GB2291301A - Signal processing apparatus and method - Google Patents
Signal processing apparatus and method Download PDFInfo
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- GB2291301A GB2291301A GB9421466A GB9421466A GB2291301A GB 2291301 A GB2291301 A GB 2291301A GB 9421466 A GB9421466 A GB 9421466A GB 9421466 A GB9421466 A GB 9421466A GB 2291301 A GB2291301 A GB 2291301A
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S13/00—Systems 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
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/06—Systems determining position data of a target
- G01S13/08—Systems for measuring distance only
- G01S13/32—Systems for measuring distance only using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated
- G01S13/34—Systems 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
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- General Physics & Mathematics (AREA)
- Radar Systems Or Details Thereof (AREA)
Description
2291301 1 SIGNAL PROCESSING APPARATUS AND METHOD This invention relates to
a signal processing apparatus and method and in particular to apparatus and methods for use in rf transmission systems operating with Frequency modulated continuous wave (FMCW) type waveforms.
The invention enables a waveform, for use in a radar system for example, to he generated which is optirnized for peak power limited transmission systems by minimising the peak- to mean ratio whilst simultaneously providing exceptionally good out-of-band emission characteristics and conventional radar waveform properties. Consequently, the method is very suitable for use with non-linear transmission systems, for example those employing a high power amplifier in compression which are required to comply with tight out-of-band spectral emission specifications.
In a conventional radar transmit sub-system FMCW waveform generation can be accomplished by either direct rf synthesis or baseband synthesis followed by up conversion.
Either technique can be implemented in analogue or digital technology. The disadvantages of rf synthesis are two fold. Firstly, the waveform flexibility is limited by either the precision in the analogue components, for analogue systems, or the computational rate for digital systems.
Secondly, the dynamic range andlor linearity of such implementations are frequently technology limited.
The disadvantage of baseband synthesis followed by up-conversion is that the precision 1) generated in a baseband synthesized waveform is in practice difficult to preserve in the up- C convertion and amplification stages because analogue mixers are by definition non-linear devices and for reasons of efficiency high power amplifiers often operate with some compression.
The problem therefore is how to preserve the fidelity of a precision generated waveform through a system with a non-linear transfer function. when, as is well known, passage of a bandlimited signal through a non-linearity results in out-of-band emission and in-band c distortion. Out-of-band emission wastes power and causes interference with other users of the band and often international regulations governing the extent of this exist while in-band distortion results in a degradation or loss of the waveforms properties.
Fundamentally, an ideal transmitted waveform must be simultaneously power efficient, bandwidth efficient and preserve the integrity of the general waveforms natural properties. To explain these subtle ideals a little further:
A maximaBy 'power efficient' waveform is one in which the ratio of the peak to mean temporal magnitude envelope is unity.
t_ A 'bandwidth efficient' waveform is one in which all of the power transmitted is uniformly 'contained' within the sweep/receiver bandwidth. Power transmitted out-of- band may not only interfere with other users but, from the radar point of view, is a system loss - since it serves no useful purpose whatsoever in the process of target detection.
3 Preservation of a waveforms natural properties is taken to mean minimisation of in-band distortion for both amplitude and phase. In this way, a waveform which has very good correlation properties is not compromised by the transmission path. It is often the case that a waveform with, say, very low time-sidelobes in correlation is very sensitive to phase distortions or bandwidth mismatch.
This invention provides a signal processing method and apparatus for producing and employing waveforms coming closer to this ideal than has previously been possible.
In a first embodiment this invention provides signal processing apparatus employing a waveform having a waveform repetition interval and bandwidth related such that the product of the waveform repetition interval and the bandwidth is an integer.
Preferably the waveform comprises a plurality of identical sweeps, each sweep having a waveform repetition interval and bandwidth such that the product of the waveform repetition interval and the bandwidth is an integer and may further comprise a series of dwells each comprising a plurality of identical sweeps.
Advantageously a window function can be applied at the start and finish of each dwell Z in order to remove the boundary discontinuity at the start and finish of the dwell. A suitable window function is a Tukey window function.
Advantageously the frequency spectrum of the waveform can be weighted, preferably by applying a window function such a Tukey window function to it.
4 In a second embodiment this invention provides a window function comprising a co?x function in which n is non zero and positive convolved with an extending function having a C5 1 constant non-zero value across a single continuous range and a value of zero elsewhere.
In this case a window function Wz can be used defined by the equation; where W -L X n E G E C9 C-X XZ-X : Z ---(X-Y)....,(X-Y) = COJL1 kl+k 1 x = -X,,V n,.tO Ey = 1 Y = -Y,,Y (X-F) Cg = -L F, W, N.-(x.y) Preferably the window function is the square root of the result of the convolution. In this case a window function Wz can be used defined by the equation; where = 1 G E:z=-(X+Y),,(X+Y) C9 X Z-X Gn = cos"(L7r) X l+k_ x = -X,...X n>-0 Ey = 1 Y = Y,,Y 1 (X.In C9 = - E W N - (x.,n A particularly advantageous arrangement of signal processing apparatus provided by the fast embodiment of the invention is to weight the waveform frequency spectrum in such signal processing apparatus with a window function provided by the second embodiment of the invention. When this is done the value of the index n in the window function can be selected to minimise the peak, to mean ratio of the waveform, the preferred way of doing this being to select the value of the index n such that the first and second Fresnel peaks in the waveform envelope magnitude function have equal magnitude.
In a third embodiment this invention provides a method of generating a waveform by defining the waveform repetition interval (T) and bandwidth (B) such that T.B. = an integer. Preferably the waveform is generated by then evaluating the equation m g(t) = (1-T-B). F, G..e j('2 ' b" ' ') n=-M 6 where M = (TB-1)12 [Gj1j, M 3 =-M Advantageously the variables a, b and c can be defined as; a = HITB b = 211(t/7) and c = -R [-1 UZI + M + 11 for phase continuity (TB odd case only) 4 2.
In a fourth embodiment this invention provides a signal processing method employing a waveform having a waveform repetition interval and bandwidth related such that the product of the waveform repetition interval and the bandwidth is an integer.
Preferably the waveform comprises a plurality of identical sweeps, each sweep having a waveform repetition interval and bandwidth such that the product of the waveform repetition interval and the bandwidth is an integer and may further comprise a series of dwells each comprising a plurality of identical sweeps.
7 Advantageously a window function can be applied at the start and finish of each dwell to remove the boundary discontinuity at the start and finish of the dwell. A suitable window function is a Tukey window function.
Advantageously the frequency spectrum of the waveform can be weighted, preferably by applying a window function such a Tukey window function to it.
It is particularly advantageous for a signal processing method according to the fourth embodiment of the invention to weight the waveform frequency spectrum with a window function provided by the second embodiment of the invention.
Apparatus and methods employing the invention will now be described by way of example only with reference to the accompanying diagrammatic figures in which; Figure 1 shows the frequency spectrum of a typical conventionally generated waveform; Figure 2 shows the frequency spectrum of a waveform produced employing the invention; Figures 3A to 31) show the frequency spectra of waveforms produced conventionally and employing Tukey windows; Figures 3E to 31-1 respectively show the frequency spectra of waveforms corresponding to those in Figures 3A to 31) respectively and produced employing the invention and Tukey 8 windows; Figures 4A to 41) are explanatory diagrams showing Tukey dwell weighting functions and Figures 4E to 4H respectively show the waveform spectral occupancies produced by the c Tukey dwell weighting functions of Figures 4A to 4D respectively.
Z1- -- Z71 Figures SA to 5D are explanatory diagrams showing Tukey spectral weighting functions C_ Z-- having different values of taper; Figures 5E to 514 respectively show the waveform envelopes corresponding to the Tukey functions of Figures SA to 51) respectively; Ficure 6 shows a full definition of the new window function according to the invention; c Figures 7A to 71) show examples of the new window function for different values of n and haviner 100% taper., L, Fi ures 7E to 71-1 respectively show the spectral ma t> 9 gnitudes corresponding to the windows shown in Figures 7A to 7D respectively; FiCrures 8A to 81) show the new window function for different values of n with 50% taper; 9 Figures 8E to 8H respectively show the spectral magnitudes corresponding to the Z, window functions shown in Figures 8A to 8D respectively; Figures 9A to 91) show the cos'Tukey spectral weighting function with 20% taper for different values of n; Figures 9E to 9H respectively show the waveform envelope magnitude functions corresponding to the spectral weighting functions of Figures 9A to 9D respectively; Figures 1 OA to 1 OD show the square root cosrukey spectral weighting function for 20% taper different values of n; Figures lOE to lOH respectively show the waveform envelope magnitude functions corresponding to the spectral weighting functions of Figures I OA to I OD respectively; Figures 11Ato 1 1H show different waveform characteristics foran optimised squareroot cos'Tukey spectral related waveform; Figure 12 is a table of some optimum values of index n for various waveform parameters.
4:5 Figure 13 shows the spectral occupancy of an optimised waveform; and Figure 14 shows signal processing apparatus for use in a radar system employing the invention.
In conventional waveform generation over a time interval (T) a bandwidth (B) is swept in a linear manner, i.e. f = + BUT.
1 Since frequency can be defined as the rate of change of phase with respect to time, f = d4)ldt the phase (h of a time-domain signal g'(t) is obtained by integration.
i.e.
Hence t:
gl(t) = A(t).e im (f d', 0 g,(t) = A(t).e j21Iff i - (M). (L11)2) for t < T12 where, A (t) is some amplitude scaling factor (usually 1).
It is a popular misconception that the spectral occupancy of a linear frequency modulated waveform (LFM), commonly known as a chirp, contains just those frequencies of the swept bandwidth. It does not. Such a signal is a time-limited signal and it is a physical fact that 'if a signal is time-limited it cannot be simultaneously bandlimited and vice versa.
Consequently, the digital representation of a chirp suffers from aliasing unless oversampled by a considerable amount.
205 A radar or sonar often uses a waveform termed a "dwell" and comprising a number of sweeps. In such a case the dwell waveform g"(t) (also time limited) is obtained by replicating the time-limited signal g'(t) at intervals of T M-, g"(t) = g(t) - E 6(t-kl) k=o 210 where represents convolution Ns = Number of sweeps in a dwell T = waveform repetition interval (WRI) Such a signal (depending on the values of T and B) may or may not be continuous, i.e.
215 it may not or may posses discontinuities in either amplitude or phase or their derivatives at the WRI boundaries.
In the optimum case, the waveform is continuous and as a result the frequency spectrum or spectral magnitude has a line structure with a line spacing dependent on the dwell time rather 220 than the WRI. However in the strict sense this is still not bandlimited as there are an infinite number of these lines. Hence the problem in digital representation. An example of such a frequency spectrum is shown in Figure 1.
In Figure 1 it can be seen that the spectral occupancy of the waveform extends far 225 beyond that of the design bandwidth B. It can be further seen that the spectral line peaks in-band are of different magnitude due to the Fresnel ripples. This also is undesirable because it increases the peak to mean ratio of the waveform, making it less power efficient.
12 In the present invention the method of waveform definition and generation is completely 230 different from that of the conventional approach hereinbefore described, and is described below as a series of steps. Although the greatest benefits can be obtained by use of all the steps it must be emphasised that some benefit can be obtained by using only some or even only one of them in isolation from the others.
235 Step 1 Define a relationship between the waveform parameters T and B, i.e.
T x B = integer In this way, the waveform is defined as true 'periodic bandlimited waveform' containing C) no discontinuities at the WRI boundaries. Such signals are entirely defined by a line spectrum 240 comprising a finite set of lines rather than an infinite set. Consequently, the waveform can be defined not only in the instantaneous frequency-domain (as is the case of the conventional chirp) but also in the normal frequency domain as comprising a finite set of unit spectral lines of 1/WRI spacing, that is spaced at the waveform repetition frequency, quadratically phased. As a result the waveform can be exactly represented by digital samples and the waveform can be precisely defined in the frequency domain even though it is time limited. In order to exactly represent a conventional (non-bandlimited) chirp waveform digitally it would theoretically be necessary to c have an infinite sampling rate. In practice a sampling rate high enough to give acceptable results t -- C_ - is used but a trade off between accuracy of representation and sampling rate must always be made.
250 The number of spectral lines in the desiCrn bandwidth is T.B.
i 13 This is the only way of defining a waveform that is perfectly bandlimited and this provides great advantages in baseband synthesis because it allows the synthesised waveform to 255 be an exact representation of the desired waveform.
Step 2 The basic waveform is obtained in the time-domain by means of a inverse finite Fourier series (or polynomial). That is to say:
260 m g(t) = (1 -TB). E G,,x j(' ' b" n=-M where M = (TB-1)12 a = ICUTB b = 2H(t/27) c = 11 [-1 TB2 + M + 11 for phase continuity (TB odd case only) 4 2 14 {Gj 13 m ,=-M 265 Since the above equation is expressed in terms of the continuous variable T it is valid for all values of time.
Therefore a dwell waveform g" (t) can be evaluated directly without the need to replicate 270 a WRI waveform g'(t) as in the conventional case. Although this could be done if there was some practical advantage in doing so.
C) Furthermore, since the function is exactly bandlimited the approach lends itself to digital synthesis.
275 Other values for the variables a, b and c can be selected to allow other phase-coded waveforms to be generated by this method if desired.
Waveforms generated in this way can be 100% power efficient when they are not 280 amplitude modulated since they can have a peak- to mean ratio of 1 and all of the transmitted power can be contained within a set design bandwidth. It is possible to trade off bandwidth against power efficiency because as the bandwidth is reduced the power efficiency will drop and vice-versa since power transmitted outside the designed bandwidth is wasted in a radar or sonar system.
285 SLCJL Digital baseband samples of the waveform are simply obtained by evaluating the above equation at discrete values in time i.e. replace the continuous variable T with k 290 So long as the sampling frequency M',r is greater than the design bandwidth B, Nyquist's rule is satisfied and the samples will be an exact representation, in the sampling theorem sense, of the waveform. In contrast samples taken at the same rate of a conventional time-domain generated chirp can never be an exact representation due to the infinite member of lines in the frequency spectrum.
295 300 In radar and sonar systems the received and transmitted signals are correlated in order to identify where the received signal has been returned from, the fact that the digital samples of the waveform produced according to the invention are an exact representation of the waveform improves the temporal robustness of the waveforms when correlated.
Figure 2 illustrates the basic spectral occupancy characteristics of the polynomal waveform evaluated from the above equation for TB = 5 and 1 = 8.
When compared with the conventional case of Figure 1 it can be seen that the number 305 of lines is finite as expected and the out-of-band emission is entirely determined by the sidelobes of the sinc due to the finite dwell. Furthermore the in-band lines are of uniform magnitude.
Unlike the conventional waveform the number of sweeps in a dwell directly affects the out-of-band emission levels since the width of the sinc is inversely proportional to the dwell- 16 310 time.
Consequently, for a given sidelobe roll-off rate, a doubling in Ns will double the roll-off rate. This is a very important feature since most practical radar or sonar waveforms comprise a relatively large number of sweeps per dwell (typically 256) and as a result will automatically 315 have a very high sidelobe roll of rate, reducing out of band emissions.
Both Figure 1 and 2 illustrate a typical spectral template for out-ofband emission levels to allow simple comparison between the conventional and inventive waveforms.
320 Step 4 Since the out-of-band emission level is entirely determined by the finite dwell-time, further improvements in out-of-band suppression can be achieved by application of a window function across the dwell.
325 However, in order to minirnise the weighting loss the essential requirement is to minimise the discontinuity at the start and end of the dwell. This can be accomplished by means of a Tukey window function, that is a window function having a raised cosine start and end taper of small percentage taper. Weighting loss is defined as; C & L_ 330 Weighting loss (db) = 1 N-1 log E Wk N M 17 Figures 3A to 31) illustrate the effect of application of a 3,125% taper Tukey window on a conventional waveform for N, = 2,4, 8 and 16 respectively while figures 3E to 311 respectively show the corresponding polynon-fial waveforms according to the invention. In the case of the 335 conventional waveforms it will be noted that the peaks of the out of band lines do not decay with increasing Ns. Whereas in the case of the new waveforms the increased decay rate is dramatic.
Thus the invention gives a very considerable improvement in out-of-band suppression for minimal weighting loss, (. 1Mb).
340 Since the raised cosine end tapers of the Tuk-ey window place the discontinuity into the second derivative the decay rate is.1 8dBloctave increasing by Adbloctave for each doubling of Ns.
Whilst increasing the percentage taper also improves the situation this is considered 345 undesirable since the weighting loss will become more significant. The effects of increasing percentage taper are shown in Figures 4. Figures 4A to 41) show the dwell weighting functions for Tukey windows with 0%, 10%, 20% and 40% taper respectively while Figures 4E to 414 respectively show the corresponding waveform spectral occupancies for the inventive waveform with N, = 4.
350 355 S1212 5 Having improved the out-of-band emission levels by dwell weighting a polynomal waveform consideration is now given to simultaneously improving the peak to mean ratio.
In the time-domain the magnitude of g(t) contains the Fresnel ripples - as illustrated by Z__ -- 18 Figures 5E to 5H.
These ripples (in excess of Mb relative to the mean) for a peak- power limited system are a problem since to avoid saturation (or clipping) it is necessary to reduce the effective 360 transmitted power.
i:
Consequently, it is very desirable to minimise this ratio by some means. It has been found that the application of spectral tapering has this effect.
Figures 5 illustrate the effect of application of a Tukey windows of 0, 10, 20 and 30% taper on the design spectral magnitude 1 Gn 1 on the time-domain amplitude envelope. Figures 5A to 51) show the Tukey spectral weighing functions and Figures 5E to 5H the corresponding time domain waveform envelope magnitude functions for Tukey windows of 0, 10, 20 and 30% taper respectively. It can be seen that as the % taper is increased there is a corresponding 370 decrease in the peak-to-mean ratio.
365 Step 6 A further extension of this idea is to change the raised cosine shape of the end taper so as to minimise the effect of the taper on the in-band signal.
375 In order to do this a new window function has been invented dubbed cosP - Tukey.
This window function is generated by convolving a cosx function with what is termed an 'extendina function' and a full definition of the new window function is given in Figure 6.
4:1 C> 19 380 The ratio of the number of elements in the generating window to extending function determines the % taper whereas the index 'n' determines the shape of the taper.
It will be realised that the co?-Tukey window function can be used generally in any 385 application where window functions are employed, but as will be explained it is particularly advantageous in conjunction with waveforms produced by the above method.
Figures 7A to 7D illustrate the cos-Tukey window with 100% taper for n = 0, 1, 2 and 3 respectively while Figures 7E to 7H respectively show the corresponding spectral magnitudes.
390 It will be noted that when n = 0 a triangular window results.
When n = 1 a raised consine window results. And for every integer increase in 'n' the sidelobe roll-off rate increases by.6dBloctave.
395 Figures 8A to 811 illustrate the same scenario as in Figures 7 for the cos'-Tukey window with 50% taper.
Figures 9A to 91) show the cos'Tukey spectral weighting function with 20% taper for 400 n=O, 1, 2 and 3 respectively while Figures 9E to 911 respectively show the corresponding waveform envelope magnitude functions.
Application of cos'Tukey window to the design spectral magnitude for a fixed 20% taper and n = 0, 1, 2 and 3 is shown in Figures 9. It can be seen that the shape of the window affects 405 the peak-to-mean ratio as well as the sidelobe roll of rate.
A further step in this process is to take the square root of the window to produce a window function dubbed the square root co?Tukey window function. The effect of this is shown in Figures 10. Figures 1 OA to 1 OD show the square root cos, Tukey spectral weighting 410 function with 20% taper for n = 0, 1, 2 and 3 respectively while figures 1 OE to 1 OH respectively show the corresponding waveform envelope magnitude functions.
This has the effect of leaving more energy in-band but it also reveals a feature which is further exploited. If Figure 1 OE is exan-tined it can be seen that a second peak emerges which 415 in this case is larger than the first. In Figure 1 OF when n= 1 this second peak is still visible but is now smaller than the first.
From this observation is concluded a very important point:
420 425 Minimum peak-to-mean ratio occurs when the size of the first and second amplitude envelope peak are equal. In other words the energy in the first peak which dominates the peakto-mean ratio is equal split between two peaks. For the case illustrated in Figures 10 this implies that there is an optimum value of 'n' which exists somewhere between 0 and 1.
It turns out that it exists at n = 0.4601. Figures 11 illustrate the complete waveform characteristics for this case.
1r 21 llA llB llc III) llE llF I1G With reference to Figures 11; Design spectral magnitude with 20% square root cos" - Tukey Window. Design quadratic phase. Amplitude envlope of waveform in the time-domain illustrating equal peaks. Corresponding time- domain phase of waveform notice also quadratic. Real and Imaginary components of waveform illustrating generated chirp. Corresponding instantaneous frequency response. Circular correlation function of waveform - Note that since it was a window applied to the spectral magnitude in waveform design the circular correlation function is the transform of window. Hence. 1 8dB/oct are time sidelobe roll off rate.
1 1H Dwell weighting function 3.125% Tukey.
440 The optimum value of the index 'n' to minimise peak to mean ratio is a function of TB and the percentage spectral taper and can be computed beforehand so that it can be used as a look-up table or could be calculated in real time for each desired waveform. Figure 12 is a table of some optimal values of 'n' found by computer optimisation for TB's in the range 20 to 100 for 445 the case of 30% spectral taper.
Fiaure 13 illustrates the spectral occupany of an optimized waveform for TB=21, Ns = 64. It can be seen that in comparison to the conventional chirp illustrated in Figure 1 there is a dramatic improvement in the outof-band emission levels. Minimum peak-to-mean (i.e. <0.9d13) provides an optimal compromise between bandwidth efficiency and power efficiency and minimises the effect of non-linearities.
Ficrure 14 shows signal processing apparatus for use in a radar system employing C, -- Z:1 waveforms produced using the techniques described above. The waveforms are produced by a digital waveform generator 1 and supplied as a series of baseband samples spaced to form an 455 exact replica of the waveform to an upconverter and drive 2. The r.f. signal from the upconverter 2 is supplied to a high power amplifier 3 which is connected to an antenna 4 for transmission.
In practical apparatus of this type the upconverter 2 and amplifier 3 will be non-linear 460 and the use of the inventive waveform definition techniques described above allow waveforms minimising the effects of these non-linearities to be produced.
23
Claims (1)
1. Signal processing apparatus employing a waveform having a waveform repetition 0 interval and bandwidth related such that the product of the waveform repetition interval and the bandwidth is an integer.
465 470 475 480 2. Signal processing apparatus as claimed in claim 1 in which the waveform comprises a t> plurality of identical sweeps, each sweep having a waveform repetition interval and bandwidth such that the product of the waveform repetition interval and the bandwidth is an integer.
3.
4.
5.
6.
Signal processing apparatus as claimed in Claim 2 in which the waveform comprises a series of dwells, each comprising a plurality of identical sweeps.
Signal processing apparatus as claimed in claim 3 in which a window function is applied at the start and finish of each dwell.
Signal processing apparatus as claimed in claim 4 in which the window function is a Tukey window function.
Signal processing apparatus as claimed in any preceding claim in which the frequency spectrum of the waveform is weighted.
485 7. Signal processing apparatus as claimed in claim 6 in which the waveform frequency CI spectrum is weighted by applying a window function to it.
24 8. Signal processing apparatus as claimed in claim 7 in which the window function used 485 is a Tukey window function.
Z 9. A window function comprising a co?x function in which n is non zero and positive convolved with an extending function having a constant non-zero value across a single continuous range and a value of zero elsewhere.
490 10. A window function as claimed in claim 9 in which n is 1.
11. A window function as claimed in claim 9 or 10 where the window function Wz is defined by the equation; 1 X R W... E G E,, ==-(x+y),...,(xy) C9 --XX 495 where a G = cos" =: x = -4,X n!0 j X (1 -+k) Ey = 1 Y = Y,,Y 1 (x.n C9 = E W_.
N, (x.y) 12. A window function as claimed in claim 9 or claim 10 in which the square root of the result of the convolution is used as the window function.
500 13. A window function as claimed in claim 12 where the window function Wz is defined by the equation; W =-1:z=-(X+Y),...,(X+Y) c. F, G. E,,, g a=-X where G n = cos" 1-xlr x = -X,,X n..O X -l+k) Ey = 1 Y = -Y,,Y -1 (X+F) C9 = E W, N, (7, P) 505 14.Signal processing apparatus employing a window function as claimed in any one of claims 9 to 13.
15. Signal processing apparatus as claimed in claim 7 in which the waveform frequency spectrum is weighted by a window function as claimed in any one of claims 9, 10 or 12.
510 16. Signal processing apparatus as claimed in claim 7 in which the waveform frequency spectrum is weighted by a window function as claimed in claim 11 or claim 13.
26 17. Signal processing apparatus as claimed in claim 16 which employs a waveform spectrally weighted by the application of a window function in which the value of the index n is selected to minimise the peak to mean ratio of the waveform.
515 J z 18. Signal processing apparatus as claimed in claim 17 in which the value of the index n is selected to make the first and second Fresnel peaks have equal magnitude.
520 19. A method of generating a waveform by defining the waveform repetition interval (T) and bandwidth (B) such that T.B. = an integer.
20. A method of generating a waveform as claimed in claim 19 in which the waveform is generated by evaluating the equation.
525 m g(t) = (I IrTT). F, G,,x J('2 b ') R-M where M= (TB - 1)12 {G. = 13n m M 21. A method of generating a waveform as claimed in claim 20 in which a = RITB b = 2H(t/7) 27 and 111 H TB-1 C = - + M + 11 for phase continuity (TB odd case only) 4 2 22. A signal processing apparatus employing a waveform generated by the method of any one of claims 19 to 21.
535 23. A signal processing method employing a waveform generated by the method of any one of claims 19 to 21.
540 24. A signal processing method employing a waveform having a waveform repetition interval and bandwidth related such that the product of the waveform repetition interval and the bandwidth is an integer.
15. A signal processing method as claimed in claim 24 in which the waveform comprises t> 545 a plurality of identical sweeps, each sweep having a waveform repetition interval and bandwidth such that the product of the waveform repetition interval and the bandwidth is an integer.
t 26. A signal processing method as claimed in claim 25 in which the waveform comprises a zn series of dwells each comprising a plurality of identical sweeps.
1 550 17. A signal processing method as claimed in claim 26 in which a window function is 2 C1 Z_ 28 applied at the start and finish of each dwell.
A signal processing method as claimed in claim 27 in which the window function is a Tukey window function.
R A signal processing method as claimed in any one of claims 24 to 28 preceding claim in C, which the frequency spectrum of the waveform is weighted.
560 30. A signal processing method as claimed in claim 29 in which the waveform frequency spectrum is weighted by applying a window function to it.
31.
A signal processing method as claimed in claim 30 in which the frequency spectrum is weighted by a Tukey window function.
565 32.
A signal processing method employing a window function as claimed in any one of claims 9 to 13.
570 33.A signal processing method as claimed in claim 30 in which the waveform frequency spectrum is weighted by a window function as claimed in any one of claims 9, 10 or 12.
34.
A signal processing method as claimed in claim 30 in which the waveform frequency 4- spectrum is weighted by a window function as claimed in claim 11 or claim 13.
575 35.
A signal processing method as claimed in claim 34 which employs a waveform -)q spectrally weighted by the application of a window function in which the value of the 1 index n is selected to minimise the peak to mean ratio of the waveform.
580 36. A signal processing method as claimed in claim 35 in which the value of the index n is selected to make the first and second Fresnel peaks have equal magnitude.
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AU25321/95A AU2532195A (en) | 1994-05-20 | 1995-05-22 | Signal processing apparatus and method |
PCT/GB1995/001163 WO1995032437A1 (en) | 1994-05-20 | 1995-05-22 | Signal processing apparatus and method |
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GB9410164A GB2290188A (en) | 1994-05-20 | 1994-05-20 | Radar range processing |
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GB9410164A Withdrawn GB2290188A (en) | 1994-05-20 | 1994-05-20 | Radar range processing |
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AU (1) | AU2531095A (en) |
GB (2) | GB2290188A (en) |
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WO2006130051A1 (en) * | 2005-05-31 | 2006-12-07 | Telefonaktiebolagt Lm Ericsson (Publ) | A stepped frequency radar device |
DE102014202864A1 (en) * | 2014-02-17 | 2015-08-20 | Robert Bosch Gmbh | Device for echo-based environment sensors |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3813599A (en) * | 1973-06-04 | 1974-05-28 | Us Navy | Bandwidth measurement system |
US4201986A (en) * | 1977-11-08 | 1980-05-06 | Thomson-Csf | Continuous wave radar equipment |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3680105A (en) * | 1970-10-05 | 1972-07-25 | Raytheon Co | Pulse compression radar system |
US4532603A (en) * | 1983-03-09 | 1985-07-30 | The United States Of America As Represented By The Secretary Of The Army | Chirp transform correlator |
-
1994
- 1994-05-20 GB GB9410164A patent/GB2290188A/en not_active Withdrawn
- 1994-10-24 GB GB9421466A patent/GB2291301A/en not_active Withdrawn
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1995
- 1995-05-22 AU AU25310/95A patent/AU2531095A/en not_active Abandoned
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3813599A (en) * | 1973-06-04 | 1974-05-28 | Us Navy | Bandwidth measurement system |
US4201986A (en) * | 1977-11-08 | 1980-05-06 | Thomson-Csf | Continuous wave radar equipment |
Also Published As
Publication number | Publication date |
---|---|
AU2531095A (en) | 1995-12-18 |
GB2290188A (en) | 1995-12-13 |
GB9421466D0 (en) | 1994-12-07 |
GB9410164D0 (en) | 1994-11-30 |
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