FM-CW radar apparatus

Abstract: An FM-CW radar apparatus is provided with: a transmitter unit (1, 2, 3) for the emission of frequency-modulated continuous carrier waves of bandwidth B; a receiver unit (6, 7) for the reception of echo signals reflected by a target, producing target-representing beat signals; a signal processing unit, to which the beat signals are applied, provided with: an A/D converter unit (8) for the sampling and digitisation of the beat signals; a first FFT processing unit (10) with the object of obtaining at least range information about a target; a second FFT processing unit (12) with the object of obtaining at least high resolution information about a target; a control unit (13), which makes the output signals, generated by the first FFT processing unit (10) and the second FFT processing unit (12), suitable for presentation on a display (14).

Description: The invention relates to an FM-CW radar apparatus provided with: a transmitter unit for the emission of frequency-modulated continuous carrier waves of bandwidth B; a receiver unit for the reception of echo signals reflected by a target, which originate from the carrier waves emitted by the transmitter unit, and for the generation of target-representing beat signals; a signal processing unit, to which the beat signals are applied, and which is equipped with: an A/D conversion unit for the sampling and digitisation of the beat signals; a first DFT processing unit, to which the sampled and digitised beat signals are applied with the object of obtaining at least range information about the target; a control unit which makes the output signals generated by the first DFT processing unit suitable for presentation on a display. The advantage of such a radar apparatus is that the emitted carrier waves are difficult to detect. This is due to the electromagnetic energy to be emitted being given off spread in time and distributed over a large bandwidth. In consequence of the spread in time the power is low, and in consequence of the relatively large bandwidth B the energy per frequency unit Δf is small. Radar apparatuses of the pulsed type exhibit the exact opposite: due to the emission of pulses, the electromagnetic energy is given off compressed in time. This implies that the power is high. For civilian applications, an FM-CW radar apparatus has the advantage, with respect to a pulse radar apparatus, that the modulated carrier waves cause little interference to other equipment, such as communication equipment. For military applications an additional advantage is that, for an adversary, it is virtually impossible to detect the modulated carrier waves of an FM-CW radar apparatus. This is because the energy per frequency unit Δf is so small that it is lost in noise. It is known that the range resolution ΔR of an FM-CW radar apparatus is substantially equal to C/2B, C representing the speed of light and B the bandwidth. If an N-point DFT processing unit is employed, the maximum detectable range R max = CN/4B . For quite some time the need has been felt for an FM-CW radar apparatus of longer range. It is known that doubling the maximum range (2R max ) can be achieved by halving the bandwidth B. It is also known that the maximum range of an FM-CW radar apparatus can be adjusted to R' max = k.R max (k ≧ 1 ; k ∈ R) by making the bandwidth equal to B/k. Thus, existing equipment (with the same N-point DFT processing unit) enables detection of a target at a larger range. However, since the bandwidth is reduced by a factor k, the detectability of the FM-CW radar apparatus is increased by the same factor. This implies that the advantage of an FM-CW radar apparatus, viz. the virtual undetectability of the emitted carrier waves, is lost. An additional disadvantage is that the range resolution decreases with a factor of k. The invention fully solves both problems, yielding an FM-CW radar apparatus of increased range, without deterioration of the detectability and the range resolution. A radar apparatus based on the FM-CW principle is known from US-A 4,568,938, where an FM-CW altimeter is disclosed. A spectral analyser for obtaining updated low resolution spectra plus one or more high resolution spectra at selected frequencies is known from "Signal Processing", vol. 14, no. 1, Jan. 1988, pp. 25-35. This known technique involves the successive application of three fast fourier transforms plus additional data combination and phase correction. The inventive radar apparatus is characterised in that: a modulation sweep of the frequency-modulated carrier waves occupies a time of k.T seconds, where k > 1 and k ∈ R; a DFT sample period of the first DFT processing unit occupies a length of time of T seconds, so that a modulation sweep covers more than one DFT sample period; the FM-CW radar apparatus is provided with a second DFT processing unit, to which is applied at least part of the first DFT processing unit's output signals, associated with one modulation sweep, and an output signal of said second DFT processing unit, containing target range information of a higher resolution than that generated by the first DFT processing unit, is applied to the control unit. An additional advantage is an improved detection of remote targets, because the beat signals are present during practically the complete sample period. It is remarkable that the output signals of the second DFT processing unit contain high-resolution range information of a range quant of the first DFT processing unit. The invention will be explained in detail with reference to the accompanying drawings, of which: Fig. 1 represents a typical FM-CW radar apparatus; Fig. 2A,B shows some known carrier wave patterns, of different ranges, which can be used with the radar apparatus of Fig. 1; Fig. 3 shows a carrier wave pattern according to the invention; Fig. 4 shows another carrier wave pattern according to the invention; Fig. 5 shows a third carrier wave pattern according to the invention. In Fig. 1 a typical FM-CW radar is shown. The radar applies FM-CW techniques to determine the range of a target. It can therefore be equipped with a transmitter (1, 2, 3) of very low output power. Using a sweep generator 1, an oscillator 2 and an amplifier 3, a CW signal, which is frequency-modulated, is emitted by way of a transmitting antenna 4. The echo signal collected by a receiving antenna 5 is applied to a receiver (6, 7) comprising a low-noise amplifier 6 and a mixer 7. By means of a power splitter 7a, part of the transmit signal is likewise applied to the mixer 7. Mixing of the transmit signal and the received echo signal yields a beat signal of beat frequency f b , which is the difference between the frequencies of the transmit signal and the received echo signal. The beat frequency f b is directly proportional to the range of the object which has (partially) reflected the emitted signal, see Fig. 2A. Consequently, by measuring the beat frequency, the range of the object can be determined. To this end the beat signal is applied to an A/D converter 8, which operates at a sample frequency f s . The output signal of the A/D converter 8 is applied to an input memory 9. The input memory contains each time N digitised and sampled beat signals originating from a sweep (see Fig. 2A). The N digitised samples of the beat signal stored in the memory 9 are applied to a DFT processing unit 10, which determines the frequency of the beat signal and hence the target range. The result of the calculation is stored in an intermediate memory 11. The range information stored in the intermediate memory 11 is applied to a control unit 13. In view of the present state of technology, said DFT processing unit will usually be arranged as an FFT processing unit. The control unit 13 generates a drive signal for a viewing screen, which in this case is of the LCD type. To enable the control unit 13 to determine the position on the screen 14 where a target is to be shown, an additional signal indicating the position of the transmit and receive antennas 4, 5 is furnished to it via line 15. To this end, the transmit and receive antennas 4, 5 are connected to a servo unit 16 which rotates the transmit and receive antennas and determines their azimuthal and/or elevation position. In Fig. 2A a typical pattern is shown of a frequency-modulated carrier wave, which is determined by the sweep generator 1. The bandwidth is designated B, and the length of time of the sweep T. The dotted curve represents the echo signal of a target. The difference between the frequencies of the transmitted signal and the reflected signal, the beat frequency, is designated f b and is a measure for the target range. The following equation applies: f b = B T . 2R C' (1) where R is the target range and C the speed of light. From formula (1) it follows that The sample frequency f s of the FFT unit 10 determines the maximum detectable beat frequency according to Combination of formulas (2) and (3) produces the following formula for the maximum detectable range R max : R max = C' 4B .f s .T (4) On the other hand the sample frequency f s is chosen such that a received echo signal of a modulation sweep is utilised to the maximum extent for the generation of target information, optimising the signal-to-noise ratio. This implies that f s = N . 1 T ; (5) in other words, an FFT calculation is performed using a maximum of N sampled and digitised numbers which have been obtained during T consecutive seconds. Combination of formulas (4) and (5) produces R max = CN 4B (6) If C and N are constants, formula (6) shows that the maximum range R max can be increased by decreasing the bandwidth B. The range resolution ΔR can easily be derived from formula (6): ΔR = C' 4B (7) As an example, Fig. 2B shows a maximum detectable range which is thirty-two times the maximum detectable range R max of Fig. 2A. The bandwidth B has been reduced to B′ = B/32 . As the same FFT processing unit is employed, the maximum detectable beat frequency f b max = f s /2 . However, now f b max corresponds with a maximum range R′ max = 32R max , see formulas (4) and (6). Fig. 2B clearly illustrates that the bandwidth B′ is smaller than the bandwidth B of Fig. 2A. The scales of Figs. 2A and 2B are adapted in order to show a clear picture. As a consequence, the transmitted microwave energy per frequency unit is thirty-two times higher. This, as explained before, increases the detectability of the radar apparatus. Moreover, there is an increased risk of interference of electro-magnetically sensitive equipment in the vicinity of the radar apparatus. From formula (7) it also follows that the range resolution ΔR′ has decreased to ΔR′ = 32ΔR . A possible waveform according to the invention of an FM-CW radar apparatus with an increased maximum detectable target range R′ max is shown in Fig. 3. The dotted line in the figure indicates that the maximum range corresponding to f b max = f s /2 has increased by a factor 32 relative to the maximum range associated with the modulation pattern of Fig. 2A. Because the length of time kT of a sweep has been increased (k = 32), the bandwidth B has remained the same. Consequently, the FM-CW radar apparatus operating in the mode according to Fig. 3 is not easier to detect than when operating in the mode of Fig. 2A. As explained before, the maximum detectable range is From formulas (6) and (8) it follows that the range resolution ΔR associated with the output signal of the FFT unit 10 has decreased by a factor k. According to the invention the range resolution ΔR can be improved by a factor (p ≦ k) if a second FFT processing unit is used. This means that, if p = k is chosen, the following formula applies substantially to the new resolution ΔR h From formula (9) it follows that the new resolution, henceforth referred to as super resolution, is independent of the adjusted maximum detectable range R′ max . According to the invention, the FM-CW radar apparatus is for this purpose equipped with a second DFT processing unit 12, which in this case is an M-point FFT processing unit. Because the maximum range R′ max of the radar apparatus equals 32R max , 1 ≦ k ≦ 32 applies. Suppose that the radar apparatus operates in a mode where R′ max = 32R max . This implies that the length of a modulation sweep is equal to 32T, see Fig. 3. The 32 output signals of the 32 consecutively executed FFT calculations are stored in the intermediate memory 11. If a target at a range R is required to be displayed with super resolution and if R ≦ R′ max , then this can be achieved in a way where the radar apparatus is switched from a search mode to a mode in which the radar antenna is trained on the target. On the basis of the signals originating from the first FFT processing unit 10, the target is displayed by the control unit 13 as a point target on the screen 14. Of the k = 32 results of the FFT calculations of one modulation sweep stored in the intermediate memory 11, p (p ≦ k) FFT results are applied to the M-point FFT processing unit 12. In this case, p = M = 32 has been chosen. The output signal of the M-point FFT processing unit 12 is applied to the control unit 13. The control unit 13 selects either the signal originating from the first FFT processing unit or the one originating from the second for display on the screen. The selection may be made by hand. The two signals can, of course, also be displayed simultaneously. If the output signal of the second FFT processing unit is selected for display, the resulting picture of the target concerned is 32 times enlarged relative to the picture originating from the first FFT processing unit 10. For the super resolution of the picture originating from the second FFT processing unit, the following applies (formula 9) The above statements can be demonstrated as follows (see also Fig. 3): The sample frequency f s of the first FFT processing unit is equal to f s = N T . Since the second FFT processing unit performs an FFT operation on the 32 consecutively obtained output signals of the first FFT processing unit, the following applies for the sample frequency f s (2) of the second FFT processing unit 12: At the start of each modulation sweep the phase of the transmit signal is reset to zero. Suppose that  r is the start phase of the beat signal of the r-th FFT sample period (0 ≦ r ≦ 31). The following applies:  r = ₀ + 2π f b r T (12) Here ₀ varies with the target range. The phase difference between two adjacent FFT sample periods r+1 and r then is: Δ =  r+1 -  r = 2π f b T (13) Suppose that the beat frequency f is equal to: where q ∈ {0, 1, 2, ..., 31} and in other words, the beat frequency f is written as a whole number of times the halved sample frequency of the first FFT processing unit 10, plus a residual term Δf which is smaller than half the sample frequency of the first FFT processing unit. Actually, the term in formula (14) is the smallest frequency difference that can be measured with the first FFT processing unit 10 and thus determines the corresponding range resolution (range quant) of the first FFT processing unit 10. Combination of formulas (13) and (14) produces: The phase difference Δ is built up in T seconds and corresponds with a frequency f' according to The second FFT processing unit measures a frequency f' according to formula (16). Since the maximum detectable frequency of the second FFT processing unit is equal to it follows that, of f', the second FFT processing unit measures only the frequency component Δf. For the frequency f'' measured by the second FFT processing unit, the following applies: f'' = Δf. (17) Loosely interpreted, formula (17) means that range information is measured within a range quant of the first FFT processing unit. For the frequency Δ(Δf), at least to be measured by the second FFT processing unit, the following applies: Consequently, for the associated range resolution ΔR h the following applies: where ΔR₁ indicates the resolution for k=1 (see formula (7)); i.e., the resolution of the first FFT processing unit when the radar operates at minimum range. If a modulation sweep comprises k FFT (first) sample periods, of which the results of p FFT calculations (p ≦ k) are applied to the second FFT processing unit (M ≧ p), the following generally applies for the resolution ΔR h : ΔR h = k p . C' 4B (20) The invention is not limited to modulation patterns whose time span covers the length of time T of an FFT calculation a whole number of times. It is possible, for example, for the FM-CW radar apparatus according to the invention to be provided with a mode whereby the sweep of a modulation pattern takes, say, 3.4T seconds and the bandwidth of the sweep is B. It will be evident that, in processing an echo signal, at least three complete FFT calculations can be performed. It can therefore be stated that, if the length of a modulation sweep is equal to kT (k ≧ 1; k ∈ R), for the maximum detectable range R′ max , applies that R′ max = k.R max , whereby R max is the maximum detectable range for k=1, i.e., the maximum detectable range when the length of a modulation sweep equals the length T of an FFT calculation. The remainder of the sampled and digitised echo signal, however, is in this case also applied to the first FFT processing unit, e.g. n points (n < N). For the other N-n points, zeroes are applied to the first FFT processing unit in the usual way. This can simply be realised by resetting the input memory 9 to zero before new information is applied. When the memory is filled for a newly executed FFT calculation, the non-used memory locations will contain a zero. It is also possible to read the input memory 9 in such a way that the periods T slightly overlap, which means that the results of a 3.4T seconds modulation pattern can deliver an input for four FFT calculations with length T. We have then a 20% overlap. The invention is not limited either to a specific form of the modulation pattern. For example, Fig. 4 shows an alternative form which yields, however, in a manner which is entirely analogous to what has been described before, the same beat frequency, which is a measure for the target range. For the wave pattern of Fig. 4, k = p = M = 4 has been chosen. In Fig. 5 a different version of a usable modulation pattern is shown. For clarity, the maximum detectable beat frequency f b = f s /2 is given with the corresponding ranges R max and R′ max . In this case, too, k = p = M = 4 has been chosen. As indicated before, the invention is not limited to the embodiment where p = k , but generally comprises p ≦ k. It is possible, for instance, to choose k = 32 and p = 16. Then, p = 16 results of FFT calculations, successively obtained by the first FFT processing unit and comprised within one modulation sweep, are applied to the intermediate memory 11. The p = 16 FFT results are subsequently applied to the 32-point second FFT processing unit. Additionally, 16 zeroes are applied to the second FFT processing unit. As described for memory 9, this can be realised by resetting the intermediate memory 11 to zero before the 16 FFT results are read. Usually, p = k will be chosen, to enable all available information to be utilised. M will preferably be chosen so that M = p ; hence, in this case, p = k = M = 32 has been chosen. Finally it should be noted that the above-described FM-CW radar apparatus can be used in a track radar as well as a search radar. In case of a track radar, the servo unit 16 is driven via line 17 in the usual way by the control unit 17, to ensure that antennas 4, 5 remain pointed at the target.

Claims: FM-CW radar apparatus provided with: a transmitter unit (1, 2, 3) for the emission of frequency-modulated continuous carrier waves of bandwidth B; a receiver unit (6, 7) for the reception of echo signals reflected by a target, which originate from the carrier waves emitted by the transmitter unit, and for the generation of target-representing beat signals; a signal processing unit, to which the beat signals are applied, and which is equipped with: an A/D conversion unit (8) for the sampling and digitisation of the beat signals; a first DFT processing unit (10), to which the sampled and digitised beat signals are applied with the object of obtaining at least range information about the target; a control unit (13) which makes the output signals generated by the first DFT processing unit (10) suitable for presentation on a display (14), characterised in that a modulation sweep of the frequency-modulated carrier waves occupies a time of k.T seconds, where k > 1 and k ∈ R; a DFT sample period of the first DFT processing unit (10) occupies a length of time of T seconds, so that a modulation sweep covers more than one DFT sample period; the FM-CW radar apparatus is provided with a second DFT processing unit (12), to which is applied at least part of the first DFT processing unit's output signals, associated with one modulation sweep, and an output signal of said second DFT processing unit (12), containing target range information of a higher resolution than that generated by the first DFT processing unit (10), is applied to the control unit (13). FM-CW radar apparatus according to claim 1, characterised in that the first DFT processing unit (10) is provided with an N-point FFT processing unit, which processes N input signals, sampled and digitised with a sample frequency f s , whereby the maximum detectable range of the radar is substantially given by: R max = CN 4B , C represents the speed of light and f s = N . 1 T ; the second DFT processing unit (12) is provided with an M-point FFT processing unit, where p output signals of the first FFT processing unit, successively obtained and associated with a modulation sweep of k.T seconds, are applied to the M-point FFT processing unit with p ≦ k, p ≦ M, p ∈ N, and where for the high resolution ΔR h substantially holds: FM-CW radar apparatus according to claim 2, characterised in that p = k . FM-CW radar apparatus according to claim 3, characterised in that p = k = M .

Inventors: REITS BERNARD JOZEF, REITS, BERNARD JOZEF
Applicants: HOLLANDSE SIGNAALAPPARATEN BV, HOLLANDSE SIGNAALAPPARATEN B.V.
Application year: 1990
Main classification: G01S13
IPC codes: G01S13, G01S7