Frequency and phase error determination apparatus

Abstract: A digital signal detector utilising a detected input digital signal derived from a reference square wave (13) and a received pulse train (12) to establish phase and frequency variations between the reference signal and the received signal. The detected signal (12) and the reference signal (13) are coupled to up-down counters (17, 18, 45, 46) wherein overflow counts from preset values are obtained which are representative of the frequency and phase difference between the reference and received signals. These overflow counts are utilised to establish phase and frequency error correction signals which may be coupled to control the reference oscillator to provide frequency and phase lock between the reference and received signals.

Description: The present invention relates to carrier frequency and phase acquisition and tracking circuits for use in phase-locked loop systems and more specifically to such circuits for use in phase-locked loop systems with low carrier signal-to-noise ratios. Carrier signal acquisition and tracking systems are known in the art. In particular, techniques for the acquisition and tracking of noisy signals such as those received from space or satellite vehicles are well established as disclosed, for example, in US -A-4,457,006 and US -A- 4,453,165. In such systems, a received RF carrier is typically modulated by a digital code sequence whose bit rate is much higher than the information signal bandwidth. One of the preferred modulation formats for these carriers is the bi-phase modulation technique in which a binary 1 and a binary O are represented by alternate 180° phase shifts. The signal bandwidth of such systems must allow for initial frequency uncertainty due to doppler shifts and non-coherent frequencies between the transmitting and receiving systems. Such bandwidths permit noise as well as information into the receiving system. In order to recover the Information with a high probability of detection, the receiving system local signals must be made coherent with the received or incoming signals. This is generally accomplished with carrier frequency and phase, acquisition and tracking techniques. In general, noisy signals are acquired and tracked with techniques which employ coherent processes, wherein a local reference is compared with the information signal to generate corrective signals for altering the frequency and phase of the local reference to match the frequency and phase of the information signal. Prior art techniques for providing coherent signal reception are effective but require relatively complex circuitry. One of the better known and documented signal comparator and error detector circuits for coherent reception is the Costas loop, as described in the book "Digital Communications by Satellite" by James J. Spilker, Jr. and published by Prentice-Hall in 1977. Costas loop circuitry, however, is relatively complex and, at least in part, utilises analogue techniques. A pair of signal multipliers, operating in phase quadrature, square the input signal. These multipliers are followed by circuitry which filter unwanted product signals and generate error correcting signals that are utilised to provide coherent reception. In some applications the error signals are filtered and amplified in analogue circuitry to directly control the local signal, while in other applications the error signals are converted to digital format by an analogue-to-digital converter for microprocessor control of the local signal. In contrast, the circuit of the present invention is completely digital, requires no multiplication or signal squaring, and requires only counters and attendant digital logic functions to filter and process error correcting signals. An all-digital phase locked loop circuit is also known from US-A-3 562 661 or from ELECTRONICS & COMMUNICATIONS IN JAPAN, vol. 63-B, no. 5, May 1980, pages 29-37, Scripta Publishing Co., Silver Spring, Maryland, US; T. KURITA et at.: "A digital phase-locked loop with AND filter". The present invention is defined in the appended claims and provides a frequency and phase error determination apparatus in which an input signal, comprising a train of rectangular pulses derived from a reference square wave and a received spread spectrum signal, is coupled to enable terminals of up-down counters such that counting occurs only during rectangular pulse intervals. A square wave signal, having a frequency lower than that of the input signal, is coupled to the up-down count function terminal to control the count direction. Thus, clock pulses are counted only during the occurrence of a rectangular pulse of the input signal, with the count direction determined by the reference square wave level. This establishes a total up count which is a direct function of the input enable excursions during the up count time and a total down count which is a direct function of the input enable excursions during the down count time. Since the square wave establishes equal up and down count times, an imbalance in the detected signal input, generated by frequency or phase offset of the received signal relative to a reference square wave, is indicated, due to circuit implementation, by excessive down counts. These excessive counts cause signals, representative of frequency or phase deviations, to be coupled to the counter borrow output terminals at a rate determined by the up-down signal frequency. Two up-down counters are utilised to generate frequency error signals and two to generate phase error signals. One of the two frequency (or phase) up-down counters generates a positive polarity error signal (borrow) and the other frequency (or phase) counter generates a negative polarity error signal in accordance with the prevailing error sense necessary for tracking. Frequency error correction signals are generated at the output terminals of the up-down counter wherein time averages of the frequency error signals are performed. At the completion of the frequency correcting function the two up-down counters employed for phase correction are enabled. One counter is utilised to advance the phase and the other counter is utilised to retard phase, of the reference square wave to achieve phase tracking of the received signal by the reference square wave. The phase error correcting signals are also coupled to a subsequent up-down counter to provide frequency correction signals during the phase tracking mode. This is accomplished by providing a frequency error correction resulting from the time average of the advance -retard phase error signals. A frequency and phase error determination apparatus in accordance with the present invention will now be described, by way of example, with reference to the accompanying drawings, in which:- Figure 1 is an illustration of waveforms associated with the determination apparatus of the present invention, Figures 2a and 2b together form a block diagram of the presently preferred embodiment of the invention and Figure 3 is an illustration of the waveforms and principles involved in deriving frequency and phase error signals by the apparatus of the invention. Figure 1 illustrates the input signal waveforms applied to the determination apparatus of the present invention and commonly encountered in spread spectrum receiving systems as employed for example, in the GPS navigation system. For clarity of illustration, the presence of noise superimposed on the received signal is not shown. This noise randomly alters the level transitions times of the received signal. Referring to Figure 1, a stable local reference signal A is utilised to generate level transition timing signals B. In like manner, the received signal which may differ in frequency and phase with respect to the local reference, as for example waveform C, or differ in phase only, as for example, waveforms F₁ and F₂, is utilised to establish level transition timing signals D and G, respectively, for the waveforms C and F. These timing signals are combined and coupled to circuitry that toggles its output signal level with each received pulse, to construct the wave form E corresponding to the received waveform C, or the wave form H corresponding to the received waveform F. This constructed waveform is the detector input signal coupled to a terminal 12 of Figure 2a. The present invention determines the frequency and phase difference between the input signal and a reference square wave to provide the error signals representative thereof to a phase-locked loop operating in a conventional manner to control the reference square wave and extract information from the received signal. Referring now to Figures 2a and 2b, a frequency and phase error determinator apparatus 10 constructed in accordance with the principles of the present invention includes an exclusive OR gate 11, having one of its input terminals coupled to the input signal terminal 12, and the other input terminal coupled to a reference square wave input terminal 13, via divider 14, wherein frequency division by a factor A is realised. The output of gate 11, in the form of a unipolar pulse train, is applied to the D input terminal of a signal synchronising D-type flip flop 15, clocked by a high frequency clock signal coupled from a terminal 16. The steady state clock frequency is an integer multiple of the input signal frequency at terminal 12. In accordance with the operation of D-type flip-flops, the signal at the D-terminal when the flip-flop 15 is clocked, is transferred to the Q-terminal. Thus Q, and Q , are similar to the D inputs and are in synchronism with the timing of the clock signal. The Q and Q output terminals of the flip flop 15 are respectively coupled to enable input terminals E₁ of up-down counters 17 and 18, alternately enabling the counters and permitting the counts to proceed in accordance with the time sequence of the synchronised detector input signal. A second enable signal is coupled to enable input terminal E₂. The origin of this enable signal will be described subsequently. The reference square wave signal from the frequency divider 14 is applied to D/U terminals of up-down (U-D)counters 17 and 18, in effect causing these counters to count up and count down in even increments of time by virtue of the square wave signal coupled to the D/U terminal. For the sake of brevity D refers to down, U refers to up. A preselected number, from a number generator 21, is loaded into the U-D counters 17 and 18 by a pulse coupled to the load terminals L from a flip-flop 22, triggered by a pulse of the square wave from the divider 14. The selected number is a design consideration and is determined by the error tolerance required and the signal-to-noise ratio of the input signal at terminal 12. Counting rate and comcomitantly phase error measurement resolution of the digital determination module is set by clock pulses coupled from clock input terminal 16. The borrow output terminals B of the U-D counters 17 and 18 provide output signals when the counters overflow on a down count. These signals represent phase errors between the input signal and the reference square wave, which is the output signal of a numerical controlled oscillator in a phase-locked loop, not shown. These phase error signals, coupled to output terminals 23a and 23b are utilised in a phase-locked loop, not shown, to establish and maintain phase lock between the signals at the input terminals 12 and 13. Since the counters 17 and 18 are enabled alternately, that is on the Q or Q output of flip flop 15, signals at the B terminals are mutually exclusive, therefore each phase error signal has a unique error correcting sense, and advances or retards the phase by fixed predetermined increments at a rate established by the frequency of the square wave coupled to the U-D terminals. The phase error pulses from the B terminals of the counters 17 and 18 are also coupled to U and D terminals of a further up-down counter 24, respectively, thereby causing the counter 24 to count up or down in accordance with the sense of the detected phase error. For example, when the up count exceeds the down count over an interval of the time, determined by the range of the counter, the counter 24 will overflow at the carry terminal C generating a pulse. This pulse is coupled to one input terminal of an OR gate 25, while the other input terminal is coupled to receive a pulse from the borrow terminal B when the down count exceeds the up count. Thus U-D counter 24, in combination with the OR gate 25, generates pulses whenever phase error signals are coupled to the U-D terminals of the up-down counter 24. The output of the OR gate 25 is applied to a frequency error generating strobe, such as a serial in-parallel out shift register 26. This pulse is clocked into the initial stage A and subsequently into stages D and E of the shift register 26 by clock pulses of frequency f C derived from the clock pulses at the clock terminal 16. Pulses at the B and C terminals of the up-down counter 24 are also coupled to reset the counter 24, while pulses at the final stage E of the shift register 26 are coupled to load data at the data terminals preselected through a generator 27. This data biases the counter to hasten the generation of the carry or borrow pulses. Each pulse at stage A of the shift register 26 is coupled via an OR gate 31 to the input terminal of a counter 32, which functions as a frequency offset register. The word at the output terminals of the counter 32 is coupled, directly or via a latch, not shown, to the numerically controlled oscillator in the phase-locked loop to control the frequency of the oscillator. Pulses coupled from the OR gate 31 increment the register up or down in accordance with signals coupled from an up-down logic unit 33, wherein the phase error counts from the counters 17 and 18 are compared to determine a phase lead or lag. Signals at stage D of the shift register 26, arriving a few clock pulses after the initial entry into stage A, are coupled, via an OR gate 34 to generate latch signals for updating the stored frequency word that controls the numerically controlled oscillator. At the time the counter 24 is loaded, all the stages of the shift-register 26 have been reset to zero and the system is set to process subsequent signals representative of the reference square wave, input signal phase relationship. Prior to establishing a phase-lock between the reference square wave (numerically controlled oscillator) and the input signal, the frequency of the numerically controlled oscillator is locked to the input signal. This is accomplished in a manner similar to that for achieving the phase lock described above. Referring again to Figures 2a and 2b the input signal is coupled via the input terminal 12 to the D input of a flip-flop 35, while the reference square wave at input terminal 13 is coupled to one terminal of a switch 36 and to a second terminal of switch 36 after division by a factor AB in dividers 14 and 37. When a low level signal is present at the final stage E of a shift register 41 and an initiation signal is coupled to a terminal 42 of an enable signal generator 43, a multiplexer 44 causes the switch 36 to couple the reference square wave, at the undivided frequency, to the U-D terminal of a counter 45 and a frequency correction is made in the manner previously described. Clock pulses for the multiplexer 44 are provided by dividing the output pulses from a monostable flip-flop 47 by a factor C and coupling the divided pulses to the clock terminals of the multiplexer 44. The multiplexer 44 will cause the switch 36 to couple signal S₂, at the reference square wave frequency divided by the factor AB, to the counter 45 and to a monostable flip-flop 47 when a clock pulse and enable signal are simultaneously coupled to the multiplexer 44. An enabling signal at the multiplexer 44 occurs when the final stage of the shift register 41 is at a low level, thereby indicating that the coarse frequency adjustment is complete. Frequency adjustments are then made for the S₂ signal in a similar manner, whereafter the multiplexer 44 couples a phase enable signal to the counters 17 and 18 and phase corrections are made as previously described. The operation of the invention may be also explained by referring to the waveforms of Figures 1 and 3. Referring to Figure 1, the input signal derived from the square wave A and received signal C, is a repetitive signal. Each cycle of this signal possesses a multiplicity of pulses having duty cycles that vary at a rate determined by the difference in frequency between the square wave reference signal A and the received signal C. As shown, the received signal C is lower in frequency than the reference signal. Before phase lock can be achieved the frequency of signal A must be adjusted to be equal to the frequency of the received signal C. Consider now waveform H, derived from the reference signal A and a received signal F having a phase offset from the reference square wave A. For this situation the detector input signal H is a string of pulses at a fixed repetition rate having a duty cycle that is determined by the phase offsets between the received signal F and the local reference A, as for example waveform H₁ for F₁ lagging A, and waveform H₂ for F₂ leading A. To establish phase lock, the pulses of the reference square wave A must be advanced or retarded. When this is accomplished the input signal is a square wave having a 50% duty cycle, identical to the reference square wave and received signal. Refer now to Figure 3, wherein a detector input signal 51, its complement 52, and a U-D count cycle are shown. During each U-D count cycle unipolar excursions of a specific number of cycles of the reference signal enable a counter clocked by a frequency f C . At the expiration of this period an equal number of unipolar excursions provide a down count which is compared to the up count. If the down count exceeds the up count, a borrow signal is generated and utilised as a correcting signal. The change in phase of the input signal for each sensing (U-D) time is where f is the offset frequency and f U-D is the frequency of the reference square wave. The magnitude of the overflow count is This count is achieved by the present invention in the following manner. An input signal with or without significant attendant noise, from the input terminal 12 is coupled to the D input of the sync flip flop 35, the output signals of which Q and Q switch synchronously with clock pulses coupled to the terminal 16. An enable signal coupled to the enable generator 43 activates the enable S₁ line to the switch 36, permitting S₁, the U-D square wave at terminal 13, to load the U-D counters 45 and 46 and initiate an up count in each counter. This signal is also routed through monostable flip flop 47 to a frequency divider 49, wherein a division by a factor C is performed. The output pulses resulting from this division are coupled to clock multiplexer 44. Half way through the U-D count a down count is initiated. The ranges of the U-D counters 45,46,17, and 18 are chosen so that no overflow occurs on an up count. The number of cycles of the input signal sampled (N) per U-D count cycle, and therefore the U-D frequencies are for the most part selected from the following considerations. S₁, the coarse acquisition range frequency is sufficiently large to keep Δ≦ 180° per U-D cycle, to avoid error sense ambiguity. S₂, the fine acquisition range frequency is sufficiently small to pull frequency uncertainty Δf to within the capture range of the phase-locked loop. S₀, the up-down rate during phase tracking must be sufficiently small to attain an adequate probability of detection in the presence of a noisy signal as is set forth in communications theory. Referring again to Figures 2a and 2b, the counter 45 will overflow if Δf the difference frequency is negative or counter 46 will overflow when Δf is positive, the extent of the overflow as previously given being :- Overflow pulses occurring at the U-D frequency clock the U-D counter 48 until an overflow occurs at which time the shift register 41 generates a clock pulse from stage A to adjust the frequency of the square wave reference generator in the phase-locked loop by a fixed increment. The shift register 41, clocked at a rate f C , generates an output pulse at a subsequent clock pulse from stage D to latch the updated frequency information. A subsequent pulse from stage E causes the multiplexer 44 to maintain the enable S₁ function. Simultaneously, the U-D counter 48 is loaded with the count preset at the DATA terminals. This in effect re-initiates the counter 48 for a new comparison between the input up and down pulses from the counters 45 and 46. The numbers loaded into the counter 48 may be chosen significantly to speed up the frequency acquisition process. This may be done by biasing the load number in accordance with the error signal sense. For example, assume the counter 48 is a divide by 16 binary counter and that the initial frequency offset generates a carry C pulse after binary 15. This carry pulse is coupled to the shift register 41 and to the number generator 27 to increment the reference number prior to loading. This increment speeds up the generation of the next carry pulse by loading a number of few counts below binary 15. In like manner DATA 1 is loaded to speed up generation of borrow output pulses. The process of overflow from counters 45 and 46 generating error signals and correcting the difference frequency continues until the count resulting from Δf no longer generates error correction signals. At this time a function shift signal is coupled to the multiplexer 44 and shift enable S₂ occurs. This causes the lower U-D frequency, thereby increasing the error count, since this count is proportional to The foregoing process is repeated until the multiplexer 44 shifts to disable the frequency acquisition circuitry and enable the phase correction circuitry. As opposed to most prior art frequency and phase error determinators the circuit of the present invention is conceptually simple, flexible in application and completely digital requiring no alignment or adjustment. Parameters such as U-D sample rate, U-D counter range number loading, and clock quantisation may be varied to fulfil a broad range of system applications.

Claims: A frequency and phase error determinator comprising means (13) for providing a reference signal having a frequency f₁ and phase p₁; means (12) for providing an input signal representative of a signal having a frequency f₂ and phase p₂ and means (16) for providing clock pulses; characterised in that it further comprises count means (11,15,17,18,24,28,32,35,41,45,46,48) responsive to the reference signal, the input signal and the clock pulses for counting the clock pulses when p₁ differs from p₂ and when f₁ differs from f₂ and for providing output signals indicating phase and frequency differences when clock pulse counts exceed preselected count values. A determinator according to claim 1, characterised in that the count means includes first synchronising means (35) coupled to receive the input signal (12) and the clock pulses (16) for providing a signal representative of the input signal at a first output terminal and a signal complementary to the representative signal at a second output terminal with each received clock pulse; and first and second up-down counter means (45,46) having enable terminals coupled respectively to the first and second output terminals of the first synchronising means, and count direction control terminals coupled to receive the reference signal (13) for counting clock pulses coupled thereto and providing output pulses at overflow terminals when the clock pulse counts exceed preselected count values. A determinator according to claim 2, characterised in that the count means further includes gate means (11) coupled to receive the input signal (12) and a signal representative of the reference signal (13) for providing a signal having a predetermined logic level at an output terminal when either, but not both, the input signal or the signal representative of the reference signal are at the predetermined logic level and a logic level complementary to the predetermined logic level otherwise, second synchronising means (15) having an input terminal coupled to the output terminal of the gate means for providing the gate means output signal at a first output terminal, and a signal complementary to the gate means output signal at a second output terminal, and fourth up-down counter means (17,18) having enable terminals coupled respectively to the first and second output terminals of the second synchronising means, and count direction control terminals coupled to receive the signal representative of the reference signal for counting clock pulses coupled thereto and providing output pulses at overflow terminals when the clock pulse counts exceed preselected count values. A determinator according to claim 3, characterised in that the count means further includes first overflow counter means (48) having up-down control terminals coupled to the overflow terminals of the first and second up-down counters (45,46), respectively, for providing carry and borrow pulses in accordance with clock pulse counts that exceed loaded count values; second overflow counter means (24) having up-down control terminals coupled to the overflow terminals of the third and fourth up-down counters (17,18) respectively, for providing carry and borrow pulses in accordance with clock pulse counts that exceed loaded count values; first and second shift register means (41,26) respectively coupled to receive the carry and borrow pulses from the first and second overflow counter means for serial storage in a plurality of register stages having individual output terminals; and frequency offset register means (32) coupled to an output terminal of a selected one of the plurality of register stages for establishing corrected frequency control signals to alter the reference signal frequency in response to signals received from the selected one stage. A determinator according to claim 4, characterised in that the count means further includes up-down logic means (33) having input terminals coupled to the overflow terminals of the first, second, third and fourth up-down counter means (45,46,17,18) and an output terminal coupled to the frequency offset register means (32) for establishing correction directions in establishing the frequency control signals. A determinator according to claim 5, characterised in that it further includes multiplexing means (44) coupled to receive signals representative of the reference signal (13) for sequentially providing enabling signals to a multiplicity of output terminals one of which is coupled to enable terminals of the third and fourth up-down counters (17,18); and switch means (36) coupled to receive enabling signals from the multiplexing means and having an output terminal coupled to the count direction control terminals of the first and second up-down counter means (45,46), a first input terminal coupled to receive the reference signal (13) and a second input terminal for selectively coupling the first and second input terminals to an output terminal in response to the enabling signals; and divider means (14,37) coupled between the reference signal means and the second input terminal of the switch means for reducing the frequency f₁ by a predetermined factor.

Inventors: NELSON ALEC LEE, NELSON, ALEC LEE
Applicants: HONEYWELL INC, HONEYWELL INC.
Application year: 1986
Main classification: H03L7
IPC codes: H04J13, G01S19