancel the distortion produced by the electrical circuit.
Brief Description of the Drawings FIG. 1 depicts a control system comprising two feed forward loops and detection circuitry;
FIG. 2 depicts a control system of the present invention;
FIG. 3 depicts the frequency response of the electrical circuit of the control system of the present invention, a pilot modulated carrier and the direction in which the pilot modulated carrier signal traverses.
1o Detailed Description Referring to FIG. 2, there is shown a control system of the present invention comprising electrical circuit 108 coupled to a first feed forward loop (i.e., loop 1) and a second feed forward loop (i.e., loop 2). The control system of the present invention further comprises Carrier circuit 171 coupled to Single Side Band (SSB) modulator 188 and to Detection circuit 191. Electrical circuit 108 produces distortion which is isolated at point A by loop 1. Loop 2 uses information obtained from Detection circuit 191 to cancel the distortion produced by electrical circuit 108. The information obtained by Detection circuit 191 is gleaned from a pilot modulated carrier signal applied to electrical 2o circuit 108 (via path 146 and coupler 105) with the use of carrier circuit 171 and Single Side Band modulator 188. Carrier circuit 171 and SSB modulator 188 cause the pilot modulated Garner signal to traverse the frequency band of operation of electrical circuit 108. As the pilot modulated carrier signal traverses the frequency band of operation of electrical circuit 108, Detection circuit 191 obtains information from the pilot only when Detection circuit 191 determines that there is substantially no interference between the traversing pilot modulated carrier signal and any signal applied to or generated by electrical circuit 108.
Referring to FIG. 3, there is shown a frequency response (300) of electrical circuit 108 with a spectral component (306) representing the pilot modulated carrier signal. The frequency response is a chart or graph showing how a particular characteristic (e.g., amplitude, phase) of an electrical circuit corresponds with frequency. The frequency band of operation is a range of frequencies within which electrical circuit 108 processes and/or generates signals. The boundaries of the frequency band of operation are defined by lower frequency f L and upper frequency f ~ . Frequencies f L and f ~
correspond to the points (302, 304) at which the frequency response is 3 dB below its maximum amplitude response (0 dB). Typically the bandwidth of a circuit is defined by the frequencies that correspond to its 3 dB points. The frequency band of operation need not be the bandwidth. Pilot modulated Garner signal 306 initially starts at a location (f, ) outside the frequency band of operation and then traverses the frequency band of to operation or at least a portion of the band in the direction shown by arrow 308. It should be noted that the particular frequency response shown is for illustrative purposes only and that electrical circuit 108 is not limited to frequency response 300. Also, pilot modulated carrier signal 306 need not initially start at a location (fl ) proximate to fL . Pilot modulated carrier signal 306 can, for example, start at a location (frequency fF ) proximate to fU and traverse the frequency band of operation in a direction opposite that of arrow 308.
Referring again to FIG. 2, Carrier circuit 171 comprises Sweep Generator 166 coupled to Voltage Controlled Oscillator (VCO) 164 which is coupled to Sputter 162.
2o Each of the outputs of Splitter 162 is coupled to an amplifier ( 160, 170).
One of the outputs is applied to Mixer 172 and the other output is applied to SSB
modulator 188.
Sweep Generator 166 produces a varying voltage signal. VCO 164 generates a carrier (i.e., a sinusoid) whose frequency is varied in direct correspondence to a varying voltage.
As the voltage generated by Sweep Generator 166 increases (or decreases), the frequency of the carrier increases (or decreases). Thus, the Carrier circuit 171 generates a carrier signal of varying frequency.
SSB modulator 188 is a well known circuit shown here comprising Oscillator 148, 90° Phase circuit 150, Band pass Filters (BPF) 152, 153 and balanced modulator 154. Oscillator 148 generates a pilot signal (e.g., a square wave) of a certain frequency that is applied to 90° Phase circuit 150. 90° Phase circuit 150 divides the frequency of the square wave to a desired frequency and generates two square waves having that same desired frequency but which are 90° out of phase with each other. Each of the signals is applied to a Band pass filter (152, 153) having a pass band that allow certain frequency components of the signals to pass through their circuitry virtually unaffected. It is well known that a square wave comprises many frequency components. The square wave generated by Oscillator 148 is converted to a sinusoid by BPF 152 and 153 because many of the frequency components of the square wave are filtered out by BPF 152 and 153.
Band pass filters 152 and 153 are well known filter circuits that allow signals that fall 1o within their pass band to pass through virtually unaffected and filter out (or significantly attenuate) signals having frequencies that fall outside of their pass bands.
The pass band is a frequency (or group of frequencies) about which the Band pass filter frequency response is tuned. The outputs of the Band pass filters 152 and 153 are applied to balance modulator 154. The output of Carrier circuit 171 is also applied to balanced modulator 154 (via path 158). Balanced modulator uses the pilot signal to modulate the carrier signal. Typically, when a carrier signal is modulated, other signals having frequencies commonly referred to as side band frequencies are created as a result of the modulation. The side band frequencies are frequencies that are higher and lower than the frequency of the carrier by an equal amount. Because of the 90° phase relationship 2o between the pilot signals applied to balanced modulator 154, one of the side bands of the resulting pilot modulated carrier signal is effectively suppressed. The output of SSB
modulator 188 is the carrier signal shifted in frequency by an amount equal to the frequency of the pilot signal, and thus the output is a pilot modulated carrier signal.
2s The pilot modulated carrier signal is applied to electrical circuit 108 and appears on path 117. A portion of the pilot modulated carrier signal is coupled to path 128 via coupler 130. The pilot modulated carrier signal is applied to Mixer 172 via amplifier 168. An output of carrier circuit 171 is also applied to Mixer 172. Mixer 172 is a well known circuit having at least two inputs and at least one output where the output is the 3o result of the two input signals being multiplied to each other. It is well known that when two signals having certain frequencies are mixed, the result are signals comprising frequencies which are the sum and difference of the frequencies of the two signals. The mixing of two signals having the same frequencies is known as synchronous detection.
Therefore, the pilot modulated carrier signal is synchronously detected by Mixer 172 and the output of Mixer 172 is fed to BPF 174 whose center frequency is equal to the frequency of the pilot signal. The output of BPF 174 is therefore the pilot signal.
The pilot signal is applied to Log Detector 176 which detects a characteristic (e.g., amplitude) of the pilot signal and converts said characteristic to a voltage.
Therefore, as the pilot modulated carrier signal traverses the frequency band of operation of electrical to circuit 108, a corresponding signal (e.g., a voltage) is derived at the output of Log Detector 178. The signal is applied to path 179 and thus one input of Comparator 178.
The signal is also applied to Low Pass Filter (LPF) 180 through switch 180.
acts as an averaging circuit and generates an average of a characteristic (e.g., amplitude) of the detected pilot signal which contains information about the pilot signal. The average is applied to Null circuit 132 via switch 184 and Buffer amplifier 186. Buffer amplifier 186 has two outputs one of which is fed back to an input of Comparator 178.
When the traversing pilot modulated carrier signal interferes with a signal applied to or generated by electrical circuit 108, the output of Log Detector 176 and thus the input on path 179 of Comparator 178 increases.
2o causing Comparator 178 to open switches 182 and 184 preventing LPF 180 from performing any averaging and from providing any such average to Null circuit 132.
Comparator 178 is a circuit that compares the amplitude of the signals at its input and generates a voltage based on the relative amplitude of its input signals.
When the amplitude of the input signal on path 179 is greater than the amplitude of the signal on path 181, Comparator 178 generates a control voltage on path 190 that causes switches 182 and 184 to open. When the switches open the averaging being performed by LPF
180 is stopped. When amplitude of the input signal on path 179 is equal to or below that of the signal on path 181, Comparator 178 closes switches 182 and 184 and LPF
3o continues its averaging and provides its output to Null circuit 132.
Therefore, Detection circuit 191 does not obtain information from the applied pilot signal when Detection circuit 191 has determined that a signal applied to or generated by electrical circuit 108 is interfering with the pilot signal.
Null circuit 132 generates control signals on path 131 upon receipt of a control 5 signal from Sweep Generator 166 via path 134. Sweep Generator 166 thus determines when Null circuit 132 uses the information obtained from Detection circuit 191. Sweep generator 166 can generate its control signals after the pilot modulated carrier signal has traversed a portion of the frequency band of operation or has traversed the entire frequency band of operation at least once or a number of times. The control signals to generated by Null circuit 132 cause Gain & Phase amplifier 122 to modify the distortion at point A such that it is canceled with distortion appearing on path 115 with the use of coupler 116.
DISTORTION PRODUCED BY ELECTRICAL CIRCUITS
Background of the Invention Field of the Invention The present invention is directed to a control system comprising an electrical circuit that uses a pilot signal to substantially cancel distortion produced by the electrical circuit and more particularly to a technique of traversing or sweeping the pilot signal to across the band of operation of the electrical circuit.
Description of the Related Art Electrical signals when applied to electrical circuits are often distorted as a result of being processed by the circuits. Also electrical circuits generate signals for various useful purposes. The distortion comprises any undesired signals produced by the electrical circuits which are added to or are somehow combined with the applied or generated signals. A well known technique for substantially canceling distortion produced by an electrical circuit uses a control system coupled to the electrical circuit to 2o which a pilot signal is applied. The applied pilot signal is detected by the control system.
The applied pilot signal can have a single spectral component (i.e., one frequency) of a certain amplitude or the applied pilot signal can comprise a plurality of spectral components of various amplitudes. Typically, the applied pilot signal has an amplitude that is at least 60 dB lower than signals applied to or generated by the electrical circuit.
The control system obtains information from the detected pilot signal and uses that information to substantially cancel the distortion produced by the electrical circuit.
A control system comprises at least one circuit which uses external signals or signals generated by the at least one circuit to process signals applied to the at least one 3o circuit. A particular implementation of the technique discussed above is shown in FIG. 1.
FIG. 1 depicts a control system, comprising two feed forward loops (loop l and loop 2) and detection circuit 132. A pilot signal is applied to electrical circuit 108 via coupler 105. Electrical circuit 108 can be any electrical and/or electronic (e.g., Radio Frequency (RF) linear amplifier, power amplifier) circuit. Loop 1 comprises coupler 105, Gain &
Phase circuit 104, splitter 102 and delay circuit 126. Coupler 105 is typically a device which combines two or more input signals and allows access to all or a portion of the combined signal. A coupler is also used to obtain a portion of a signal appearing at its input and output. Gain & Phase circuit 104 is typically a circuit which modifies the amplitude and phase of signals applied to its input based on the values of control signals applied to its control inputs (not shown). Splitter 102 is a circuit with one input and at least two outputs where a signal applied to the input is substantially replicated at the outputs. Delay circuit 126 is typically a circuit which applies a certain amount of delay to a signal applied to its input.
When a signal is applied to the input of the control system (i.e., to sputter 102), the distortion experienced by the applied signal due to electrical circuit 108 is isolated at point A (i.e., path 123). In particular, an input signal is applied to splitter 102. Sputter 102 substantially replicates the input signal on paths 103 and 127. In path 103 the input signal is applied to Gain & Phase circuit 104, coupler 105 and electrical circuit 108. In path 127, the input signal is delayed by delay circuit 126 and then fed to cancellation circuit 124 via path 125. Although not shown, it will be readily understood to those 2o skilled in the art that the amplitude and phase of the input signal on path 125 can be detected (using well known detection circuitry) and converted to control signals that are applied to the control inputs (not shown) of Gain and Phase circuit 104. Using coupler 112, a portion of the input signal (plus any distortion produced by electrical circuit 108) appearing at the output of electrical circuit 108 is fed to cancellation circuit 124 via path 113. Cancellation circuit 124 can be implemented as a combiner circuit which has at least two inputs and one output. A combiner circuit combines signals applied to its inputs and transfers the combined signal to its output. Gain and Phase circuit 104 is adjusted such that the amplitude and phase of the input signal on path 113 are modified resulting in that signal being substantially 180° out of phase (+/- 1 ° ) and relatively the same 3o amplitude (i.e., substantially the inverse) with the input signal on path 125 such that when the two signals are combined by cancellation circuit 124 they substantially cancel each other leaving the distortion (produced by electrical circuit 108) at point A
(path 123).
Thus Loop 1 is designed to isolate the distortion produced by electrical circuit 108.
Loop 2, which comprises delay circuit 114, coupler 116, Gain & Phase circuit 122, and amplifier 120, is designed to use information obtained by Detection circuit 132 from a pilot signal applied to electrical circuit 108 to substantially cancel the distortion produced by electrical circuit 108. In particular, a pilot signal is applied to electrical circuit 108 via coupler 105. The pilot signal (processed by electrical circuit 108) appears on path 115 and at the output of coupler 116, i.e., on path 117. The pilot signal also 1o appears at point A on path 123 after having propagated through path 113 via coupler 112.
A portion of the pilot signal processed by electrical circuit 108 is fed to detection circuit 132 via coupler 130 and path 128. Detection circuit 132 comprises well known circuits (e.g., Log detector/amplifier, Sample & Hold circuit, Null circuit) to detect signal -characteristics (e.g., amplitude) of the pilot signal. Detection circuit 132 detects the amplitude of the input and uses this information to generate control signals on path 131 to cause Gain & Phase circuit 122 to modify the pilot signal. The pilot signal at point A is modified such that the pilot signal appearing on path 118 is substantially the inverse (relatively same amplitude, 180° out of phase, +/- 1 ° ) of the pilot signal appearing on path 115. Amplifier 120 provides additional gain to the output of Gain & Phase circuit 122. The additional gain is calculated such that the signal appearing on path 118 has an amplitude substantially equal to the amplitude of the signal on path 115.
Delay circuit 114 is designed such that the two pilot signals arrive at coupler 116 at substantially the same moment; that is, the two pilot signals are substantially synchronized (aligned in time) to each other. When the two pilot signals are combined by coupler 116 they cancel each other.
Detection circuit 132 now has the information that allows Gain & Phase circuit 122 to modify distortion appearing at point A and thus cancel distortion appearing at the output of electrical circuit 108. When an input signal is applied to the control system, 3o any distortion produced by electrical circuit 108 is isolated at point A
(on path 123) as discussed above. The signal on path 115 is the input signal (processed by electrical circuit 108) plus any distortion produced by electrical circuit 108. The distortion at point A is modified by Gain and Phase circuit 122 based on the information (i.e., signal characteristics) obtained from the previously applied pilot signal so that the distortion on path 129 is substantially the inverse of the distortion on path 115. The distortions on path 115 and path 118 are combined at coupler 116 causing the distortions to substantially cancel each other resulting in an output signal that is substantially free of distortion.
Electrical circuit 108 has a bandwidth that defines a frequency band of operation.
It is desirable that the pilot signal be spectrally located substantially in the middle of the 1o frequency band of operation of electrical circuit 108. However, placing the pilot signal anywhere in the band of operation of electrical circuit 108 causes interference to occur between the input signal and the pilot signal adding more distortion to the input signal.
The interference is any interaction between the pilot signal and an applied or generated signal that adversely affects one or more characteristic (e.g., amplitude, frequency, phase) of the applied or generated signal and/or the pilot signal. Thus, interference not only distorts any signal that is applied or generated by the electrical circuit, but also affects the pilot signal. As discussed above, the pilot signal is typically 60 dB lower than the applied or generated signals and thus would be interfered with by such signals. A
distorted pilot signal provides inaccurate information about the distortion and thus the very purpose of 2o such a pilot signal is defeated. Also, even when the pilot signal is located in the middle of the frequency band of operation, it does not experience the distortions located in other parts (e.g., lower band or upper band) of the frequency band of operation.
What is therefore needed is to use a pilot signal that obtains information about the entire frequency band of operation of the electrical circuit and does so without interfering with any signals applied to or generated by the electrical circuit.
Summary of the Invention The present invention is a control system comprising an electrical circuit that 3o produces distortion where the electrical circuit has a frequency band of operation. A
carrier signal modulated by a pilot signal is applied to the electrical circuit and is traversed across at least a portion of the frequency band of operation of the electrical circuit. As the pilot modulated carrier signal traverses the at least portion of the frequency band of operation of the electrical circuit information about the distortion produced by the electrical circuit is selectively obtained from the pilot signal.
Information about the distortion is not obtained during periods of time when the control system has determined that there is interference between the traversing pilot modulated carrier signal and signals applied to or created by the electrical circuit.
The information obtained is used by the control system to substantially cancel the distortion produced by the electrical circuit.
1o The control system of the present invention also comprises a first feed forward loop and a second feed forward loop coupled to the electrical circuit. The control system of the present invention further comprises a Carrier circuit coupled to a Single Side Band (SSB) modulator which is coupled to the electrical circuit. The control system of the 15 present invention still further comprises a Detection circuit coupled to the carrier circuit and the second feed forward loop. The Carrier circuit is configured to generate a traversable carrier signal. The SSB modulator is configured to generate a single side band pilot signal and to modulate the carrier with the single side band pilot.
The Carrier circuit is further configured to cause the pilot modulated carrier signal to traverse at least 2o a portion of the frequency band of operation of the electrical circuit without interference from any signal applied to or generated by the electrical circuit. As the pilot modulated carrier signal traverses the at least portion of the frequency band of operation, the Detection circuit selectively obtains information about the distortion produced by the electrical circuit and provides the information to the second feed forward loop. The first 25 feed forward loop is configured to isolate the distortion produced by the electrical circuit.
The second feed forward loop is configured to use the information obtained by the Detection circuit to substantially cancel the distortion produced by the electrical circuit.
Brief Description of the Drawings FIG. 1 depicts a control system comprising two feed forward loops and detection circuitry;
FIG. 2 depicts a control system of the present invention;
FIG. 3 depicts the frequency response of the electrical circuit of the control system of the present invention, a pilot modulated carrier and the direction in which the pilot modulated carrier signal traverses.
1o Detailed Description Referring to FIG. 2, there is shown a control system of the present invention comprising electrical circuit 108 coupled to a first feed forward loop (i.e., loop 1) and a second feed forward loop (i.e., loop 2). The control system of the present invention further comprises Carrier circuit 171 coupled to Single Side Band (SSB) modulator 188 and to Detection circuit 191. Electrical circuit 108 produces distortion which is isolated at point A by loop 1. Loop 2 uses information obtained from Detection circuit 191 to cancel the distortion produced by electrical circuit 108. The information obtained by Detection circuit 191 is gleaned from a pilot modulated carrier signal applied to electrical 2o circuit 108 (via path 146 and coupler 105) with the use of carrier circuit 171 and Single Side Band modulator 188. Carrier circuit 171 and SSB modulator 188 cause the pilot modulated Garner signal to traverse the frequency band of operation of electrical circuit 108. As the pilot modulated carrier signal traverses the frequency band of operation of electrical circuit 108, Detection circuit 191 obtains information from the pilot only when Detection circuit 191 determines that there is substantially no interference between the traversing pilot modulated carrier signal and any signal applied to or generated by electrical circuit 108.
Referring to FIG. 3, there is shown a frequency response (300) of electrical circuit 108 with a spectral component (306) representing the pilot modulated carrier signal. The frequency response is a chart or graph showing how a particular characteristic (e.g., amplitude, phase) of an electrical circuit corresponds with frequency. The frequency band of operation is a range of frequencies within which electrical circuit 108 processes and/or generates signals. The boundaries of the frequency band of operation are defined by lower frequency f L and upper frequency f ~ . Frequencies f L and f ~
correspond to the points (302, 304) at which the frequency response is 3 dB below its maximum amplitude response (0 dB). Typically the bandwidth of a circuit is defined by the frequencies that correspond to its 3 dB points. The frequency band of operation need not be the bandwidth. Pilot modulated Garner signal 306 initially starts at a location (f, ) outside the frequency band of operation and then traverses the frequency band of to operation or at least a portion of the band in the direction shown by arrow 308. It should be noted that the particular frequency response shown is for illustrative purposes only and that electrical circuit 108 is not limited to frequency response 300. Also, pilot modulated carrier signal 306 need not initially start at a location (fl ) proximate to fL . Pilot modulated carrier signal 306 can, for example, start at a location (frequency fF ) proximate to fU and traverse the frequency band of operation in a direction opposite that of arrow 308.
Referring again to FIG. 2, Carrier circuit 171 comprises Sweep Generator 166 coupled to Voltage Controlled Oscillator (VCO) 164 which is coupled to Sputter 162.
2o Each of the outputs of Splitter 162 is coupled to an amplifier ( 160, 170).
One of the outputs is applied to Mixer 172 and the other output is applied to SSB
modulator 188.
Sweep Generator 166 produces a varying voltage signal. VCO 164 generates a carrier (i.e., a sinusoid) whose frequency is varied in direct correspondence to a varying voltage.
As the voltage generated by Sweep Generator 166 increases (or decreases), the frequency of the carrier increases (or decreases). Thus, the Carrier circuit 171 generates a carrier signal of varying frequency.
SSB modulator 188 is a well known circuit shown here comprising Oscillator 148, 90° Phase circuit 150, Band pass Filters (BPF) 152, 153 and balanced modulator 154. Oscillator 148 generates a pilot signal (e.g., a square wave) of a certain frequency that is applied to 90° Phase circuit 150. 90° Phase circuit 150 divides the frequency of the square wave to a desired frequency and generates two square waves having that same desired frequency but which are 90° out of phase with each other. Each of the signals is applied to a Band pass filter (152, 153) having a pass band that allow certain frequency components of the signals to pass through their circuitry virtually unaffected. It is well known that a square wave comprises many frequency components. The square wave generated by Oscillator 148 is converted to a sinusoid by BPF 152 and 153 because many of the frequency components of the square wave are filtered out by BPF 152 and 153.
Band pass filters 152 and 153 are well known filter circuits that allow signals that fall 1o within their pass band to pass through virtually unaffected and filter out (or significantly attenuate) signals having frequencies that fall outside of their pass bands.
The pass band is a frequency (or group of frequencies) about which the Band pass filter frequency response is tuned. The outputs of the Band pass filters 152 and 153 are applied to balance modulator 154. The output of Carrier circuit 171 is also applied to balanced modulator 154 (via path 158). Balanced modulator uses the pilot signal to modulate the carrier signal. Typically, when a carrier signal is modulated, other signals having frequencies commonly referred to as side band frequencies are created as a result of the modulation. The side band frequencies are frequencies that are higher and lower than the frequency of the carrier by an equal amount. Because of the 90° phase relationship 2o between the pilot signals applied to balanced modulator 154, one of the side bands of the resulting pilot modulated carrier signal is effectively suppressed. The output of SSB
modulator 188 is the carrier signal shifted in frequency by an amount equal to the frequency of the pilot signal, and thus the output is a pilot modulated carrier signal.
2s The pilot modulated carrier signal is applied to electrical circuit 108 and appears on path 117. A portion of the pilot modulated carrier signal is coupled to path 128 via coupler 130. The pilot modulated carrier signal is applied to Mixer 172 via amplifier 168. An output of carrier circuit 171 is also applied to Mixer 172. Mixer 172 is a well known circuit having at least two inputs and at least one output where the output is the 3o result of the two input signals being multiplied to each other. It is well known that when two signals having certain frequencies are mixed, the result are signals comprising frequencies which are the sum and difference of the frequencies of the two signals. The mixing of two signals having the same frequencies is known as synchronous detection.
Therefore, the pilot modulated carrier signal is synchronously detected by Mixer 172 and the output of Mixer 172 is fed to BPF 174 whose center frequency is equal to the frequency of the pilot signal. The output of BPF 174 is therefore the pilot signal.
The pilot signal is applied to Log Detector 176 which detects a characteristic (e.g., amplitude) of the pilot signal and converts said characteristic to a voltage.
Therefore, as the pilot modulated carrier signal traverses the frequency band of operation of electrical to circuit 108, a corresponding signal (e.g., a voltage) is derived at the output of Log Detector 178. The signal is applied to path 179 and thus one input of Comparator 178.
The signal is also applied to Low Pass Filter (LPF) 180 through switch 180.
acts as an averaging circuit and generates an average of a characteristic (e.g., amplitude) of the detected pilot signal which contains information about the pilot signal. The average is applied to Null circuit 132 via switch 184 and Buffer amplifier 186. Buffer amplifier 186 has two outputs one of which is fed back to an input of Comparator 178.
When the traversing pilot modulated carrier signal interferes with a signal applied to or generated by electrical circuit 108, the output of Log Detector 176 and thus the input on path 179 of Comparator 178 increases.
2o causing Comparator 178 to open switches 182 and 184 preventing LPF 180 from performing any averaging and from providing any such average to Null circuit 132.
Comparator 178 is a circuit that compares the amplitude of the signals at its input and generates a voltage based on the relative amplitude of its input signals.
When the amplitude of the input signal on path 179 is greater than the amplitude of the signal on path 181, Comparator 178 generates a control voltage on path 190 that causes switches 182 and 184 to open. When the switches open the averaging being performed by LPF
180 is stopped. When amplitude of the input signal on path 179 is equal to or below that of the signal on path 181, Comparator 178 closes switches 182 and 184 and LPF
3o continues its averaging and provides its output to Null circuit 132.
Therefore, Detection circuit 191 does not obtain information from the applied pilot signal when Detection circuit 191 has determined that a signal applied to or generated by electrical circuit 108 is interfering with the pilot signal.
Null circuit 132 generates control signals on path 131 upon receipt of a control 5 signal from Sweep Generator 166 via path 134. Sweep Generator 166 thus determines when Null circuit 132 uses the information obtained from Detection circuit 191. Sweep generator 166 can generate its control signals after the pilot modulated carrier signal has traversed a portion of the frequency band of operation or has traversed the entire frequency band of operation at least once or a number of times. The control signals to generated by Null circuit 132 cause Gain & Phase amplifier 122 to modify the distortion at point A such that it is canceled with distortion appearing on path 115 with the use of coupler 116.
Claims (3)
1. A control system comprising an electrical circuit (108) that produces distortion where the electrical circuit has a frequency band of operation and where a pilot signal is applied to the electrical circuit and the pilot signal is used by the control system to substantially cancel the distortion, the control system CHARACTERIZED BY:
a Carrier circuit (171) configured to generate a traversable carrier signal (306) modulated by the pilot signal which pilot modulated carrier signal is caused by the Carrier circuit to traverse at least a portion of the frequency band of operation of the electrical circuit allowing the control system to selectively obtain information from the traversable pilot modulated carrier signal that is used by the control system to substantially cancel the distortion.
a Carrier circuit (171) configured to generate a traversable carrier signal (306) modulated by the pilot signal which pilot modulated carrier signal is caused by the Carrier circuit to traverse at least a portion of the frequency band of operation of the electrical circuit allowing the control system to selectively obtain information from the traversable pilot modulated carrier signal that is used by the control system to substantially cancel the distortion.
2. The control system of claim 1 further CHARACTERIZED BY a Single Side Band modulator (188) configured to generate the pilot signal, the Single Side Band modulator being coupled to the Carrier circuit uses the pilot signal to modulate the traversable carrier.
3. The control system of claim 1 further CHARACTERIZED BY a Detection circuit (191) coupled to the control system and configured to obtain information from the traversable pilot modulated carrier signal during time periods in which the Detection circuit has determined that there is no interference between the traversable pilot modulated carrier and any signal applied to or generated by the electrical circuit.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/162,697 | 1998-09-29 | ||
| US09/162,697 US5926067A (en) | 1998-09-29 | 1998-09-29 | Sweep pilot technique for a control system that reduces distortion produced by electrical circuits |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2279031A1 CA2279031A1 (en) | 2000-03-29 |
| CA2279031C true CA2279031C (en) | 2002-01-22 |
Family
ID=22586752
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002279031A Expired - Fee Related CA2279031C (en) | 1998-09-29 | 1999-07-29 | Sweep pilot technique for a control system that reduces distortion produced by electrical circuits |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US5926067A (en) |
| EP (1) | EP0991182B1 (en) |
| JP (1) | JP2000124838A (en) |
| KR (1) | KR100552251B1 (en) |
| CN (1) | CN1250254A (en) |
| AU (1) | AU764137B2 (en) |
| BR (1) | BR9904249A (en) |
| CA (1) | CA2279031C (en) |
| DE (1) | DE69940587D1 (en) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6411644B1 (en) * | 1998-09-29 | 2002-06-25 | Lucent Technologies Inc. | Frequency hop pilot technique for a control system that reduces distortion produced by electrical circuits |
| US6157254A (en) * | 1998-09-29 | 2000-12-05 | Lucent Technologies Inc. | Double side band pilot technique for a control system that reduces distortion produced by electrical circuits |
| US6198346B1 (en) * | 1998-11-18 | 2001-03-06 | At&T Corp. | Adaptive linear amplifier without output power loss |
| US6359507B1 (en) * | 1999-08-18 | 2002-03-19 | Lucent Technologies Inc. | Method and apparatus for an automatic predistortion system |
| US6392481B1 (en) * | 1999-11-30 | 2002-05-21 | Nokia Networks Oy | Method and apparatus for improved fed forward amplification |
| JP3533351B2 (en) * | 1999-12-28 | 2004-05-31 | 日本無線株式会社 | Feed forward amplifier and control circuit thereof |
| US6320461B1 (en) * | 2000-05-12 | 2001-11-20 | Jhong Sam Lee | Ultra-linear feedforward RF power amplifier |
| US6340915B1 (en) * | 2000-11-20 | 2002-01-22 | Soma Networks, Inc. | Feed forward amplifier |
| US7053702B2 (en) * | 2000-11-20 | 2006-05-30 | Soma Networks, Inc. | Feed forward amplifier |
| CN1300935C (en) * | 2001-06-11 | 2007-02-14 | 松下电器产业株式会社 | Method and circuit for control of feedforward distortion compensation amplifier |
| US6614298B2 (en) | 2001-08-13 | 2003-09-02 | Soma Networks, Inc. | Apparatus and method for controlling adaptive circuits |
| US6677817B2 (en) | 2001-12-17 | 2004-01-13 | Powerwave Technologies, Inc. | Feed forward amplifier with amplifier stage failure detection using pilot tones |
| US6556076B1 (en) | 2001-12-17 | 2003-04-29 | Powerwave Technologies, Inc. | Feed forward amplifier with amplifier stage failure detection using pilot tones |
| US8474359B2 (en) * | 2009-10-01 | 2013-07-02 | Colleen Clinger George | Grape cutter |
| CN102811072B (en) * | 2012-07-26 | 2014-06-04 | 京信通信系统（广州）有限公司 | Signal transmission method and device |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5307022A (en) * | 1991-04-15 | 1994-04-26 | Motorola, Inc. | High dynamic range modulation independent feed forward amplifier network |
| US5130663A (en) * | 1991-04-15 | 1992-07-14 | Motorola, Inc. | Feed forward amplifier network with frequency swept pilot tone |
| US5485120A (en) * | 1994-07-28 | 1996-01-16 | Aval Communications Inc. | Feed-forward power amplifier system with adaptive control and control method |
| US5528196A (en) * | 1995-01-06 | 1996-06-18 | Spectrian, Inc. | Linear RF amplifier having reduced intermodulation distortion |
| US5796304A (en) * | 1996-04-24 | 1998-08-18 | Powerwave Technologies, Inc. | Broadband amplifier with quadrature pilot signal |
| US5923214A (en) * | 1997-12-17 | 1999-07-13 | Motorola, Inc. | Feedforward amplifier network with swept pilot tone for reducing distortion generated by a power amplifier |
-
1998
- 1998-09-29 US US09/162,697 patent/US5926067A/en not_active Expired - Lifetime
-
1999
- 1999-07-29 CA CA002279031A patent/CA2279031C/en not_active Expired - Fee Related
- 1999-09-20 BR BR9904249-5A patent/BR9904249A/en not_active Application Discontinuation
- 1999-09-21 DE DE69940587T patent/DE69940587D1/en not_active Expired - Lifetime
- 1999-09-21 EP EP99307440A patent/EP0991182B1/en not_active Expired - Lifetime
- 1999-09-22 AU AU48884/99A patent/AU764137B2/en not_active Ceased
- 1999-09-27 JP JP11272058A patent/JP2000124838A/en active Pending
- 1999-09-28 CN CN99120769A patent/CN1250254A/en active Pending
- 1999-09-29 KR KR1019990041780A patent/KR100552251B1/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| DE69940587D1 (en) | 2009-04-30 |
| JP2000124838A (en) | 2000-04-28 |
| CA2279031A1 (en) | 2000-03-29 |
| CN1250254A (en) | 2000-04-12 |
| KR100552251B1 (en) | 2006-02-15 |
| AU4888499A (en) | 2000-03-30 |
| EP0991182B1 (en) | 2009-03-18 |
| KR20000023531A (en) | 2000-04-25 |
| AU764137B2 (en) | 2003-08-14 |
| BR9904249A (en) | 2000-08-29 |
| EP0991182A2 (en) | 2000-04-05 |
| EP0991182A3 (en) | 2001-11-14 |
| US5926067A (en) | 1999-07-20 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKLA | Lapsed |
Effective date: 20130730 |