US2480038A - Compensation of distortion in guided waves - Google Patents

Compensation of distortion in guided waves Download PDF

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US2480038A
US2480038A US675340A US67534046A US2480038A US 2480038 A US2480038 A US 2480038A US 675340 A US675340 A US 675340A US 67534046 A US67534046 A US 67534046A US 2480038 A US2480038 A US 2480038A
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delay
wave
pulse
distortion
signal
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Warren P Mason
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AT&T Corp
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/02Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S13/50Systems of measurement based on relative movement of target
    • G01S13/52Discriminating between fixed and moving objects or between objects moving at different speeds
    • G01S13/522Discriminating between fixed and moving objects or between objects moving at different speeds using transmissions of interrupted pulse modulated waves
    • G01S13/524Discriminating between fixed and moving objects or between objects moving at different speeds using transmissions of interrupted pulse modulated waves based upon the phase or frequency shift resulting from movement of objects, with reference to the transmitted signals, e.g. coherent MTi
    • G01S13/526Discriminating between fixed and moving objects or between objects moving at different speeds using transmissions of interrupted pulse modulated waves based upon the phase or frequency shift resulting from movement of objects, with reference to the transmitted signals, e.g. coherent MTi performing filtering on the whole spectrum without loss of range information, e.g. using delay line cancellers or comb filters

Definitions

  • Delay devices and especially wave guide delay lines, are characterized, in general, by attenuation and phase shift.
  • the attenuation can usuallybe compensated by an amplifier which provides a gain equal to the transmission loss or attenuation of the line.
  • the phase shift is more difficult to compensate, and in some applications a comparatively small amount of phase distortion may seriously affect the performance of the apparatus.
  • systems have been proposed in which a sequence of energy pulses are transmittedover two parallel paths one of which contains a delay line, the output signals from the two paths being balanced against each other in a suitable indicating device to give a null signal as long as all pulses of the sequence are alike, and a difference signal when theydifier.
  • the delayed pulses always differ from the undelayed pulses so that an undesired diilference signal appears, even when the original pulses of the sequence are identical, and masks the difference signal. It is a specific object of the inventionto reduce this masking effect.
  • phase distortion for which this invention provides compensation arises from the fact that each pure sinusoidal component of a guided wave of a particular type is propagated with a phase velocity which depends on its frequency, being, in general, greater than the phase velocity in-the unconfined medium, approaching this value as the frequency increases without limit, but departing therefrom to an ever greater extent as the cut-off frequency of the guide is approached. Components having lower phase velocities are delayed more thanare components having higher phase velocities. There is thus a relative phase delay between components, and phase distortion results. (The cut-off frequency the phase distortion for each particular type of guide is related in a specific manner to the length and the transverse dimensions of the guide.
  • the relative phase delay is a definite assignable function, for each particular type of guide, of its length and transverse dimensions.
  • two wave guide delay lines of a particular type are provided, instead of one as in the past, and their dimensions are so adjusted that the relative delay function is the same for 'both, while their signal delays are different.
  • Energy is fed to a matching circuit by two parallel paths, the longer delay line being connected in one path and the shorter line in the other.
  • the invention in its wave guide aspects, therefore, is of use wherever it is required to balance or compensate for the distortion which results from propagation of a wave along a guide while still retaining the useful effects of the propagation.
  • delay device aspects it is of use wherever a delay device of any type is employed for the sake of its useful delay and it is desired to compensate for the inherent phase distortion of the delay device.
  • MTI moving target indicator
  • Fig. 1 is a functional schematic diagram of a moving target indicator system modified to include the distortion compensator of the invention
  • Fig. 2 is 'a diagram illustrating the relations between delayed andundelayed pulses for a fixed object
  • Fig. 3 is a diagram illustrating the relations between delayed and undelayed pulses for a moving object
  • Fig. 4 shows a longitudinal section and Fig. 5 a cross-section of both members of a matched pair of circular cross-section hollow wave guide delay lines dimensioned in accordance with the invention
  • Fig. 6 shows a longitudinal section and Fig. 7 a cross-section of both members of a matched pair of rectangular cross-section hollow wave guide delay lines dimensioned in accordance with the invention:
  • Fig. 8 shows a longitudinal section and Fig. 9 a cross-section of both members of a matched pair of circular cross-section elastic solidrod or wire wave guide delay lines dimensioned in accordance with the invention.
  • the resulting pulse modulated carrier is radiated by the antenna 2 as short, sharp spurts of radio frequency energy spaced apart at intervals'An, the system being quiescent between.
  • the carrier frequency is preferably very high, for example, 200 megacycles per second so that, by the use of a suitable antenna, high directivity of radiation may be obtained.
  • the radiation may be directed toward any desired object by any desired means.
  • the pulse-modulated radio frequency energy travels outward from the antenna 2 in the desired direction, is reflected by any objects i that may be in its path, and returns to be picked up by a receiving antenna H.
  • the radio frequency may be beaten down as by an oscillator l3 and modulator [4 to a suitable intermediate frequency, for example, 5 megacycles per second. This process does not alter the wave shape of the envelope. which is schematically indicated at i5, and consists of short, sharp spurts of energy of the intermediate frequency, for example 5 megacycles per second, spaced apart by intervals Ati.
  • This pulse-modulated intermediate frequency wave is next passed through two parallel paths, l6, l1, one of which id contains a guided wave delay device l8, adjusted to give a propagation delay Atz between input terminals and output terminals.
  • the line propagation delay Atz is equal to the pulse period Ati, though in the present system Atz exceeds Atr, as will appear hereinbelow.
  • the delay line i8 may comprise a tube, pipe or trough of appropriate length containing a wave-supporting medium such as a liquid 49. The characteristics of mercury are such that it is well suited for the purpose.
  • - pipe, tube, or trough may be straight or folded Fig. 10 shows a longitudinal section and Fig. 11
  • Fig. 1 is a functional schematic diagram of a circuit arrangement adapted to provide an indication of the movement of any object or target l which may be within the radiation field of an antenna 2 and to be non-responsive to the presence of fixed or momentarily stationary objects or targets within the field.
  • a multivibrator 3 or other source supplies a periodic sequence of short, sharp pulses 4 spaced apart by a time interval Atr.
  • These pulses modulate the amplitude of a carrier wave, derived from an oscillator 5, any suitable modulating device 6 being provided for the purpose.
  • the interior surfaces 20 of the tube walls and of any internal reflectors are preferably etched or ground.
  • Energy may be applied to the near end by a transmitter T and abstracted from the distant end by way of a receiver R.
  • the transmitter T and the receiver R. may each comprise an electro-mechanical transducer such as a piezoelectric crystal element.
  • the external electrode of either or both crystals may be domed.
  • a mercury delay line waveguide including these features is described and claimed in H. J. Mc- Skimin application Serial No. 653,255, flied March 9, 1946.
  • Features of corresponding function for dielectric wave guides are described and shown in United States Patent 2,147,717 to S. A. Schel-- kunoif.
  • the pulse-modulated intermediate frequency waves l5 which are propagated over the delay line I8 and delayed thereby by a time interval Atz are then amplified, as necessary, as by an adjustable gain amplifier 2i.
  • the intermediate frequency is removed by a detector 22 and the resulting pulses are supplied by way of a transformer 23 to an indicating device, for example to the vertical deflection plates 24 of a cathode-ray oscilloscope 25 which may be of conventional construction.
  • the pulse-modulated intermediate frequency energy also travels over a by-path I! which does not include any delay device, through a variable gain amplifier 21, a detector 28 which removes the intermediate glassstic of all guided wave delay lines.
  • the pulse shape at the far end of the line I8 is 2,4ao,oss
  • the spurts II of pulse-modulated intermediate frequency energy entering the delay line I8 and the by-path II from the demodulator I4 are all alike, recurring at intervals At1. If it were not for distortion in the delay line I8 the (n+1)th pulse arriving at the vertical deflection plates by way of the by-path would be exactly cancelled by the preceding nth pulse arriving by way of the delay line, so that no indication would appear on the screen of the cathode-ray oscilloscope 25.
  • the cathode-ray oscilloscope beam may be swept horizontally at constant speed as by a saw-tooth wave voltage applied to the horizontal deflection plates 30, which sawtooth wave voltage may be derived from a sawtooth wave oscillator 3i synchronized with the multivibrator 3.
  • the indication due to the difference, either in magnitude or in time of occurrence, between the delayed pulse and the undelayed pulse, which is illustrated ference between these delays is equal to the multivibrator pulse period, 1.
  • Fig. 3 appears on the cathode-ray oscilloscope I screen as a pip whose location along a horizontal axis is proportional to the object distance.
  • Various known refinements and modifications of the ranging feature may be employed as desired.
  • resulting difierence signal from a large fixed object may be suificient to mask the desired signal from a smaller and more important moving object.
  • the later undelayed pulse is distorted to the same extent and in the same manner as the earlier delayed one, by passing the later pulse in the by-path II through an auxiliary guided wave delay line 35 having the same relative phase delay distortion coefficient as the primary delay line, but a different time delay Ats.
  • the auxiliary delay line 35 in the by-path Il may be provided with a transmitter T and a receiver R like those of the primary line I8 and may be of identical construction with the primary delay line I8 but having one-quarter the length and one-half the diameter of the latter.
  • v propagation velocity in the unconfined medium.
  • 1 D can be set equal to zero for a cylindrical guide.
  • n indicates the order of the Bessel function and m the degree of the root, or mode of the oscillation.
  • the delay line is driven by an axially vibrating crystal only the zero order vibration will be generated in which case the modular constants are given by the first line of the table above.
  • the appropriate boundary condition is that the radial velocity, given by the negative radial derivative of the velocity potential, is zero at the walls. That is,
  • a is the attenuation constant and p is the phase constant of the guide; i. e., the phase shift per unit length.
  • the "cut-off frequency of the guide is the frequency at which the propagation constant is zero. From (11) it is evidently Below this frequency the wave will be attenuated. At frequencies above the cut-01f it will be propagated without attenuation. When unattenuated propagation takes place, the phase velocity is given by From (11) at frequencies in the range of unattenuated propagation and not too close to the cut-ofi frequency, the total phase shift from end to end of the guide is given by This expression is seen to contain two terms. The first is directly proportional to frequency, which is desirable for undistorted transmission. The second is inversely proportional to frequency and therefore represents the relative delay of one component frequency as compared with another which gives rise to phase distortion.
  • Equations 10, 11 and 14 the signal strength at the output of the primary delay line is proportional to the velocity potential due to a pulse which entered the line at time t. It may be written in complex form as Adjustment of the relative gains of the amplifiers makes the magnitudes of these two series alike, term for term, in which case Then each term of (15) may be balanced against the corresponding term of (16), giving, for the difference, a series of terms each of which is of the form From (14), series expansion of the bracketed term in (17) gives terms containing successive 4 powers of the quantity 1 l l i Bi l-i Ba i 01-42) +5 CT 1:;
  • the principles of the invention are applicable to wave guide delay lines of many types other than those analyzed in detail above.
  • the relative phase delay is found to be some assignable function of the length and transverse dimensions, and it is only necessary, in order to practice the invention in its wave guide aspect, to provide an auxiliary guide in which this function is the same as it is for the principal guide but which has a difierent length and therefore a different signal delay, to apply the same signals to both, and to balance their outputs.
  • the same principles may be applied to delay devices other than wave guides.
  • a. source of a sequence of pulse signals recurring at equal time intervals means for radiating said pulsed signals in a desired direction, means for receiving only echo pulsed signals reflected from objects lying in the path of said radiated signals, a relatively long delay unit, a relatively short delay unit, the difierence in the delay of said units being equal to the pulse recurrence interval, the phase distortion coemcient of the short delay unit being substantially identical with the phase distortion coefficient of the long delay unit, means for launching said received echo pulse signals simultaneously into the proximate ends of both of said units, means associated with the distant end of each of said delay units for picking up signals propagated lengthwise of said delay unit, means for deriving a signal related to the difierence between the signal picked up from said longer unit and signal picked up from said shorter unit, whereby said received echo signals reflected from stationary objects lying in the path of said radiated signals will be precisely balanced out and measurable difference signals will be obtained only from
  • a pulse-reflection, object-detectingandranging system the combination with a source of pulsed signals recurring at equal time intervals and means for radiating said pulsed signals in a desired direction, of a signal receiver responsive only to reflections of said pulsed signals reflected fromcbjects'lying in the path of said radiated signals, a plurality of parallel transmission paths intermediate said source and said receiver, a primary delay unit having longitudinal and transverse dimensions in one of said paths, adaptedto introduce a.
  • auxiliary delay unit in another of said paths, having a delay differing from that of said primary unit by precisely the time interval between said recurring pulses and different longitudinal and transverse dimensions which impart to said auxiliary delay unit the same distortion function as said primary delay unit,.and means for balancing signals traveling by one of said paths against signals traveling by the other of said paths to produce a difierence signal only when said time of recurrence of said signals is changing whereby pulses reflected from objects in motion only will produce a measurable difierence signal.
  • a plurality of parallel trans,- mission .paths connecting said source to said receiver, a primary liquid delay unit in one of said paths, adapted to introduce a preassigned time delay into signals propagated through said unit in proportion to its length and introducing undesired distortion in proportion to its length and in inverse proportion to the square of its transverse dimensions, an auxiliary liquid delay unit in another of said paths, having a different length to the square of transverse dimensions, and different dimensions and the same ratio of length and means for balancing signals traveling by one of said paths against signals traveling by the other of said paths to produce a difierence signal.
  • a primary elastic solid delay unit in one of said paths adapted to introduce a preassigned time delay into signals propagated along said unit in proportion to its length and introducing undesired distortion in proportion to the product of its length and the square of its transverse dimensions
  • an auxiliary elastic solid delay unit in another of said paths having a difl'erent length and diiferent transverse dimensions and the same product of length and transverse dimensions, and means for balancing signals traveling by one of said paths against signals traveling by the other of said paths to produce a difference signal.
  • a primary delay unit having longitudinal and transverse dimensions in one of said paths, adapted to introduce a preassigned time delay exceeding the interval between successive signal pulses into pulse signals propagated therethrough and introducing undesired phase distortion into 12 said signals in proportion to a specified functionom of said longitudinal and transverse dimensions.
  • an auxiliary delay unit in another of said paths having a time delay equal to the difference between the time delay of said primary delay unit and the time interval between successive signal pulses, and having difierent longitudinal and transverse dimensions and the same phase distortion function of longitudinal and transverse dimensions as said primary delay unit, and means for balancing each pulse as propagated through said primary unit against a later pulse propagated through said auxiliary unit to produce a diflerence signal.

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Description

Aug. 23, 1949. w. P. MASON COMPENSATION OF DISTORTION IN GUIDED WAVES 2 Sheets-Sheet 1 Filed June 8, 1946 Iii nv Moa RFAMP 2. G I F T 0 mm mm 0 A s n B m m m M S P n a s N 0 Y E E A R r L E u M n M w m 2 a M I l m} a H W A T TORNEY Aug. 23, 1949. w. P. MASON 2,430,038
COMPENSATION OF DISTORTION IN GUIDED WAVES Filed June 8, 1946 2 Sheets-Sheet 2 INVENTOR W- P. MASON AT. TORNE V Patented Aug. 23, 1949 I UNITED STATES PATENT OFFICE COMPENSATION OF DISTORTION IN GUIDED WAVES' Warren P. Mason, West Orange, N. J., asslgnor to Bell Telephone Laboratories, Incorporated, New York, N. Y., a corporation of New York Application June 8, 1946, Serial No. 675,340
Claims. (Cl. 343-8) of a wave guide is the frequency below which the guide will not support a wave of the type in question over. any substantial distance, serving rather to attenuate rapidly any oscillatory energy delivered to its proximate end.)
At frequencies in the useful range of the guide, that is to say at frequencies which are not too close to the. cut-off frequency, it turns out that balance between a signal which has been modified in form by propagation over a wave guide of substantial length and another signal which has not been so propagated.
Delay devices, and especially wave guide delay lines, are characterized, in general, by attenuation and phase shift. The attenuation can usuallybe compensated by an amplifier which provides a gain equal to the transmission loss or attenuation of the line. The phase shift is more difficult to compensate, and in some applications a comparatively small amount of phase distortion may seriously affect the performance of the apparatus. For example, systems have been proposed in which a sequence of energy pulses are transmittedover two parallel paths one of which contains a delay line, the output signals from the two paths being balanced against each other in a suitable indicating device to give a null signal as long as all pulses of the sequence are alike, and a difference signal when theydifier. However, as a result of phase distortion in the delay line, the delayed pulses always differ from the undelayed pulses so that an undesired diilference signal appears, even when the original pulses of the sequence are identical, and masks the difference signal. It is a specific object of the inventionto reduce this masking effect.
One type of phase distortion for which this invention provides compensation arises from the fact that each pure sinusoidal component of a guided wave of a particular type is propagated with a phase velocity which depends on its frequency, being, in general, greater than the phase velocity in-the unconfined medium, approaching this value as the frequency increases without limit, but departing therefrom to an ever greater extent as the cut-off frequency of the guide is approached. Components having lower phase velocities are delayed more thanare components having higher phase velocities. There is thus a relative phase delay between components, and phase distortion results. (The cut-off frequency the phase distortion for each particular type of guide is related in a specific manner to the length and the transverse dimensions of the guide. For example, in the case of a non-absorptive supersonic compression wave guide of length l and of circular cross-section radius r, the relative phase delay distortion coeflicient for any particular angular frequency w is given by whereas the signal delay is of course proportional to the length l and independent of the radius r. This relation is developed below.
For a guide of rectangular cross-section, the
' corresponding expressions are twornamely:
D.=k2;f-,, D.'=k2
where 2a is the length of the longer side of the section, and 2b is the length of its shorter side. Similar relations hold for electromagnetic waves in dielectric guides of rectangular or circular cross-section. In the case of an absorptive acoustic or supersonic guide, the correspondin relation is In the case of a compression wave in an elastic solid rod or wire the corresponding expression is For a torsional wave in a solid rod or wire the expression is similar, namely Q r -l r In these expressions 701, Ice, Ice, k4, etc, are constants depending only on the characteristics of the wave-supporting medium and on the frequency. They are independent of the dimensions of the guide.
The feature which is common to these expressions and which characterizes wave guides of the types above referred to as well as others is that the relative phase delay is a definite assignable function, for each particular type of guide, of its length and transverse dimensions. In ac-' Me usa cordance with the invention in its wave guide aspect, therefore, two wave guide delay lines of a particular type are provided, instead of one as in the past, and their dimensions are so adjusted that the relative delay function is the same for 'both, while their signal delays are different. Energy is fed to a matching circuit by two parallel paths, the longer delay line being connected in one path and the shorter line in the other. Thus the waves which reach the matching circuit by the two different paths, though delayed by unequal amounts, will have been distorted by equal amounts, so that for equal input signals, a substantial balance may be had in the matching circuit.
The invention in its wave guide aspects, therefore, is of use wherever it is required to balance or compensate for the distortion which results from propagation of a wave along a guide while still retaining the useful effects of the propagation. In its delay device aspects it is of use wherever a delay device of any type is employed for the sake of its useful delay and it is desired to compensate for the inherent phase distortion of the delay device. Among other applications it finds use in a moving target indicator (MTI) system, in which embodiment it will be described in the ensuing detailed description and illustrated in the accompanying drawings, in which:
Fig. 1 is a functional schematic diagram of a moving target indicator system modified to include the distortion compensator of the invention;
Fig. 2 is 'a diagram illustrating the relations between delayed andundelayed pulses for a fixed object;
Fig. 3 is a diagram illustrating the relations between delayed and undelayed pulses for a moving object;
Fig. 4 shows a longitudinal section and Fig. 5 a cross-section of both members of a matched pair of circular cross-section hollow wave guide delay lines dimensioned in accordance with the invention;
Fig. 6 shows a longitudinal section and Fig. 7 a cross-section of both members of a matched pair of rectangular cross-section hollow wave guide delay lines dimensioned in accordance with the invention:
Fig. 8 shows a longitudinal section and Fig. 9 a cross-section of both members of a matched pair of circular cross-section elastic solidrod or wire wave guide delay lines dimensioned in accordance with the invention; and
an amplifier l, the resulting pulse modulated carrier is radiated by the antenna 2 as short, sharp spurts of radio frequency energy spaced apart at intervals'An, the system being quiescent between. The carrier frequency is preferably very high, for example, 200 megacycles per second so that, by the use of a suitable antenna, high directivity of radiation may be obtained. The radiation may be directed toward any desired object by any desired means.
The pulse-modulated radio frequency energy travels outward from the antenna 2 in the desired direction, is reflected by any objects i that may be in its path, and returns to be picked up by a receiving antenna H. After suitable amplification, as by an amplifier l2, the radio frequency may be beaten down as by an oscillator l3 and modulator [4 to a suitable intermediate frequency, for example, 5 megacycles per second. This process does not alter the wave shape of the envelope. which is schematically indicated at i5, and consists of short, sharp spurts of energy of the intermediate frequency, for example 5 megacycles per second, spaced apart by intervals Ati.
This pulse-modulated intermediate frequency wave is next passed through two parallel paths, l6, l1, one of which id contains a guided wave delay device l8, adjusted to give a propagation delay Atz between input terminals and output terminals. In prior systems the line propagation delay Atz is equal to the pulse period Ati, though in the present system Atz exceeds Atr, as will appear hereinbelow. The delay line i8 may comprise a tube, pipe or trough of appropriate length containing a wave-supporting medium such as a liquid 49. The characteristics of mercury are such that it is well suited for the purpose. The
- pipe, tube, or trough may be straight or folded Fig. 10 shows a longitudinal section and Fig. 11
a cross-section of both members of a pair of absorptive-walled acoustic wave guide delay lines dimensioned in accordance with the invention.
Referring now to the figures, Fig. 1 is a functional schematic diagram of a circuit arrangement adapted to provide an indication of the movement of any object or target l which may be within the radiation field of an antenna 2 and to be non-responsive to the presence of fixed or momentarily stationary objects or targets within the field. Such systems may take various forms and may differ in major or in minor particulars. In the simple system shown, a multivibrator 3 or other source supplies a periodic sequence of short, sharp pulses 4 spaced apart by a time interval Atr. The repetition rate may be of the order of 1000 pulses per second, in which case Atr=0.001 second. These pulses modulate the amplitude of a carrier wave, derived from an oscillator 5, any suitable modulating device 6 being provided for the purpose. After suitable amplification as by as preferred. If a high impedance liquid such as mercury is employed, the interior surfaces 20 of the tube walls and of any internal reflectors are preferably etched or ground. Energy may be applied to the near end by a transmitter T and abstracted from the distant end by way of a receiver R. The transmitter T and the receiver R. may each comprise an electro-mechanical transducer such as a piezoelectric crystal element. To prevent or reduce transmission of guided wave energy in undesired modes, the external electrode of either or both crystals may be domed. A mercury delay line waveguide including these features is described and claimed in H. J. Mc- Skimin application Serial No. 653,255, flied March 9, 1946. Features of corresponding function for dielectric wave guides are described and shown in United States Patent 2,147,717 to S. A. Schel-- kunoif.
The pulse-modulated intermediate frequency waves l5 which are propagated over the delay line I8 and delayed thereby by a time interval Atz are then amplified, as necessary, as by an adjustable gain amplifier 2i. The intermediate frequency is removed by a detector 22 and the resulting pulses are supplied by way of a transformer 23 to an indicating device, for example to the vertical deflection plates 24 of a cathode-ray oscilloscope 25 which may be of conventional construction.
In known systems to which the present invention has not been applied, the pulse-modulated intermediate frequency energy also travels over a by-path I! which does not include any delay device, through a variable gain amplifier 21, a detector 28 which removes the intermediate freistic of all guided wave delay lines. the pulse shape at the far end of the line I8 is 2,4ao,oss
quency, and to the same vertical deflection plates.
24, in inverted phase.
When the object I is fixed and stationary, the spurts II of pulse-modulated intermediate frequency energy entering the delay line I8 and the by-path II from the demodulator I4 are all alike, recurring at intervals At1. If it were not for distortion in the delay line I8 the (n+1)th pulse arriving at the vertical deflection plates by way of the by-path would be exactly cancelled by the preceding nth pulse arriving by way of the delay line, so that no indication would appear on the screen of the cathode-ray oscilloscope 25.
This situation is illustrated in Fig. 2. But with a' moving object I, this cancellation does not take place. Because the later delayed pulse and the earlier undelayed one do not reach the vertical deflection plates 24 at the same instant, but at instants which differ by an amount proportional to the speed of movement of the object I, a signal is applied to the vertical deflection plates which is the difference between the signal propagated over the delay line I8 and the by-path signal. Furthermore any noticeable movement of the object I such as a change in its orientation without noticeable translation produces the same result by eilecting a difference between the magnitude of the earlier, delayed (nth) pulse and that of the later undelayed' (n+1) th pulse. Thus the system gives an indication of the presence of moving objects. This indication may easily include a measure of the object distance by various known expedients. For example, the cathode-ray oscilloscope beam may be swept horizontally at constant speed as by a saw-tooth wave voltage applied to the horizontal deflection plates 30, which sawtooth wave voltage may be derived from a sawtooth wave oscillator 3i synchronized with the multivibrator 3. With such an arrangement the indication due to the difference, either in magnitude or in time of occurrence, between the delayed pulse and the undelayed pulse, which is illustrated ference between these delays is equal to the multivibrator pulse period, 1. e.,'At2-At3=Atl. These relations are shown iri Figs. 4a to 4d. inclusive. Or, the auxiliary line length may be 6 the primary delay line length and its diameter that of the primary line, in which case At2= %At1 and Ata=%Ati. Any ratios will serve which satisfy the relations high impedance liquid such as mercury.
in Fig. 3, appears on the cathode-ray oscilloscope I screen as a pip whose location along a horizontal axis is proportional to the object distance. Various known refinements and modifications of the ranging feature may be employed as desired.
However, certain phase distortion is character- As a result,
not the same as that of the pulse applied to the near end, so that, even with a fixed object I there results incomplete cancellation between the later delayed pulse and the earlier undelayed one. The
resulting difierence signal from a large fixed object may be suificient to mask the desired signal from a smaller and more important moving object.
In accordance with the invention the later undelayed pulse is distorted to the same extent and in the same manner as the earlier delayed one, by passing the later pulse in the by-path II through an auxiliary guided wave delay line 35 having the same relative phase delay distortion coefficient as the primary delay line, but a different time delay Ats. For example, with liquid compression wave delay lines the auxiliary delay line 35 in the by-path Il may be provided with a transmitter T and a receiver R like those of the primary line I8 and may be of identical construction with the primary delay line I8 but having one-quarter the length and one-half the diameter of the latter. If these ratios are selected then the dimensions should be such that the delay due to the primary line is At2=4At1 and the delay due to the auxiliary line is Ata=' /4At 1, so that the dif- Thewave equation which describes this situation is where 1p =velocity potential of a disturbance to be propagated r=radial distance from tube axis 0=angular distance about tube axis ar=distance along tube axis (direction of principal propagation) t=time, and
v=propagation velocity in the unconfined medium.
On the assumption that each component part of any disturbance may be treated as periodic with an angular frequency w=2wf, then =(r, 0, which! Substitution in (1) gives 22 l m 1 932 W 5. r it"? ae ta a The standard method of solution is to assume substitute in (3) and divide by (4). This gives d e W+1L29=0 d R 1 dB 41' n W T17 (F where To is the radius of the delay line tube, and a is discussed below. These three equations have the solutions where A, B, C, D, E, and F are constants.
In the first equation n must be an integer because the value of 9 must repeat itself each time 0 increases by 21:- radions. If n=0 the velocity poaeeaoee f 7 tential is independent of i. e., the behavior has axial symmetry. In the second equation is the Bessel's function of the first hind of order n and K a o is the Bessels function of the second kind and of order 11.. Since the latter is infinite when r=0,
1 D can be set equal to zero for a cylindrical guide.
As explained in H. J. McSkim in application Serial No. 653,255, filed March 9, 1946, the im pedance of the etched or ground interior surfaces Jn(a) =0 (7) The various roots, a1, as, am, etc. of the Bessel functions of the various orders, J0, J1, J2, etc. are reproduced in the following table. Because they distinguish the various modes in which energy may be propagated through the, guide, they are known as modular constants.
. Mode 711 Order 1:
in which n indicates the order of the Bessel function and m the degree of the root, or mode of the oscillation.
For the usual case in which the delay line is driven by an axially vibrating crystal only the zero order vibration will be generated in which case the modular constants are given by the first line of the table above.
Similarly, for a low impedance medium such as a gas, confined in a tube having high impedance walls, the appropriate boundary condition is that the radial velocity, given by the negative radial derivative of the velocity potential, is zero at the walls. That is,
b F:)T0=O which gives, by differentiation of (6b),
The roots of various degrees (m) of this equation, for various orders 11 of the Bessel's function, are
In either case the complete solution of (3) is This expression represents a wave of frequency propagated in the a: direction, the propagation constant being a,, or
.'Y B-v' where a is the attenuation constant and p is the phase constant of the guide; i. e., the phase shift per unit length.
The "cut-off frequency of the guide is the frequency at which the propagation constant is zero. From (11) it is evidently Below this frequency the wave will be attenuated. At frequencies above the cut-01f it will be propagated without attenuation. When unattenuated propagation takes place, the phase velocity is given by From (11) at frequencies in the range of unattenuated propagation and not too close to the cut-ofi frequency, the total phase shift from end to end of the guide is given by This expression is seen to contain two terms. The first is directly proportional to frequency, which is desirable for undistorted transmission. The second is inversely proportional to frequency and therefore represents the relative delay of one component frequency as compared with another which gives rise to phase distortion.
However, it will also be observed that for each component frequency and for each root (1111, where m is the modular constant, that the distortion will be alike in two guides which are characterized by the same value of l/To In accordance with the invention use is made of this relation by providing an auxiliary wave guide delay line which has the same value of 1/70 as does the principal delay line, but, of course, a different length and therefore a different delay, and balancing the output of one against that of the other.
The manner in which this balancing or cancellation comes about may be formulated mathematically as follows. Referring to Equations 10, 11 and 14, the signal strength at the output of the primary delay line is proportional to the velocity potential due to a pulse which entered the line at time t. It may be written in complex form as Adjustment of the relative gains of the amplifiers makes the magnitudes of these two series alike, term for term, in which case Then each term of (15) may be balanced against the corresponding term of (16), giving, for the difference, a series of terms each of which is of the form From (14), series expansion of the bracketed term in (17) gives terms containing successive 4 powers of the quantity 1 l l i Bi l-i Ba i 01-42) +5 CT 1:;
When the dimensional relations of the invention are met,
so that each of these terms vanishes individually., Therefore the whole expression (17) for the difierence signal is equal to zero.
The principles of the invention are applicable to wave guide delay lines of many types other than those analyzed in detail above. In each case the relative phase delay is found to be some assignable function of the length and transverse dimensions, and it is only necessary, in order to practice the invention in its wave guide aspect, to provide an auxiliary guide in which this function is the same as it is for the principal guide but which has a difierent length and therefore a different signal delay, to apply the same signals to both, and to balance their outputs. The same principles may be applied to delay devices other than wave guides.
For the mathematical formulation of the behavior of wave guides of configurations and types other than the one analyzed herein, which are diagrammatically illustrated in Figs. 6 to 11, inclusive and from which may be derived the expressions given above for the relative phase delay coeflicients of rectangular guides, dielectric guides, absorptive compressional guides and solid elastic guides, compressional or torsional, reference is made to Electromechanical Transducers and Wave Filters, by W. P. Mason (Van Nostrand 1942); to United States Patent 2,147,717 to S. A. Schelkunofi; to United States Patent 1,775,775 to Harry Nyquist; and to Theory of Sound by Lord Rayleigh, vol. I, page 252.
What is claimed is:
1. In a pulse-reflection, object-detecting-andranging system, a. source of a sequence of pulse signals recurring at equal time intervals, means for radiating said pulsed signals in a desired direction, means for receiving only echo pulsed signals reflected from objects lying in the path of said radiated signals, a relatively long delay unit, a relatively short delay unit, the difierence in the delay of said units being equal to the pulse recurrence interval, the phase distortion coemcient of the short delay unit being substantially identical with the phase distortion coefficient of the long delay unit, means for launching said received echo pulse signals simultaneously into the proximate ends of both of said units, means associated with the distant end of each of said delay units for picking up signals propagated lengthwise of said delay unit, means for deriving a signal related to the difierence between the signal picked up from said longer unit and signal picked up from said shorter unit, whereby said received echo signals reflected from stationary objects lying in the path of said radiated signals will be precisely balanced out and measurable difference signals will be obtained only from reflecting objects which are in motion, and means for indicating said difierence signals along a timed sweep whereby the range of reflecting objects in motion onlyis indicated.
2. In a, pulse-reflection, object-detectingandranging system the combination with a source of pulsed signals recurring at equal time intervals and means for radiating said pulsed signals in a desired direction, of a signal receiver responsive only to reflections of said pulsed signals reflected fromcbjects'lying in the path of said radiated signals, a plurality of parallel transmission paths intermediate said source and said receiver, a primary delay unit having longitudinal and transverse dimensions in one of said paths, adaptedto introduce a. preassigned time delay into signals in said path and introducing undesired distortion in proportion to a specified function of said longitudinal and transverse dimensions, an auxiliary delay unit in another of said paths, having a delay differing from that of said primary unit by precisely the time interval between said recurring pulses and different longitudinal and transverse dimensions which impart to said auxiliary delay unit the same distortion function as said primary delay unit,.and means for balancing signals traveling by one of said paths against signals traveling by the other of said paths to produce a difierence signal only when said time of recurrence of said signals is changing whereby pulses reflected from objects in motion only will produce a measurable difierence signal.
3. In combination with a signal source and a signal receiver, a plurality of parallel trans,- mission .paths connecting said source to said receiver, a primary liquid delay unit in one of said paths, adapted to introduce a preassigned time delay into signals propagated through said unit in proportion to its length and introducing undesired distortion in proportion to its length and in inverse proportion to the square of its transverse dimensions, an auxiliary liquid delay unit in another of said paths, having a different length to the square of transverse dimensions, and different dimensions and the same ratio of length and means for balancing signals traveling by one of said paths against signals traveling by the other of said paths to produce a difierence signal.
4. In combination with a signal source and a signal receiver, a plurality of parallel transmission paths connecting said source to said receiver, a primary elastic solid delay unit in one of said paths, adapted to introduce a preassigned time delay into signals propagated along said unit in proportion to its length and introducing undesired distortion in proportion to the product of its length and the square of its transverse dimensions, an auxiliary elastic solid delay unit in another of said paths, having a difl'erent length and diiferent transverse dimensions and the same product of length and transverse dimensions, and means for balancing signals traveling by one of said paths against signals traveling by the other of said paths to produce a difference signal.
5. In combination with a source of a recurring sequence of signal pulses and a pulse signal receiver, a plurality of parallel transmission paths connecting said source to said receiver, aprimary delay unit having longitudinal and transverse dimensions in one of said paths, adapted to introduce a preassigned time delay exceeding the interval between successive signal pulses into pulse signals propagated therethrough and introducing undesired phase distortion into 12 said signals in proportion to a specified functiom of said longitudinal and transverse dimensions. an auxiliary delay unit in another of said paths, having a time delay equal to the difference between the time delay of said primary delay unit and the time interval between successive signal pulses, and having difierent longitudinal and transverse dimensions and the same phase distortion function of longitudinal and transverse dimensions as said primary delay unit, and means for balancing each pulse as propagated through said primary unit against a later pulse propagated through said auxiliary unit to produce a diflerence signal. I WARREN P. MASON:
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,129,669 Bowen Sept. 13, 1938 2,310,692 Hansell Feb. 9, 1943 2,416,895 Bartelink Mar. 4, 1947
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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2639420A (en) * 1946-02-18 1953-05-19 Us Sec War Radar system for moving target indication
US2650357A (en) * 1947-11-13 1953-08-25 Philco Corp Delay controlled pulse generator
US2656531A (en) * 1950-09-12 1953-10-20 Atlas David Device to permit radar contour mapping of rain intensity in rainstorms
US2697826A (en) * 1946-05-08 1954-12-21 Robert H Dicke Moving target indicating system
US2714205A (en) * 1945-03-24 1955-07-26 Grayson Harry Radar apparatus for distinguishing between moving and stationary objects
US2740963A (en) * 1951-01-29 1956-04-03 Gilfillan Bros Inc Automatic amplitude cancellation in moving target indicator
US2750499A (en) * 1950-01-14 1956-06-12 Nat Res Dev Circuits for ultrasonic delay lines
US2797410A (en) * 1950-07-28 1957-06-25 Rca Corp Radar moving target indication method and system
US3038155A (en) * 1955-05-02 1962-06-05 Csf Radar noise suppressing system
US3114110A (en) * 1951-05-01 1963-12-10 Irving H Page Fixed pulse rejection system for radar moving target indicator
US3274592A (en) * 1948-10-07 1966-09-20 Massachusetts Inst Technology Pulse echo moving object locator system

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2129669A (en) * 1937-03-30 1938-09-13 Bell Telephone Labor Inc Guided wave transmission
US2310692A (en) * 1939-06-16 1943-02-09 Rca Corp Method of and means for reducing multiple signals
US2416895A (en) * 1942-10-02 1947-03-04 Gen Electric Pulse signalling system

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2129669A (en) * 1937-03-30 1938-09-13 Bell Telephone Labor Inc Guided wave transmission
US2310692A (en) * 1939-06-16 1943-02-09 Rca Corp Method of and means for reducing multiple signals
US2416895A (en) * 1942-10-02 1947-03-04 Gen Electric Pulse signalling system

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2714205A (en) * 1945-03-24 1955-07-26 Grayson Harry Radar apparatus for distinguishing between moving and stationary objects
US2639420A (en) * 1946-02-18 1953-05-19 Us Sec War Radar system for moving target indication
US2697826A (en) * 1946-05-08 1954-12-21 Robert H Dicke Moving target indicating system
US2650357A (en) * 1947-11-13 1953-08-25 Philco Corp Delay controlled pulse generator
US3274592A (en) * 1948-10-07 1966-09-20 Massachusetts Inst Technology Pulse echo moving object locator system
US2750499A (en) * 1950-01-14 1956-06-12 Nat Res Dev Circuits for ultrasonic delay lines
US2797410A (en) * 1950-07-28 1957-06-25 Rca Corp Radar moving target indication method and system
US2656531A (en) * 1950-09-12 1953-10-20 Atlas David Device to permit radar contour mapping of rain intensity in rainstorms
US2740963A (en) * 1951-01-29 1956-04-03 Gilfillan Bros Inc Automatic amplitude cancellation in moving target indicator
US3114110A (en) * 1951-05-01 1963-12-10 Irving H Page Fixed pulse rejection system for radar moving target indicator
US3038155A (en) * 1955-05-02 1962-06-05 Csf Radar noise suppressing system

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