CA1333922C - Phase controlled demodulation system for digital communication - Google Patents
Phase controlled demodulation system for digital communicationInfo
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- CA1333922C CA1333922C CA000616675A CA616675A CA1333922C CA 1333922 C CA1333922 C CA 1333922C CA 000616675 A CA000616675 A CA 000616675A CA 616675 A CA616675 A CA 616675A CA 1333922 C CA1333922 C CA 1333922C
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Abstract
A phase controlled demodulation system for digital communication includes a quadrature detector for receiving a modulated digital signal and generating therefrom a pair of I
and Q demodulated signals. A phase difference detection and filter circuit detects a phase difference between the I and Q
demodulated signals, and another circuit detects a carrier-to-noise ratio of one of the I and Q demodulated signals. A
further circuit detects a ratio difference between the detected carrier-to-noise ratio and a predetermined value, and a voltage controlled oscillator responsive to the detected phase difference and the detected ratio difference generates a carrier as a replica of the carrier of the received digital signal and applies the carrier to the quadrature detector.
and Q demodulated signals. A phase difference detection and filter circuit detects a phase difference between the I and Q
demodulated signals, and another circuit detects a carrier-to-noise ratio of one of the I and Q demodulated signals. A
further circuit detects a ratio difference between the detected carrier-to-noise ratio and a predetermined value, and a voltage controlled oscillator responsive to the detected phase difference and the detected ratio difference generates a carrier as a replica of the carrier of the received digital signal and applies the carrier to the quadrature detector.
Description
- l - 1333922 This application is a divisional of Canadian patent application serial No. 570,052 filed on June 22, 1988 in the name of NEC Corporation.
BACKGROUND OF THE INVENTION
The present invention relates to a phase controlled demodulation system, and more specifically to a pseudo sync detector circuit which is capable of detecting when a demodulator that provides synchronous detection of an input signal, using a carrier recovered from the input signal, is in a pseudo sync state or pseudo locked state, and preventing such conditions.
A prior art demodulator circuit comprises a voltage controlled oscillator, a quadrature demodulator which receives an input PSK (phase shift keying) signal fed through an input terminal and provides quadrature detection of the PSK signal using the output signal of the voltage controlled oscillator, and a phase detection and filtering circuit for detecting the phase difference between the two output signals of the quadrature demodulator and supplies a control signal in accordance with the detected phase difference to the voltage controlled oscillator.
With this circuit arrangement, a carrier loop is formed to cause the voltage controlled oscillator to recover the carrier of the PSK signal and the quadrature demodulator supplies the two output signals as demodulated signals to two output terminals, respectively. As a result, this demodulator circuit can be considered as a carrier recovery circuit in the sense that it recovers the carrier of the received signal, and more correctly it should be called a demodulator circuit in a wider sense of the word.
When the frequency of the input PSK signal is in the locking range of the carrier loop, this demodulator circuit is said to be in a locked stage (normal lock or sync state) and the recovered carrier is controlled so that its frequency is maintained at a value equal to the frequency of the carrier of the PSK signal. However, if the input frequency goes beyond the lock range of the loop to such a degree that there is a frequency difference ~f which is given by fs/N (where fs is the signal speed and N is a positive integer), the recovered carrier no longer coincides with the frequency of the input PSK signal and becomes stabilized outside the lock range although the loop is in a process for pulling it into the lock range. This phenomenon is called "pseudo locked state".
For this reason, the prior art demodulator circuit is designed to have a narrow lock range to prevent pseudo lock. As a result, when the input PSK signal suffers a sudden change in frequency it is impossible to keep or bring the circuit in a sync state.
In applications, where such a demodulator circuit is used in a transmission system having large frequency variations, a pilot signal is exchanged between the opposite ends of the system and an automatic frequency control circuit is provided to control the voltage controlled oscillator in accordance with the pilot signal.
However, the automatic frequency control circuit, which is external to the loop, is complex and costly.
SUMMARY OF THE INVENTION
The object of the present invention is to provide a new ` 1333~22 71024-92D
and improved phase controlled demodulation system which is capable of detecting when a demodulator that provides synchronous detection, using a carrier recovered from an input signal, is in a pseudo sync state or pseudo locked state, and preventing the demodulator from falling into such conditions.
- It is found that the carrier-to-noise (C/N) ratio of a demodulator output will vary with a deviation of the frequency of the carrier recovered by the demodulator from the frequency of the received carrier. A carrier-to-noise ratio detector, in accordance with the present invention, can therefore be used instead of the costly automatic frequency control circuit for preventing the demodulator from being locked in a pseudo sync state. This is accomplished by controlling the voltage controlled oscillator provided in a closed loop of the demodulator in accordance with the derived C/N ratio such that the latter is maintained at a maximum level.
In accordance with the invention, there is provided a phase controlled demodulation system for digital communication, comprising: a quadrature detector for receiving a modulated digital signal and generating therefrom a pair of I and Q
demodulated signals; a phase difference detection and filter circuit for detecting a phase difference between said I and Q
demodulated signals; means for detecting a carrier-to-noise ratio of one of said I and Q demodulated signals; means for detecting a ratio difference between the detected carrier-to-noise ratio and a predetermined value; and a voltage controlled oscillator responsive to the detected phase difference and the detected ratio difference for generating a carrier as a replica of the carrier of said received digital signal and applying said carrier to said quadrature detector.
BRIEF DESCRIPTION OF THE DRAWINGS
The present invention will be described in further detail with reference to the accompanying drawings, in which:
Figure 1 is a block diagram of a carrier-to-noise detector according to a first embodiment of the present invention;
Figure 2 is a circuit diagram of the absolute value circuit of Figure l;
Figure 3 is a circuit diagram of the delay circuit of Figure 1;
Figure 4 is a circuit diagram of the C/N ratio divider of Figure l;
Figure 5 is a graphic illustration of the probability density distribution of noise at various noise levels;
Figure 6 is a graphic illustration of Eb/No values measured by the detector of Figure 1 as a function of input Eb/No values for comparison with theoretical Eb/No values;
Figure 7 is a block diagram of the carrier-to-noise ratio detector according to a second embodiment of the invention;
Figure 8 is a circuit diagram of the polarity inverter of Figure 6;
Figure 9 is a graphic illustration of Eb/No values measured by the detector of Figure 7 as a function of input Eb/No values for comparison with theoretical Eb/No values;
Figure 10 is a block diagram of the carrier-to-noise detector according to a third embodiment of the present invention;
13339~2 71024-92D
Figure 11 is a circuit diagram of the weighting circuit of Figure 10;
Figures 12a and 12b are graphic illustrationsof the probability density distributions of noise components derived respectively from the outputs of absolute value circuit and weighting circuit of Figure 10;
Figure 13 is a graphic illustration of Eb/No values measured by the detector of Figure 10 as a function of input Eb/No values for comparison with theoretical Eb/No values; and Figure 14 is a block diagram of a pseudo sync detector circuit in accordance with the invention.
DETAILED DESCRIPTION
Referring to Figure 1, there is shown a C/N ratio detector according to a first embodiment of the present invention.
The C/N detector comprises an analog-to-digital converter 1 which is connected to receive a demodulated 2-PSK signal from a demodulator, not shown, and driven at a clock rate used to recover symbols by the demodulator for sampling the demodulated signal at the recovered symbol rate. An absolute value circuit 2 is connected to the output of the A/D converter to convert the negative value of the digital output to a positive value and supplies an absolute value signal to a first averaging circuit 3 the output of which is connected to a first squaring circuit 4 to produce an output representing the carrier component value C.
The output of A/D converter 1 is further applied to a second squaring circuit 5 to which a second averaging circuit 6 is connected to produce an output representing the total component value (C + N). A subtractor 7 is connected to the outputs of the circuits 4 and 6 to subtract the output of squaring circuit 4 from the output of averaging circuit 6 to obtain the noise component value N. A division circuit 8 is connected to the output of squaring circuit 4 and to the output of the subtractor 7 to determine the ratio C/N.
More specifically, the output of the demodulator is an analog signal having eye patterns at the recovery timing of symbols which corresponds to signal points. A/D converter 1 converts the sampled value into n-bit digital data stream di (where i = 0, 1, 2, ...., n). If n is three, data bit stream di can be represented as shown in Table 1. This data bit stream is applied to the absolute value circuit 2 as well as to the second squaring circuit 5.
Absolute value circuit 2 converts the data di into an absolute value ¦di¦. As shown in Figure 2, the absolute value circuit 2 comprises an n-bit polarity inverter 12 and an (n+l)-bit adder 13. If n=3, polarity inverter 12 comprises exclusive OR
gates 12-1, 12-2 and 12-3 each having a first input terminal connected to the most significant bit (MSB) position output of A/D converter 1 and a second input terminal connected to a respective bit position output of A/D converter 1. The polarity inverter 12 inverts the logic state of the input of each exclusive OR gate when the MSB is at logic 1 and applies the inverted bits to adder 13, while it passes the inputs of all the exclusive OR gates to adder 13 without altering their logic states when the MSB is at logic 0. Adder 13 adds MSB of the 3-bit inputs from A/D converter 1 to the least significant bit (LSB) of the 3-bit inputs from the polarity inverter 12 and produces 1333~22 4-bit outputs. As a result, absolute values shown in Table 2 are derived.
Outputs o_ A/D Conv. 1 O
nJ
Outputs of A.V. Circuit 2 00:
00:
0~
O
O
0~ :.
Averaging circuit 3 averages the absolute values for a period of N symbols which is sufficiently long to suppress short term variations and applies an average value to squaring circuit 4. As shown in Figure 3, averaging circuit 3 comprises an adder 14 connected to the output of averaging circuit 2, a one-sample delay 15 which is reset at N-symbol intervals and connected between the output of the adder 14 and a second input of the adder 15. Adder 14 and delay 15 form an integrator for integrat-ing N symbols which is divided by a division circuit 16 by a constant N. Since the noise component contained in digital data has a Gaussian distribution centered on an amplitude A at zero noise level, the noise component is cancelled out by the averaging process just described, and therefore, the output of averaging circuit 3 gives the amplitude of a signal point of the demodulated signal under noiseless conditions and is represented by Equation (1) .
Nl_o I i I (1) Therefore, the output of squaring circuit 4 supplies a noiseless carrier component C, or the signal power S, which can be represented by:
S = A (2) Since the noise component has a Gaussian distribution with respect to the amplitude A at a noiseless signal point, the noise component power ~2 is given by:
BACKGROUND OF THE INVENTION
The present invention relates to a phase controlled demodulation system, and more specifically to a pseudo sync detector circuit which is capable of detecting when a demodulator that provides synchronous detection of an input signal, using a carrier recovered from the input signal, is in a pseudo sync state or pseudo locked state, and preventing such conditions.
A prior art demodulator circuit comprises a voltage controlled oscillator, a quadrature demodulator which receives an input PSK (phase shift keying) signal fed through an input terminal and provides quadrature detection of the PSK signal using the output signal of the voltage controlled oscillator, and a phase detection and filtering circuit for detecting the phase difference between the two output signals of the quadrature demodulator and supplies a control signal in accordance with the detected phase difference to the voltage controlled oscillator.
With this circuit arrangement, a carrier loop is formed to cause the voltage controlled oscillator to recover the carrier of the PSK signal and the quadrature demodulator supplies the two output signals as demodulated signals to two output terminals, respectively. As a result, this demodulator circuit can be considered as a carrier recovery circuit in the sense that it recovers the carrier of the received signal, and more correctly it should be called a demodulator circuit in a wider sense of the word.
When the frequency of the input PSK signal is in the locking range of the carrier loop, this demodulator circuit is said to be in a locked stage (normal lock or sync state) and the recovered carrier is controlled so that its frequency is maintained at a value equal to the frequency of the carrier of the PSK signal. However, if the input frequency goes beyond the lock range of the loop to such a degree that there is a frequency difference ~f which is given by fs/N (where fs is the signal speed and N is a positive integer), the recovered carrier no longer coincides with the frequency of the input PSK signal and becomes stabilized outside the lock range although the loop is in a process for pulling it into the lock range. This phenomenon is called "pseudo locked state".
For this reason, the prior art demodulator circuit is designed to have a narrow lock range to prevent pseudo lock. As a result, when the input PSK signal suffers a sudden change in frequency it is impossible to keep or bring the circuit in a sync state.
In applications, where such a demodulator circuit is used in a transmission system having large frequency variations, a pilot signal is exchanged between the opposite ends of the system and an automatic frequency control circuit is provided to control the voltage controlled oscillator in accordance with the pilot signal.
However, the automatic frequency control circuit, which is external to the loop, is complex and costly.
SUMMARY OF THE INVENTION
The object of the present invention is to provide a new ` 1333~22 71024-92D
and improved phase controlled demodulation system which is capable of detecting when a demodulator that provides synchronous detection, using a carrier recovered from an input signal, is in a pseudo sync state or pseudo locked state, and preventing the demodulator from falling into such conditions.
- It is found that the carrier-to-noise (C/N) ratio of a demodulator output will vary with a deviation of the frequency of the carrier recovered by the demodulator from the frequency of the received carrier. A carrier-to-noise ratio detector, in accordance with the present invention, can therefore be used instead of the costly automatic frequency control circuit for preventing the demodulator from being locked in a pseudo sync state. This is accomplished by controlling the voltage controlled oscillator provided in a closed loop of the demodulator in accordance with the derived C/N ratio such that the latter is maintained at a maximum level.
In accordance with the invention, there is provided a phase controlled demodulation system for digital communication, comprising: a quadrature detector for receiving a modulated digital signal and generating therefrom a pair of I and Q
demodulated signals; a phase difference detection and filter circuit for detecting a phase difference between said I and Q
demodulated signals; means for detecting a carrier-to-noise ratio of one of said I and Q demodulated signals; means for detecting a ratio difference between the detected carrier-to-noise ratio and a predetermined value; and a voltage controlled oscillator responsive to the detected phase difference and the detected ratio difference for generating a carrier as a replica of the carrier of said received digital signal and applying said carrier to said quadrature detector.
BRIEF DESCRIPTION OF THE DRAWINGS
The present invention will be described in further detail with reference to the accompanying drawings, in which:
Figure 1 is a block diagram of a carrier-to-noise detector according to a first embodiment of the present invention;
Figure 2 is a circuit diagram of the absolute value circuit of Figure l;
Figure 3 is a circuit diagram of the delay circuit of Figure 1;
Figure 4 is a circuit diagram of the C/N ratio divider of Figure l;
Figure 5 is a graphic illustration of the probability density distribution of noise at various noise levels;
Figure 6 is a graphic illustration of Eb/No values measured by the detector of Figure 1 as a function of input Eb/No values for comparison with theoretical Eb/No values;
Figure 7 is a block diagram of the carrier-to-noise ratio detector according to a second embodiment of the invention;
Figure 8 is a circuit diagram of the polarity inverter of Figure 6;
Figure 9 is a graphic illustration of Eb/No values measured by the detector of Figure 7 as a function of input Eb/No values for comparison with theoretical Eb/No values;
Figure 10 is a block diagram of the carrier-to-noise detector according to a third embodiment of the present invention;
13339~2 71024-92D
Figure 11 is a circuit diagram of the weighting circuit of Figure 10;
Figures 12a and 12b are graphic illustrationsof the probability density distributions of noise components derived respectively from the outputs of absolute value circuit and weighting circuit of Figure 10;
Figure 13 is a graphic illustration of Eb/No values measured by the detector of Figure 10 as a function of input Eb/No values for comparison with theoretical Eb/No values; and Figure 14 is a block diagram of a pseudo sync detector circuit in accordance with the invention.
DETAILED DESCRIPTION
Referring to Figure 1, there is shown a C/N ratio detector according to a first embodiment of the present invention.
The C/N detector comprises an analog-to-digital converter 1 which is connected to receive a demodulated 2-PSK signal from a demodulator, not shown, and driven at a clock rate used to recover symbols by the demodulator for sampling the demodulated signal at the recovered symbol rate. An absolute value circuit 2 is connected to the output of the A/D converter to convert the negative value of the digital output to a positive value and supplies an absolute value signal to a first averaging circuit 3 the output of which is connected to a first squaring circuit 4 to produce an output representing the carrier component value C.
The output of A/D converter 1 is further applied to a second squaring circuit 5 to which a second averaging circuit 6 is connected to produce an output representing the total component value (C + N). A subtractor 7 is connected to the outputs of the circuits 4 and 6 to subtract the output of squaring circuit 4 from the output of averaging circuit 6 to obtain the noise component value N. A division circuit 8 is connected to the output of squaring circuit 4 and to the output of the subtractor 7 to determine the ratio C/N.
More specifically, the output of the demodulator is an analog signal having eye patterns at the recovery timing of symbols which corresponds to signal points. A/D converter 1 converts the sampled value into n-bit digital data stream di (where i = 0, 1, 2, ...., n). If n is three, data bit stream di can be represented as shown in Table 1. This data bit stream is applied to the absolute value circuit 2 as well as to the second squaring circuit 5.
Absolute value circuit 2 converts the data di into an absolute value ¦di¦. As shown in Figure 2, the absolute value circuit 2 comprises an n-bit polarity inverter 12 and an (n+l)-bit adder 13. If n=3, polarity inverter 12 comprises exclusive OR
gates 12-1, 12-2 and 12-3 each having a first input terminal connected to the most significant bit (MSB) position output of A/D converter 1 and a second input terminal connected to a respective bit position output of A/D converter 1. The polarity inverter 12 inverts the logic state of the input of each exclusive OR gate when the MSB is at logic 1 and applies the inverted bits to adder 13, while it passes the inputs of all the exclusive OR gates to adder 13 without altering their logic states when the MSB is at logic 0. Adder 13 adds MSB of the 3-bit inputs from A/D converter 1 to the least significant bit (LSB) of the 3-bit inputs from the polarity inverter 12 and produces 1333~22 4-bit outputs. As a result, absolute values shown in Table 2 are derived.
Outputs o_ A/D Conv. 1 O
nJ
Outputs of A.V. Circuit 2 00:
00:
0~
O
O
0~ :.
Averaging circuit 3 averages the absolute values for a period of N symbols which is sufficiently long to suppress short term variations and applies an average value to squaring circuit 4. As shown in Figure 3, averaging circuit 3 comprises an adder 14 connected to the output of averaging circuit 2, a one-sample delay 15 which is reset at N-symbol intervals and connected between the output of the adder 14 and a second input of the adder 15. Adder 14 and delay 15 form an integrator for integrat-ing N symbols which is divided by a division circuit 16 by a constant N. Since the noise component contained in digital data has a Gaussian distribution centered on an amplitude A at zero noise level, the noise component is cancelled out by the averaging process just described, and therefore, the output of averaging circuit 3 gives the amplitude of a signal point of the demodulated signal under noiseless conditions and is represented by Equation (1) .
Nl_o I i I (1) Therefore, the output of squaring circuit 4 supplies a noiseless carrier component C, or the signal power S, which can be represented by:
S = A (2) Since the noise component has a Gaussian distribution with respect to the amplitude A at a noiseless signal point, the noise component power ~2 is given by:
2 1 ~ ( ¦ d ¦ -A) 2 (3) i=O
By substituting Equation (1) into Equation (3), the following relation is obtained:
N-1d 2 2 N L _o i A ( 4 ) On the other hand, the output of A/D converter 1 is squared by second squaring circuit 5 and averaged over N symbols by the second averaging circuit 6 in a manner similar to the 20 processes performed by averaging circuit 3 and squaring circuit 4 just described. As a result, the first term of Equation (4) can be obtained at the output of averaging circuit 6, namely, ~ + A . Subtractor 7 subtracts the signal power A at the output of squaring circuit 4 from the (~ + A ) output of 1 3 3 3 9 ~ 2 71024-92D
averaging circuit 6 to derive a noise power a which is used by division circuit 8 to divide the output A2 of squaring circuit 4.
As shown in Figure 4, division circuit 8 comprises a conversion table, or a read only memory 17. A set of values S/a2 are stored in cell locations addressable as a function of variables S and a2.
Although satisfactory for most applications, the first embodiment is not suited for systems severely affected by noise.
As shown in Figure 5, the probability density distribution of a received 2-PSK signal adopts a curve 40 which is a Gaussian distribution under low noise conditions. Thus, the polarity inversion of the negative values by absolute value circuit 2 causes the signal point with amplitude -A to be folded over to the signal point with amplitude A, while maintaining the symmetry of the curve 40. However, under high noise conditions, there is an increase in variance a2 of the Gaussian distribution and the probability density distribution of the received signal adopts a curve as shown at 41. Therefore, the fold-over effect of the absolute value circuit 2 will result in a distribution curve 42 under high noise conditions with the result that the average value of the amplitudes of received signal is shifted to a signal point with an amplitude A'. The amount of this error increases with increase in noise. As shown in Figure 6, Eb/No ratios measured with the circuit of Figure 1 show increasing discrepancy from theoretical values as the input Eb/No ratio decreases.
A second embodiment of the present invention is shown in Figure 7. This embodiment eliminates the disadvantage of the 1 3 3 3 ~ ~ 2 71024-92D
first embodiment by taking advantage of the forward error coding and decoding techniques employed in digital transmission systems.
Instead of using the absolute value circuit 2 of Figure 1, the second embodiment includes a delay 20 connected to the output of A/D converter 1, an FEC (forward error correcting) decoder 21 for decoding the output of A/D converter 1 and correcting errors and feeding an FEC encoder 22. The output of encoder 22 is connected to one input of a polarity inverter 23 to which the output of delay 20 is also applied. Polarity inverter 23 supplies a decision threshold to the first averaging circuit 3.
FEC decoder 21 performs error decoding operation on the output of A/D converter 1 by correcting errors according to a known error correcting to application to the FEC encoder of a transmitter, not shown. This signal is applied to FEC encoder 22 in the same way as the transmitter's FEC encoder. With the error decoding and encoding processes, the output of FEC encoder 22 can be considered more akin to the output of the transmitter's FEC encoder than the output of the receiver's demodulator is to it. Therefore, a binary 1 at the output of encoder 22 indicates that the received input signal is at a signal point having an amplitude A in a probability density distribution of amplitudes (Figure 5) and a binary 0 at the encoder output indicates that the input signal is at a signal point with an amplitude -A.
The output of A/D converter 1 is delayed by circuit 20 by an amount equal to the total delay introduced by decoder 21 and encoder 22 so that the inputs to the polarity inverter 23 are rendered time-coincident with each other.
33~922 Polarity inverter 23 uses the output of FEC encoder 22 as a criterion to determine whether the output of the delay 20 lies at a signal point having an amplitude A or at a signal point having an amplitude -A. In response to a binary 1 from encoder 22, polarity inverter 23 applies the output from delay 20 without altering its polarity to averaging circuit 3 and in response to a binary 0, it applies the output of delay 20 to averaging circuit 3 by inverting its polarity. As shown in Figure 8, polarity inverter 23 comprises a NOT circuit 30 connected to the output of FEC encoder 22, exclusive OR gates 31-1 to 31-n, and an adder 32. Each exclusive OR gate 31 has a first input terminal connected to the output of the NOT circuit 30 and a second input terminal connected to a respective one of the n outputs of the delay circuit 20. Since the output of delay 20 is represented by 2's complements of the n-bit data, binary 0 at the output of encoder 22 causes the logic states of the outputs of delay 20 to be inverted by exclusive OR gates 31-1 through 31-n and summed with a binary 1 from inverter 30 which is summed by adder 32 with the LSB of the n-bit outputs from exclusive OR gates 31, while a binary 1 at the output of encoder 22 causes the delay 20 outputs to pass through gates 31 to adder 32 without undergoing polarity inversion.
As a result of this polarity inversion process, the probability density distribution of the demodulated signal is centered on the signal point having amplitude A and adopts the curve 40 of Figure 5 and the average value of the amplitudes of the received signal rendered equal to the amplitude at the signal point with amplitude A.
1~ 3 3 ~ 2 2 71024-92D
In this embodiment, the output of the first squaring circuit 4 can be expressed by the following equation:
~lN-l \2 S = ~N ~oSGN ( i) where, SGN (di) represents the criterion data from FEC encoder 22.
Figure 9 is a graphic representation of the relationship between the Eb/No values obtained by circuit of Figure 7 and theoretical Eb/No values. As is apparent, there is a complete agreement between the measured and theoretical values down to low Eb/No input values. This indicates that C/N ratio can be precisely determined even if the transmission system suffers severe noise.
To allow accurate determination of C/N ratio, the use of a powerful error correcting algorithm such as soft decision Viterbi decoding algorithm or convolutional decoding techniques is preferred.
Measurement of C/N ratio of a system without interrupt-ing its service can also be effected alternatively by a third embodiment shown in Figure 10. This embodiment differs from the first embodiment by the inclusion of an adaptive weighting circuit 50.
Since the probability density distribution of the amplitudes of the received signal adopts a curve A (see Figure 12a) at low noise levels and a curve B at high noise levels (Figure 12b), at low noise levels the averaged absolute values of amplitudes becomes approximately equal to the amplitude at 13 3 3 ~ 2 2 71024-92D
the signal point S. However, at high noise levels, the averaged absolute values result in an asymmetrical curve C with respect to point S.
The absolute value of the output of A/D converter 1 is taken by absolute value circuit 2 and weighted with a prescribed weighting factor by the adaptive weighting circuit 50.
Let S(t) represent the signal component of a received signal and N(t) the noise component. Since noise component has a Gaussian distribution, an average value N(t) of noise components N(t) can be regarded as being equal to zero, namely N(t) = 0. The output signal of the adaptive weighting circuit 50 is applied to the first averaging circuit 3 where short term variations, i.e., noise component N(t) are removed to produce an output ¦S(t)¦W(u), where W(u) represents the weighting factor, and u = ¦S(t) + N(t)¦.
Therefore, the output signal of the first squaring circuit 4 is given by S(t) W(u) . This signal is applied to the subtractor 7 and division circuit 8.
By the squaring and averaging operations by the squaring circuit 5 and the average circuit 6 on the output {S(t) + N(t)} of A/D converter 1, the input signal applied from averaging circuit 6 to the subtractor 7 is given by the following relation:
{S(t)+N(t)}2 S(t)2+N(t)2+2S(t)N(t) S(t)2+N(t)2+2S(t)N(t) (6) Since N(t)=0, the third term of Equation (6) becomes zero and so Equation (6) can be rewritten as:
- 14 - 1333~22 {S(t)+N(t)} =S(t) +N(t) (7) This weighting factor is determined so that the adverse fold-over effect produced by taking the absolute values is minimized. The following conditions are examples of weighting factor in which the value x represents the output of the absolute value circuit 2 and TH is a threshold value.
(1) W(x)=x (2) W(x)=l x >TH
=0 x <TH
By substituting Equation (1) into Equation (3), the following relation is obtained:
N-1d 2 2 N L _o i A ( 4 ) On the other hand, the output of A/D converter 1 is squared by second squaring circuit 5 and averaged over N symbols by the second averaging circuit 6 in a manner similar to the 20 processes performed by averaging circuit 3 and squaring circuit 4 just described. As a result, the first term of Equation (4) can be obtained at the output of averaging circuit 6, namely, ~ + A . Subtractor 7 subtracts the signal power A at the output of squaring circuit 4 from the (~ + A ) output of 1 3 3 3 9 ~ 2 71024-92D
averaging circuit 6 to derive a noise power a which is used by division circuit 8 to divide the output A2 of squaring circuit 4.
As shown in Figure 4, division circuit 8 comprises a conversion table, or a read only memory 17. A set of values S/a2 are stored in cell locations addressable as a function of variables S and a2.
Although satisfactory for most applications, the first embodiment is not suited for systems severely affected by noise.
As shown in Figure 5, the probability density distribution of a received 2-PSK signal adopts a curve 40 which is a Gaussian distribution under low noise conditions. Thus, the polarity inversion of the negative values by absolute value circuit 2 causes the signal point with amplitude -A to be folded over to the signal point with amplitude A, while maintaining the symmetry of the curve 40. However, under high noise conditions, there is an increase in variance a2 of the Gaussian distribution and the probability density distribution of the received signal adopts a curve as shown at 41. Therefore, the fold-over effect of the absolute value circuit 2 will result in a distribution curve 42 under high noise conditions with the result that the average value of the amplitudes of received signal is shifted to a signal point with an amplitude A'. The amount of this error increases with increase in noise. As shown in Figure 6, Eb/No ratios measured with the circuit of Figure 1 show increasing discrepancy from theoretical values as the input Eb/No ratio decreases.
A second embodiment of the present invention is shown in Figure 7. This embodiment eliminates the disadvantage of the 1 3 3 3 ~ ~ 2 71024-92D
first embodiment by taking advantage of the forward error coding and decoding techniques employed in digital transmission systems.
Instead of using the absolute value circuit 2 of Figure 1, the second embodiment includes a delay 20 connected to the output of A/D converter 1, an FEC (forward error correcting) decoder 21 for decoding the output of A/D converter 1 and correcting errors and feeding an FEC encoder 22. The output of encoder 22 is connected to one input of a polarity inverter 23 to which the output of delay 20 is also applied. Polarity inverter 23 supplies a decision threshold to the first averaging circuit 3.
FEC decoder 21 performs error decoding operation on the output of A/D converter 1 by correcting errors according to a known error correcting to application to the FEC encoder of a transmitter, not shown. This signal is applied to FEC encoder 22 in the same way as the transmitter's FEC encoder. With the error decoding and encoding processes, the output of FEC encoder 22 can be considered more akin to the output of the transmitter's FEC encoder than the output of the receiver's demodulator is to it. Therefore, a binary 1 at the output of encoder 22 indicates that the received input signal is at a signal point having an amplitude A in a probability density distribution of amplitudes (Figure 5) and a binary 0 at the encoder output indicates that the input signal is at a signal point with an amplitude -A.
The output of A/D converter 1 is delayed by circuit 20 by an amount equal to the total delay introduced by decoder 21 and encoder 22 so that the inputs to the polarity inverter 23 are rendered time-coincident with each other.
33~922 Polarity inverter 23 uses the output of FEC encoder 22 as a criterion to determine whether the output of the delay 20 lies at a signal point having an amplitude A or at a signal point having an amplitude -A. In response to a binary 1 from encoder 22, polarity inverter 23 applies the output from delay 20 without altering its polarity to averaging circuit 3 and in response to a binary 0, it applies the output of delay 20 to averaging circuit 3 by inverting its polarity. As shown in Figure 8, polarity inverter 23 comprises a NOT circuit 30 connected to the output of FEC encoder 22, exclusive OR gates 31-1 to 31-n, and an adder 32. Each exclusive OR gate 31 has a first input terminal connected to the output of the NOT circuit 30 and a second input terminal connected to a respective one of the n outputs of the delay circuit 20. Since the output of delay 20 is represented by 2's complements of the n-bit data, binary 0 at the output of encoder 22 causes the logic states of the outputs of delay 20 to be inverted by exclusive OR gates 31-1 through 31-n and summed with a binary 1 from inverter 30 which is summed by adder 32 with the LSB of the n-bit outputs from exclusive OR gates 31, while a binary 1 at the output of encoder 22 causes the delay 20 outputs to pass through gates 31 to adder 32 without undergoing polarity inversion.
As a result of this polarity inversion process, the probability density distribution of the demodulated signal is centered on the signal point having amplitude A and adopts the curve 40 of Figure 5 and the average value of the amplitudes of the received signal rendered equal to the amplitude at the signal point with amplitude A.
1~ 3 3 ~ 2 2 71024-92D
In this embodiment, the output of the first squaring circuit 4 can be expressed by the following equation:
~lN-l \2 S = ~N ~oSGN ( i) where, SGN (di) represents the criterion data from FEC encoder 22.
Figure 9 is a graphic representation of the relationship between the Eb/No values obtained by circuit of Figure 7 and theoretical Eb/No values. As is apparent, there is a complete agreement between the measured and theoretical values down to low Eb/No input values. This indicates that C/N ratio can be precisely determined even if the transmission system suffers severe noise.
To allow accurate determination of C/N ratio, the use of a powerful error correcting algorithm such as soft decision Viterbi decoding algorithm or convolutional decoding techniques is preferred.
Measurement of C/N ratio of a system without interrupt-ing its service can also be effected alternatively by a third embodiment shown in Figure 10. This embodiment differs from the first embodiment by the inclusion of an adaptive weighting circuit 50.
Since the probability density distribution of the amplitudes of the received signal adopts a curve A (see Figure 12a) at low noise levels and a curve B at high noise levels (Figure 12b), at low noise levels the averaged absolute values of amplitudes becomes approximately equal to the amplitude at 13 3 3 ~ 2 2 71024-92D
the signal point S. However, at high noise levels, the averaged absolute values result in an asymmetrical curve C with respect to point S.
The absolute value of the output of A/D converter 1 is taken by absolute value circuit 2 and weighted with a prescribed weighting factor by the adaptive weighting circuit 50.
Let S(t) represent the signal component of a received signal and N(t) the noise component. Since noise component has a Gaussian distribution, an average value N(t) of noise components N(t) can be regarded as being equal to zero, namely N(t) = 0. The output signal of the adaptive weighting circuit 50 is applied to the first averaging circuit 3 where short term variations, i.e., noise component N(t) are removed to produce an output ¦S(t)¦W(u), where W(u) represents the weighting factor, and u = ¦S(t) + N(t)¦.
Therefore, the output signal of the first squaring circuit 4 is given by S(t) W(u) . This signal is applied to the subtractor 7 and division circuit 8.
By the squaring and averaging operations by the squaring circuit 5 and the average circuit 6 on the output {S(t) + N(t)} of A/D converter 1, the input signal applied from averaging circuit 6 to the subtractor 7 is given by the following relation:
{S(t)+N(t)}2 S(t)2+N(t)2+2S(t)N(t) S(t)2+N(t)2+2S(t)N(t) (6) Since N(t)=0, the third term of Equation (6) becomes zero and so Equation (6) can be rewritten as:
- 14 - 1333~22 {S(t)+N(t)} =S(t) +N(t) (7) This weighting factor is determined so that the adverse fold-over effect produced by taking the absolute values is minimized. The following conditions are examples of weighting factor in which the value x represents the output of the absolute value circuit 2 and TH is a threshold value.
(1) W(x)=x (2) W(x)=l x >TH
=0 x <TH
(3) W(x)=l x >TH
=-a x <TH
=-a x <TH
(4) W(x)=x Figure 11 is one example of the adaptive weighting circuit 50 which is constructed according to the condition (3).
Weighting circuit 50 comprises a comparator 51, a multiplier 52 and a selector 53 to which the outputs of absolute circuit 2 and multiplier 52 are applied to be selectively coupled to the division circuit 8. Comparator 51 compares between the output of the absolute value circuit 2 and a threshold value TH and applies a logic selection signal to the selector 53. If the output of absolute value circuit 2 is higher than threshold value TH, the selection signal is at logic 1 and if otherwise, the selection signal is at logic 0. Multiplier 52 multiplies the weighting factor -a on the output of the absolute value circuit 2 and applies it to selector 53. If the comparator 51 output is at logic 1, the output of absolute value circuit 2 is passed through the selector 52 to the averaging circuit 3 and if - 15 ~ 1 3 3 3 ~ 2 2 otherwise, the output of multiplier 52 is passed to the averaging circuit 3.
Due to the weighting operation, the probability density distribution of the amplitudes of input signal adopts a curve shown at D in Figure 12b which is shifted to the right from the position of curve C (Figure 12a) by an amount equal to the distance between the intermediate point 0 and the threshold value TH. The weighting factor -a is so determined that the noise component which would otherwise cause the most serious fold-over effect is reduced to a minimum.
Subtractor 7 performs the following subtraction S(t)2+NIt)2-S(t) W(u) to produce an output which represents N(t)2, which is applied to the division circuit 8. As in the first embodiment, the division circuit 8 comprises a conversion table to which the signals N(t)2 and S(t)2+N(t)2 are applied as address signals.
Figure 13 is a graphic representation of the characteristic of the third embodiment using a threshold value 0.25, and a weight-ing factor -0.5. Comparison between Figures 6 and 13 indicates that precision of the circuit is improved by as much as 4 dB at high noise levels (low Eb/No inputs).
The C/N ratio of a demodulator output is found to vary with a deviation of the frequency of the carrier recovered by the demodulator from the frequency of the received carrier. The carrier-to-noise ratio detector of the present invention can therefore be used instead of the costly automatic frequency control circuit for preventing the demodulator from being locked ~ 16 ~ 1333922 in a pseudo sync state. This is accomplished by controlling a voltage controlled oscillator provided in a closed loop of the demodulator in accordance with the derived C/N ratio such that the latter is maintained at a maximum level.
As shown in Figure 14, a pseudo sync detector circuit can be implemented by the C/N ratio detector of the present invention. A demodulator 60 includes a quadrature detector 61 which receives an input PSK signal at terminal 64 and a recovered carrier from a voltage controlled oscillator 62 and produces demodulated signals at terminals 65. The demodulated output signals are applied to a phase detection and filtering circuit 63 to control the VCO 62 in accordance with a phase difference detected between the two output signals. One of the output signals is applied to the input of the C/N ratio detector of the present invention which is identical to that shown in Figure 1. The output of the division circuit 8 of the C/N ratio detector is applied to a controller 66 including a differential amplifier for comparison with a reference threshold. This reference threshold corresponds to a DC voltage at which the VCO 62 generates a carrier at the desired frequency when the C/N
ratio of the demodulator 60 is at a maximum value. The output of the differential amplifier 66 is representative of the deviation of the C/N ratio from its maximum value and is applied to the control terminal of the VCO 62.
When the demodulator is in a sync state, the C/N ratio of the demodulator is at the maximum value. However, if it goes out of sync and enters a pseudo sync state, the noise component increases in the outputs of the demodulator 60 and hence the C/N
ratio of the demodulator decreases, causing the output of the differential amplifier 66 to vary correspondingly. In this way, the VCO frequency is controlled until the output of the division circuit 8 returns to the maximum value of the C/N ratio.
The foregoing description shows only preferred embodiments of the present invention. Various modifications are apparent to those skilled in the art without departing from the scope of the present invention which is only limited by the appended claims. Therefore, the embodiments shown and described are only illustrative, not restrictive.
Weighting circuit 50 comprises a comparator 51, a multiplier 52 and a selector 53 to which the outputs of absolute circuit 2 and multiplier 52 are applied to be selectively coupled to the division circuit 8. Comparator 51 compares between the output of the absolute value circuit 2 and a threshold value TH and applies a logic selection signal to the selector 53. If the output of absolute value circuit 2 is higher than threshold value TH, the selection signal is at logic 1 and if otherwise, the selection signal is at logic 0. Multiplier 52 multiplies the weighting factor -a on the output of the absolute value circuit 2 and applies it to selector 53. If the comparator 51 output is at logic 1, the output of absolute value circuit 2 is passed through the selector 52 to the averaging circuit 3 and if - 15 ~ 1 3 3 3 ~ 2 2 otherwise, the output of multiplier 52 is passed to the averaging circuit 3.
Due to the weighting operation, the probability density distribution of the amplitudes of input signal adopts a curve shown at D in Figure 12b which is shifted to the right from the position of curve C (Figure 12a) by an amount equal to the distance between the intermediate point 0 and the threshold value TH. The weighting factor -a is so determined that the noise component which would otherwise cause the most serious fold-over effect is reduced to a minimum.
Subtractor 7 performs the following subtraction S(t)2+NIt)2-S(t) W(u) to produce an output which represents N(t)2, which is applied to the division circuit 8. As in the first embodiment, the division circuit 8 comprises a conversion table to which the signals N(t)2 and S(t)2+N(t)2 are applied as address signals.
Figure 13 is a graphic representation of the characteristic of the third embodiment using a threshold value 0.25, and a weight-ing factor -0.5. Comparison between Figures 6 and 13 indicates that precision of the circuit is improved by as much as 4 dB at high noise levels (low Eb/No inputs).
The C/N ratio of a demodulator output is found to vary with a deviation of the frequency of the carrier recovered by the demodulator from the frequency of the received carrier. The carrier-to-noise ratio detector of the present invention can therefore be used instead of the costly automatic frequency control circuit for preventing the demodulator from being locked ~ 16 ~ 1333922 in a pseudo sync state. This is accomplished by controlling a voltage controlled oscillator provided in a closed loop of the demodulator in accordance with the derived C/N ratio such that the latter is maintained at a maximum level.
As shown in Figure 14, a pseudo sync detector circuit can be implemented by the C/N ratio detector of the present invention. A demodulator 60 includes a quadrature detector 61 which receives an input PSK signal at terminal 64 and a recovered carrier from a voltage controlled oscillator 62 and produces demodulated signals at terminals 65. The demodulated output signals are applied to a phase detection and filtering circuit 63 to control the VCO 62 in accordance with a phase difference detected between the two output signals. One of the output signals is applied to the input of the C/N ratio detector of the present invention which is identical to that shown in Figure 1. The output of the division circuit 8 of the C/N ratio detector is applied to a controller 66 including a differential amplifier for comparison with a reference threshold. This reference threshold corresponds to a DC voltage at which the VCO 62 generates a carrier at the desired frequency when the C/N
ratio of the demodulator 60 is at a maximum value. The output of the differential amplifier 66 is representative of the deviation of the C/N ratio from its maximum value and is applied to the control terminal of the VCO 62.
When the demodulator is in a sync state, the C/N ratio of the demodulator is at the maximum value. However, if it goes out of sync and enters a pseudo sync state, the noise component increases in the outputs of the demodulator 60 and hence the C/N
ratio of the demodulator decreases, causing the output of the differential amplifier 66 to vary correspondingly. In this way, the VCO frequency is controlled until the output of the division circuit 8 returns to the maximum value of the C/N ratio.
The foregoing description shows only preferred embodiments of the present invention. Various modifications are apparent to those skilled in the art without departing from the scope of the present invention which is only limited by the appended claims. Therefore, the embodiments shown and described are only illustrative, not restrictive.
Claims
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A phase controlled demodulation system for digital communication, comprising:
a quadrature detector for receiving a modulated digital signal and generating therefrom a pair of I and Q demodulated signals;
a phase difference detection and filter circuit for detecting a phase difference between said I and Q demodulated signals;
means for detecting a carrier-to-noise ratio of one of said I and Q demodulated signals;
means for detecting a ratio difference between the detected carrier-to-noise ratio and a predetermined value; and a voltage controlled oscillator responsive to the detected phase difference and the detected ratio difference for generating a carrier as a replica of the carrier of said received digital signal and applying said carrier to said quadrature detector.
a quadrature detector for receiving a modulated digital signal and generating therefrom a pair of I and Q demodulated signals;
a phase difference detection and filter circuit for detecting a phase difference between said I and Q demodulated signals;
means for detecting a carrier-to-noise ratio of one of said I and Q demodulated signals;
means for detecting a ratio difference between the detected carrier-to-noise ratio and a predetermined value; and a voltage controlled oscillator responsive to the detected phase difference and the detected ratio difference for generating a carrier as a replica of the carrier of said received digital signal and applying said carrier to said quadrature detector.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA000616675A CA1333922C (en) | 1987-06-23 | 1993-07-22 | Phase controlled demodulation system for digital communication |
Applications Claiming Priority (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62-156044 | 1987-06-23 | ||
JP15604487A JPS64843A (en) | 1987-06-23 | 1987-06-23 | C/n measuring circuit |
JP62-156045A JPH01844A (en) | 1987-06-23 | C/N measurement circuit | |
JP62-156045 | 1987-06-23 | ||
JP16210987A JPS645248A (en) | 1987-06-29 | 1987-06-29 | C/n measuring circuit |
JP62-162109 | 1987-06-29 | ||
JP62-175658 | 1987-07-14 | ||
JP62175658A JPS6418339A (en) | 1987-07-14 | 1987-07-14 | Pseudo synchronizing detecting circuit |
CA000570052A CA1332450C (en) | 1987-06-23 | 1988-06-22 | Carrier-to-noise detector for digital transmission systems |
CA000616675A CA1333922C (en) | 1987-06-23 | 1993-07-22 | Phase controlled demodulation system for digital communication |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA000570052A Division CA1332450C (en) | 1987-06-23 | 1988-06-22 | Carrier-to-noise detector for digital transmission systems |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1333922C true CA1333922C (en) | 1995-01-10 |
Family
ID=27508308
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA000616675A Expired - Lifetime CA1333922C (en) | 1987-06-23 | 1993-07-22 | Phase controlled demodulation system for digital communication |
Country Status (1)
Country | Link |
---|---|
CA (1) | CA1333922C (en) |
-
1993
- 1993-07-22 CA CA000616675A patent/CA1333922C/en not_active Expired - Lifetime
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