[go: nahoru, domu]

GB2083966A - Frequency-modulation radar - Google Patents

Frequency-modulation radar Download PDF

Info

Publication number
GB2083966A
GB2083966A GB8127941A GB8127941A GB2083966A GB 2083966 A GB2083966 A GB 2083966A GB 8127941 A GB8127941 A GB 8127941A GB 8127941 A GB8127941 A GB 8127941A GB 2083966 A GB2083966 A GB 2083966A
Authority
GB
United Kingdom
Prior art keywords
signal
frequency
difference
target
transmitted
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB8127941A
Other versions
GB2083966B (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Allard Way Holdings Ltd
Original Assignee
Elliott Brothers London Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Elliott Brothers London Ltd filed Critical Elliott Brothers London Ltd
Priority to GB8127941A priority Critical patent/GB2083966B/en
Publication of GB2083966A publication Critical patent/GB2083966A/en
Application granted granted Critical
Publication of GB2083966B publication Critical patent/GB2083966B/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/40Means for monitoring or calibrating
    • G01S7/4052Means for monitoring or calibrating by simulation of echoes
    • G01S7/4056Means for monitoring or calibrating by simulation of echoes specially adapted to FMCW
    • 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
    • G01S13/06Systems determining position data of a target
    • G01S13/08Systems for measuring distance only
    • G01S13/32Systems for measuring distance only using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated
    • G01S13/34Systems for measuring distance only using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated using transmission of continuous, frequency-modulated waves while heterodyning the received signal, or a signal derived therefrom, with a locally-generated signal related to the contemporaneously transmitted signal
    • G01S13/343Systems for measuring distance only using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated using transmission of continuous, frequency-modulated waves while heterodyning the received signal, or a signal derived therefrom, with a locally-generated signal related to the contemporaneously transmitted signal using sawtooth modulation

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

In an FMCW radar ranging system, the modulation being of ramp form so that the return signal should exhibit a constant frequency difference dependent on the range delay, lack of linearity of the transmitted signal ramp causes false difference frequencies to arise which reduce ranging certainty. This is overcome by obtaining a target difference frequency signal as before and deriving a reference difference signal by feeding a portion of the transmitted signal into a fixed delay 13 and mixing 14 as for a target. The reference difference signal also, therefore, suffers from ramp non-linearities. A sampling signal of correspondingly irregular repetition rate is picked off 15 this reference difference signal and used to sample the target difference signal. The samples are therefore non-linearly distributed in time in a way which offsets the non-linearity of the transmitted frequency ramp. By treating the samples as though they were equally spaced in time, conventional narrowband frequency analysis can be used to derive the target ranges. <IMAGE>

Description

SPECIFICATION Radar ranging system This invention relates to frequency modulated continuous wave (FMCW) ranging systems.
Radar ranging systems commonly employ a frequency modulated continuous wave (FMCW) transmitted signal as an alternative to a pulse system to provide a time marker on the transmitted wave. If the transmitted signal is a microwave frequency swept through a predetermined range repeatedly and linearly, the frequency difference between the transmitted signal and the signal reflected from a target (the radar 'returns'} is a measure of the time lapse of the reflected signal and thus of the target range. Thus Figures 1 (a) and 1 (b) illustrate the basic FMCW Radar in which r.f. transmissions are radiated from an antenna, reflected from an object at a distance d metres, and return to the radar after a time At = 2d/c where c is the velocity of light.The transmitted frequency is made to increase linearly with time so that there is a difference Af between the transmitted frequency and the frequency of reflected signals.
Af is proportional to the time delay At of the reflected signals and to the rate of change of transmitted frequency df dt In orderto measure the range, d, it is therefore necessary to measure the difference frequency Af and to know the rate of change of transmitted frequency df/dt. Various methods have been published for controlling df/dt, one such method being described in US Patent Specification 4106020. The method there described corrects the measured value of range by detecting the difference frequency and counting the number of cycles over a period chosen to scale the count appropriately.
There are, however, many difficult applications where the return signals are weak compared with system noise, and multiple returns are present. High resolution filtering is therefore necessary to achieve a good signal to noise ratio and to resolve components from different ranges before the wanted signal can be detected. If this filtering is carried out by a narrowband filter, there is a limitation on the improvement available due to non-linearity in the transmitted tuning characteristic. Changes in df/dt cause the difference frequency to change, and so the returns from a fixed range will cover a band of frequencies, with a corresponding loss in output signal/noise ratio from a narrowband filter.A method of compensation is therefore required which is applicable before the signals are detected and which therefore enables high resolution filtering at the output.
According to the present invention, in a radar ranging system comprising a swept-frequency transmitter, a difference-frequency circuit providing a target difference-frequency signal of frequency equal to the difference between the transmitted and reflected signals, a sampling circuit for sampling the target difference-frequency signal and processing circuitry for deriving the target range from the values of the samples and their repetition frequency, a reference difference-signal is provided by the transmitted signal and a version thereof time displaced by a predetermined period, the sampling of the target difference-frequency signal being performed at the reference difference-frequency to avoid the effect of a non-linear frequency sweep.
The system may include means for producing an intermediate frequency (I.F.) signal from the outputs of the swept-frequency transmitter and a microwave local oscillator, and a delay line to which the l.F.
signal is applied, the resulting delayed l.F. signal being differenced with the undelayed I.F. signal to produce the sampling signal.
Several embodiments of a radar ranging system in accordance with the invention, will now be described, by way of example, with reference to the accompanying drawings, of which: Figure 1 shows a block diagram and associated frequency modulation diagram of a conventional FMCW radar system; Figure 2 shows a block diagram of a basic radar system according to the invention; and Figure 3 shows a modification of the system of Figure 2.
The basic system of Figure 1 has already been referred to. It incorporates a voltage tunable microwave oscillator 1, which is swept in frequency by the output of a ramp generator 2. The oscillator output is then applied to a circulator 3 having an output port connected to a transmitting and receiving antenna 4. The radar returns are received by the antenna and fed back to the circulator 3 which passes them on to a receiver including a mixer 5. The transmitted signal from the oscillator 1 normally achieves some leakage from the input port of the circulator 3 to the output port feeding the mixer 5.
The leakage portion of the transmitted signal and the reflected signal are mixed in the receiver 5 and a difference frequency signal produced. This leakage is indicated by a path 6.
As explained above, the frequency of this difference signal will depend upon the sweep rate of the transmitted signal and the time lapse between transmission and reception ofthe reflected signal. If the sweep rate is constant the difference frequency is proportional to the target range. If, however, as is commonly the case, the sweep rate is not constant, the difference frequency will vary throughout the sweep and will therefore not be a good indication of range.
A frequency analyser 7 is employed to measure the difference frequency, since in practice there will generally be returns from a number of different targets and hence the output of the differencing circuits will comprise a number of sine waves of different frequencies. The analyser samples the input signal at a predetermined sampling frequency, quantises the analogue samples and performs a digital analysis to determine the frequency of the signal (if a single frequency) or the frequencies of the components, if derived from a multi-target situation.
Clearly, a non-linear sweep will, since it produces frequency modulation, cause the analyser to indicate the presence of multiple targets when in fact there is only one present.
Figure 2 shows a basic embodiment of an FMCW radar incorporating the invention. The same arrangement of oscillator 1, ramp generator 2, circulator 3, antenna 4 and mixer 5 is employed as before. In addition however, to the production of the target difference-frequency signal, by way of the antenna 4 and circulator 3, a reference differencefrequency signal is produced by way of a coupler 9, a circulator 11 and a fixed delay circuit 13.
A portion of the transmitted signal is passed by the coupler 9 to the delay circuit 13 by way of the circulator 11. On reflection to the circulator 11, the delayed signal is applied to a mixer circuit 14 together with a 'leaked' portion of transmitted signal, as for the main mixer 5. The resulting reference difference signal is applied to a detector circuit 15.
The reference signal has a frequency which, in the same way as for the target difference signal, is dependent upon the sweep rate and the 'range' which is simulated by the delay 13. Since this delay is constant, the reference frequency varies solely in dependence upon the rate of change of frequency of the sweep signal.
On application to the circuit 15, the reference signal is detected, amplified and limited, to produce a 'square' waveform, the transitions of which provide sampling pulses in known manner. The repetition rate of these sampling pulses will then vary in exact correspondence with any departure from linearity of the sweep rate.
The target difference signal is derived by the circulator 3 and mixer 5, and applied to a sample-andhold circuit 16 which produces an analogue sample at the instant of each sampling pulse from the circuit 15. The sample-and-hold circuit also includes an analogue/digital converter which quantises the analogue samples to produce a series of digital sample values.
Assuming the sweep rate is non-linear these digital samples will arise at a rate which may, for example, increase throughout each sweep. This variation is, however, ignored by supplying them to a buffer store 18 at whatever rate they arise. They are then processed simply as a series of samples of constant time spacing and are analysed accordingly by a frequency analyser 7 to determine the apparent frequencies of the component or components, which are now directly related to target ranges.
The constant sample rate assumed by the analyser 7 in determining the frequency from the sample values may be the average value of the actual sampling rate or may be an arbitrary value which would have the effect of scaling the target difference frequency.
It may be seen that by means of the invention, if the target difference frequency increases throughout the sweep (without any change in target range) the sampling frequency is increased correspondingly so that samples are taken at the same point on the waveform (and thus have the same value) as if the difference frequency had been constant.
It has been assumed above that the delay imposed on the reference signal, although fixed, is arbitrary.
This is not so because analysis of a set of samples to determine the waveform(s) from which they arose requires that the samples occur at at least twice the frequency of the highest frequency component. In this case the highest frequency component will arise from the most distant target, i.e. from the upper limit of the range of targets that the system accommodates. Consequently, the reference difference frequency, i.e. the sampling frequency must be obtained from a delay (13) which is at least twice the time lapse corresponding to the upper limit of the target range.
In practice, it is not easy to obtain a significant delay with a mocrowave signal and one way of overcoming the difficulty is the arrangement of Figure 3.
In this arrangement a portion of the swept signal is applied to a mixer 20 which also receives a microwave local oscillator (19) signal of fixed frequency.
Thus the whole of the swept signal is shifted to a relatively low frequency band. This intermediate frequency (I.F.) signal is applied to a circulator 11 which passes it to a delay line 13. A significant delay is easily achieved at the low frequency and the reflected signal is mixed with the incident signal in the mixer 14 to provide the same reference difference signal for sampling as before.
In a further alternative, the delay 13 in Figure 2 is accepted at a low value easily achieved at the microwave frequency. The reference difference signal resulting is consequently of too low a frequency but is multiplied up in a phase lock loop by phase comparison with the divided output of a voltage controlled oscillator. The oscillator output itself then provides the reference signal of suitably high frequency.
The term 'target' has been used in this specification to denote the reflecting object but this does not of course necessarily imply any military significance.
In fact a prime application of the invention is in the determination of the topography of a coal mine and the control of automated mining operations.
It will be seen that the invention provides an FMCW ranging system in which compensation for non-linearities in the frequency modulation rate is achieved. The method of compensation remains effective in the presence of multiple returns and also when the signal to noise ratio is low.

Claims (4)

1. A radar ranging system comprising a sweptfrequency transmitter (1), a difference-frequency circuit (3) providing a target difference-frequency signal of frequency equal to the difference between the transmitted and reflected signals, a sampling circuit (16) for sampling the target difference-frequency signal and processing circuitry (7) for deriving the target range from the values of the samples and their repetition frequency, wherein a reference difference-frequency signal is provided (9, 11, 13, 14, 15) by the transmitted signal and a version thereof time displaced by a predetermined period, the sampling of the target difference-frequency signal being performed at the reference difference-frequency to avoid the effect of a non-linear frequency sweep.
2. A radar ranging system according to Claim 1, including means (20) for producing an intermediate frequency (I.F.) signal from the outputs of the swept-frequency transmitter (1 ) and a microwave local oscillator (19), a delay line (13) to which the I.F.
signal is applied, the resulting delayed I.F. signal being differenced (14) with the un-delayed l.F. signal to produce the sampling signal.
3. A radar ranging system according to Claim 1, wherein said reference difference-frequency signal is provided by multiplication of the frequency of a first signal derived by differencing the transmitted signal with a time-displaced version thereof, the necessary time displacement being then reduced in inverse proportion to the multiplication factor.
4. A radar ranging system according to Claim 3, wherein said multiplication is effected by a phaselocked loop having a controlled frequency input which is divided down to provide a signal the frequency of which is compared with that of said first signal to control said frequency input.
GB8127941A 1980-09-17 1981-09-16 Frequency-modulation radar Expired GB2083966B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8127941A GB2083966B (en) 1980-09-17 1981-09-16 Frequency-modulation radar

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8030085 1980-09-17
GB8127941A GB2083966B (en) 1980-09-17 1981-09-16 Frequency-modulation radar

Publications (2)

Publication Number Publication Date
GB2083966A true GB2083966A (en) 1982-03-31
GB2083966B GB2083966B (en) 1984-06-06

Family

ID=26276924

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8127941A Expired GB2083966B (en) 1980-09-17 1981-09-16 Frequency-modulation radar

Country Status (1)

Country Link
GB (1) GB2083966B (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2573217A1 (en) * 1984-11-13 1986-05-16 Trt Telecom Radio Electr DELAY SIMULATOR FOR FREQUENCY-MODIFIED CONTINUOUS WAVE DISTANCE MEASURING DEVICE
EP0234479A2 (en) * 1986-02-19 1987-09-02 IDEA, Incorporated Radar tank gauge
GB2219078A (en) * 1988-05-06 1989-11-29 Gersan Ets Identifying the position of objects or zones
EP0518442A1 (en) * 1991-06-14 1992-12-16 Philips Electronics Uk Limited FMCW radar range calibration appts
FR2747788A1 (en) * 1991-06-11 1997-10-24 Le Centre Thomson D Applic Rad Calibration and processing system for coherence of continuous radar with linear frequency modulation
WO2004008078A1 (en) * 2002-07-11 2004-01-22 Agilent Technologies, Inc. Delaying interferometer
WO2006035199A1 (en) * 2004-09-28 2006-04-06 Qinetiq Limited Frequency modulated continuous wave (fmcw) radar having improved frequency sweep linearity
WO2006103391A1 (en) * 2005-03-29 2006-10-05 Qinetiq Limited Coherent frequency modulated continuous wave radar
JP2008514910A (en) * 2004-09-28 2008-05-08 キネテイツク・リミテツド Frequency modulated continuous wave (FMCW) radar with improved frequency sweep linearity
US20150355318A1 (en) * 2014-06-04 2015-12-10 Rosemount Aerospace Inc. Enhanced rf detection system

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5206699A (en) 1988-05-06 1993-04-27 Gersan Establishment Sensing a narrow frequency band of radiation and gemstones

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2573217A1 (en) * 1984-11-13 1986-05-16 Trt Telecom Radio Electr DELAY SIMULATOR FOR FREQUENCY-MODIFIED CONTINUOUS WAVE DISTANCE MEASURING DEVICE
EP0182418A1 (en) * 1984-11-13 1986-05-28 Telecommunications Radioelectriques Et Telephoniques T.R.T. Delay simulator for a frequency-modulated continuous wave-ranging system
EP0234479A2 (en) * 1986-02-19 1987-09-02 IDEA, Incorporated Radar tank gauge
EP0234479A3 (en) * 1986-02-19 1989-11-15 IDEA, Incorporated Radar tank gauge
GB2219078A (en) * 1988-05-06 1989-11-29 Gersan Ets Identifying the position of objects or zones
GB2219078B (en) * 1988-05-06 1992-08-26 Gersan Ets Identifying the position of objects or zones
FR2747788A1 (en) * 1991-06-11 1997-10-24 Le Centre Thomson D Applic Rad Calibration and processing system for coherence of continuous radar with linear frequency modulation
EP0518442A1 (en) * 1991-06-14 1992-12-16 Philips Electronics Uk Limited FMCW radar range calibration appts
WO2004008078A1 (en) * 2002-07-11 2004-01-22 Agilent Technologies, Inc. Delaying interferometer
WO2006035199A1 (en) * 2004-09-28 2006-04-06 Qinetiq Limited Frequency modulated continuous wave (fmcw) radar having improved frequency sweep linearity
JP2008514910A (en) * 2004-09-28 2008-05-08 キネテイツク・リミテツド Frequency modulated continuous wave (FMCW) radar with improved frequency sweep linearity
US7592943B2 (en) 2004-09-28 2009-09-22 Qinetiq Limited Frequency modulated continuous wave (FMCW) radar having improved frequency linearity
AU2005288732B2 (en) * 2004-09-28 2009-11-26 Qinetiq Limited Frequency modulated continuous wave (FMCW) radar having improved frequency sweep linearity
WO2006103391A1 (en) * 2005-03-29 2006-10-05 Qinetiq Limited Coherent frequency modulated continuous wave radar
US7982661B2 (en) 2005-03-29 2011-07-19 Qinetiq Limited Coherent frequency modulated continuous wave radar
US20150355318A1 (en) * 2014-06-04 2015-12-10 Rosemount Aerospace Inc. Enhanced rf detection system
US9335405B2 (en) * 2014-06-04 2016-05-10 Rosemount Aerospace Inc. Enhanced RF detection system

Also Published As

Publication number Publication date
GB2083966B (en) 1984-06-06

Similar Documents

Publication Publication Date Title
US3969725A (en) Distance measuring equipment
US4176351A (en) Method of operating a continuous wave radar
US4568938A (en) Radar altimeter nearest return tracking
US3774206A (en) Pseudo-randomly phase modulated radar altimeter
US6211812B1 (en) Quiet radar method and apparatus
US4008475A (en) Stabilizing and calibration circuit for FM-CW radar ranging systems
US5731782A (en) Ranging systems
US4245221A (en) FM-CW Radar ranging system with automatic calibration
US4359779A (en) FM Transmitter with frequency ramp phase and amplitude correction means
US4635060A (en) Coherent-on-receive radar with prephase correction circuit
GB2083966A (en) Frequency-modulation radar
US3715753A (en) Coherent range and length resolution
US2517549A (en) Pulse radar system for detecting moving objects
US4435709A (en) Radar ranging system for use with sloping target
US3577144A (en) Distance measuring systems
US4860014A (en) Doppler radar with multiphase modulation of transmitted and reflected signal
US3065465A (en) Distance measuring devices
EP0048170B1 (en) Radar ranging system
US3112481A (en) Continuous wave frequency modulation distance measuring apparatus
US2913717A (en) Moving target radar system
US4567484A (en) Doppler radar measuring apparatus
US4065768A (en) Radar apparatus
US2678440A (en) Airborne moving target indicating radar system
US4121212A (en) Double sideband pulse radar
US2555121A (en) Moving target indication radar system

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee