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Signal Processing by Digital Generalized Detector in Complex Radar Systems

33

Equation 2.34 is analogous to the convolution integral describing a process at the linear system output with impulse response h(t) if the stochastic process x(s) comes in at the linear system input:

Z(t) = h(t s)x(s)ds.

(2.35)

−∞

 

This analogy allows us to use the linear filter to calculate the correlation integral, the impulse response of which is matched with the expected signal s(t). Matching is reduced to choice of a corresponding linear filter impulse response satisfying the following condition:

T (t0 + α) = Z(α).

(2.36)

For the considered case of detection problem the impulse response of the matched linear filter must be mirrored with respect to the expected signal

h(t) = as(t0 t),

(2.37)

where

t0 is the delay of signal peak at the matched filter output, which in the case of the pulse signal must be t0 ≥ τ0

a is the fixed scale factor

If the process x(t) = s(t, α) + w(t) comes in at the matched filter input, then according to (2.36) the process forming at the matched filter output at the instant t0 = τ0 is defined in line with the following formula:

Z(t) = a

x(u)s 0 t + u)du.

(2.38)

 

t − τ0

 

 

In particular, when w(t) = 0, we obtain

 

 

Z(t) = a

s(u)s 0 t + u) du = aRss 0 t),

(2.39)

t − τ0

 

 

 

where Rss 0 t) is the autocorrelation function of expected signal s(t, α).

As it follows from (2.38) and (2.39), the signal at the matched filter output coincides with the mutual correlation function of the signal model and expected signal accurate within the fixed factor. When the white noise is absent, that is, w(t) = 0, the output signal coincides with the same accuracy with the autocorrelation function Rss 0 t) of expected signal s(t, α) at the time instant (τ0 t).

Signal-to-noise ratio (SNR) by energy at the matched filter output is given by

 

SNR =

2Es ,

(2.40)

 

0

 

where 0.5 0 is the two-sided power spectral density of white noise. The Neyman–Pearson detector brings us the analogous results [12]. Thus, the matched filter allows us to obtain the maximal SNR at the output within the limits of classical signal detection theory. Realization of analog matched

34

Signal Processing in Radar Systems

filters in practice is very difficult, especially in the case of wideband signals. Moreover, it is impossible to carry out a parameter tuning for analog matched filters. For this reason, digital matched filters are widely used.

2.2.2  Generalized Detector

Recall the main functioning principles of the generalized detector (GD) constructed based on the generalized approach to signal processing in noise [13–17]. The GD is a composition of the linear systems, Neyman–Pearson receiver, and energy detector. A flowchart of a GD explaining the main functioning principles is shown in Figure 2.5. Here, we use the following notations: the model signal generator or local oscillator (MSG), the preliminary linear system or filter (PF), and the additional linear system of filter (AF).

Consider briefly the main statements regarding AF and PF. There are two linear systems at the GD front end that can be presented, for example, as bandpass filters, namely, the PF with the impulse response hPF(τ) and the AF with the impulse response hAF(τ). For simplicity of analysis, we consider that these filters have the same values for amplitude–frequency responses and bandwidths. Moreover, a resonant frequency of the AF is detuned relative to a resonant frequency of the PF on such a value that the incoming signal cannot pass through the AF. Thus, the received signal and noise can appear at the PF output and the only noise appears at the AF output (see Figure 2.5).

It is a well-known fact that if a value of detuning between the AF and PF resonant frequencies is more than 4 ÷ 5 fs, where fs is the signal bandwidth, the processes forming at the AF and PF outputs can be considered as independent and uncorrelated processes. In practice, the coefficient of

 

 

yi[n] =

wi[n]

 

H0

 

 

αilsi[n] + wi[n]

H1

 

 

 

ξAFi[n]

 

 

AF

 

 

 

 

 

 

 

 

 

ξPFi[n]

H0

 

 

 

Input

xi[n] =

 

 

 

 

 

 

 

 

 

αilsi[n] + ξPFi[n]

H1

 

 

 

 

 

 

PF

 

 

×

 

 

 

 

 

 

 

 

 

 

 

 

 

MSG

 

 

 

 

×

+

 

++

 

 

 

+

 

 

 

 

×

+

 

 

 

Σ

 

×

+

 

 

Output

 

 

 

 

 

 

 

 

 

 

 

 

ΣN [ξ AF2

i[n] – ξ PF2 i[n]]

H0

 

 

 

 

i=1

 

 

 

 

 

 

ΣN [αil2 si2[n]+ [ξ AF2 i[n] – ξ PF2 i[n]]

H1

 

 

i=1

 

 

 

 

FIGURE 2.5  Generalized detector.

Signal Processing by Digital Generalized Detector in Complex Radar Systems

35

correlation is not more than 0.05. In the case of signal absence in the input process, the statistical parameters at the AF and PF outputs will be the same under the condition that these filters have the same amplitude–frequency responses and bandwidths by value, because the same noise is coming in at the AF and PF inputs. We may think that the AF and the PF do not change the statistical parameters of input process, since they are the linear front-end systems of a GD. For this reason, the AF can be considered as a generator of reference sample with a priori information a “no” signal is obtained in the additional reference noise forming at the AF output.

There is a need to make some comments regarding the noise forming at the PF and AF outputs. If the white Gaussian noise with zero mean and finite variance σ2n comes in at the AF and PF inputs, the linear front-end system of the GD, the noise forming at the AF and PF outputs is Gaussian, too, because AF and PF are the linear systems and, in general, the noise takes the following form:

 

ξPF (t) = hPF (τ)w(t − τ)dτ and

ξAF (t) = hAF (τ)w(t − τ)dτ,

(2.41)

 

−∞

−∞

 

where ξPF(t) and ξAF(t) are the narrowband Gaussian noise. If, for example, the additive white Gaussian noise with zero mean and two-sided power spectral density 0.5 0 is coming in at the AF and PF inputs, then the noise forming at the AF and PF outputs is Gaussian with zero mean and variance given by [14, pp. 264–269]

σ2n =

0 ω02

,

8 F

 

 

where if the AF or the PF is the RLC oscillator circuit, then the AF or the PF bandwidth resonance frequency ω0 are defined in the following manner:

F = πβ, ω0 =

1

, where β =

R

.

LC

 

 

 

2L

(2.42)

F and

(2.43)

The main functioning condition of a GD is the equality over the whole range of parameters between the expected signal s(t, α) and the model signal forming at the MSG or local oscillator output s*(t τ0, a). How we can satisfy this condition in practice is discussed in detail in Refs. [14, pp. 669–695,17]. More detailed discussion about choosing between the PF and the AF and their amplitude–frequency responses is given also in Refs. [15,16].

According to Figure 2.5 and the main functioning principle of a GD, the process forming at the GD output takes the following form:

ZGDout (t) = aRss 0 t) + ξ2AF (t) − ξ2PF (t).

(2.44)

From (2.44) we see that the signal at the GD output coincides with the mutual correlation function of the signal model and expected signal accurate within the fixed factor. In a statistical sense, the background noise ξ2AF (t) − ξ2PF (t) forming at the GD output tends to approach zero when the number of samples or the time interval of observation tends to approach infinity [15,17]. SNR by energy at the GD output is given by [14]

SNR =

Es

=

Es

,

(2.45)

 

 

 

n4

 

2n

 

where σ2n is defined by (2.42).

36

Signal Processing in Radar Systems

2.2.3  Digital Generalized Detector

Now consider briefly the main principles of designing and construction of the digital GD (DGD). The DGD flowchart is represented in Figure 2.6. We see that processes at the outputs of MSG, PF, and AF are sampled and quantized, which is equivalent to passing these processes through digital filters. The model signal forming at the MSG output after sampling and quantization can be presented in the following form:

s (lTs ) = aTss [(n0 l)Ts ],

(2.46)

where n0 = τ0/Ts is the number of discrete elements of the model signal. For simplicity, we can assume that a = Ts−1. Then

s (lTs ) = s [(n0 l)Ts ],

(2.47)

where l = (0, 1,…, n0 − 1).

If the main functioning condition of GD, that is, an equality over the whole range of parameters between the expected signal s(t, α) and the model signal forming at the MSG output s*(τ0 t + u) is satisfied, the process at the DGD output, when the additive mixture of the signal s(t) and stationary white Gaussian noise w(t) comes in at the input, can be represented in the following form [18–21]:

 

n0 −1

n0

−1

 

ZDGDout

(kTs ) = 2C(l)x[(k l)Ts ]s [(n0 l)Ts ] − C(l)x2[(k l)Ts ]

 

l= 0

l= 0

 

 

n0

−1

 

 

 

 

+ C(l2AF[(k l)Ts ],

 

 

(2.48)

 

l= 0

 

 

 

 

 

Sampling

 

 

 

 

 

and

AF

 

 

 

 

quantization

 

 

Input

 

 

 

 

 

 

 

Sampling

 

 

 

 

 

and

PF

 

 

 

×

quantization

 

 

 

 

Sampling

 

 

 

 

 

 

 

 

 

 

and

MSG

 

 

 

×

quantization

 

 

++

 

+

 

 

 

+

 

 

 

 

×

++

 

Integrator

 

 

 

 

 

×

Output

 

 

 

 

 

 

FIGURE 2.6  Digital generalized detector.

Signal Processing by Digital Generalized Detector in Complex Radar Systems

37

where

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

;

 

 

 

 

 

 

 

 

 

 

 

 

x[(k l)Ts ] = x(t)

 

t = τ0 ; s [(n0 l)Ts ] = s (t)

 

t = τ0 ; s[(n0 l)Ts ] = s(t)

 

t = τ0

 

 

 

 

 

ξPF[(k l)Ts ] = ξPF (t)

 

 

ξAF[(k l)Ts ] = ξAF (t)

 

 

 

 

(2.49)

 

 

;

 

 

 

 

 

 

 

 

t = τ0

 

 

 

 

t = τ0

 

 

 

 

 

 

 

 

 

 

and

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

C(l) = TsC0 (l)

(2.50)

are the coefficients determined by numerical integration using the technique of rectangles (any technique may be used):

C0(l) = 1,1,…,1, 0.

(2.51)

If in (2.48) we replace n0 l by i in the first term, after elementary mathematical transformations of the first term with the second term we obtain

Rss (kTs ) = s (iTs )s[(k − (n0 i))Ts ].

(2.52)

i

 

Equation 2.52 represents, by analogy with (2.39), the autocorrelation function of the expected signal s(t, α). The autocorrelation function (2.52) of the signal at the DGD output is a periodic function by frequency. At low values of fs, cross-sections of the autocorrelation function (2.52) may overlap, which leads to distortions of the process forming at the DGD output. However, if fs were chosen in agreement with the sampling theorem, these distortions would be negligible.

As it follows from (2.52), when the expected signal s(iTs) comes in at the DGD input, the signal at the DGD output is matched with the autocorrelation function (2.52) accurate within the cofactor aTs. Since the autocorrelation function (2.52) is symmetric with respect to its maximum Rss (0), the data samples of the sequence {ZGDout (kTs )} at the DGD output will at first increase and after reaching the upper limit at kTs = n0Ts, that is, the maximal value of the autocorrelation function (2.52), decrease to zero within the limits of the time interval between n0Ts and 2n0Ts. The envelope of the data samples of the sequence {ZGDout (kTs )} at the DGD output coincides with an envelope of the autocorrelation function Rss (kTs ) given by (2.52). This peculiarity of data samples of the sequence {ZGDout (kTs )} at the DGD output agrees with that of analog GD.

The limiting value of the DGD output signal energy is equal to the energy of expected signal sequence s(kTs) and is reached at the finite signal bandwidth and Ts (2 fs)−1, where fs is the signal bandwidth. If the signal spectrum is infinite and we must take into account some effective signal bandwidth fseff under sampling, there are energy losses owing to superposition of unaccounted power spectral density tails under their mutual shift on k/Ts. These energy losses may be

taken into consideration introducing an additional noise within the power spectral density 0.5 ′ .

0

The receiver noise of DGD is the stationary random sequence with the power spectral density

0.5 ″ uniform within the limits of the bandwidth −(2T )−1 f < (2T )−1 and depends on T .

0 s s s

It is well known that the sampling and quantization techniques are used to digitize analog signals. For example, the sampling technique is used to discretize a signal within the limits of the time interval, and the quantization technique is used to discretize a signal by amplitude within the limits of the sampling interval. For this reason, there is a need to distinguish between the errors caused by these two digitizing techniques, which allows us to obtain a high accuracy of receiver performance.

38

Signal Processing in Radar Systems

Amplitude quantization and sampling can be considered as additional noises ζ1(kTs) and ζ2(kTs) with zero mean and finite variances σζ21 and σ2ζ 2, respectively. If the relationship between the chosen amplitude quantization step x and the mean square deviation σ′ of process at sampling, and quantization block output is determined by x < σ ′, then the absolute value of mutual correlation function between the amplitude quantization error and the signal is approximately 10−9 with respect to the values of the autocorrelation function of the signal. Therefore, it is reasonable to neglect this mutual correlation function. As a first approximation, it is reasonable to assume that the noises ζ1(kTs) and ζ2(kTs) are Gaussian.

We may suggest that the additive component ζΣ(kTs) can be presented in the form of summary uncorrelated interferences: the interference caused by quantization ζ1(kTs), normal Gaussian with zero mean and the finite variance σζ21, and the interference caused by sampling ζ2(kTs), normal Gaussian with zero mean, and the finite variance σ2ζ2 . Thus, the summary additive interference ζΣ(kTs) can be presented in the following form:

ζΣ (kTs ) = ζ1(kTs ) + ζ2 (kTs )

(2.53)

and is the normal Gaussian with zero mean and the finite variance given by

σζ2Σ = σζ21 + σζ22

(2.54)

This is a direct consequence of Bussgang’s theorem [22].

Taking into consideration the aforementioned statements, the total background noise at the DGD output is defined by the receiver noise and interferences caused by quantization and sampling:

the total background noise = ξ2AF

(kTs ) − ξ2PF

(kTs ),

(2.55)

Σ

 

Σ

 

where

 

 

 

ξPFΣ (kTs ) = ξPF (kTs ) + ζΣ (kTs ) = ξPF (kTs ) + ζ1(kTs ) + ζ2 (kTs )

(2.56)

is the noise forming at the PF output of DGD input linear system consisting of the normal Gaussian noise ξPF(kTs) with zero mean and the variance σ2n ; the interference ζ1(kTs) with zero mean and the variance σζ21 , which is caused by quantization; and the interference ζ2(kTs) with

zero mean and the variance σζ22, which is caused by sampling. Noise ξPF(kTs) and interferences ζ1(kTs) and ζ2(kTs) do not correlate with each other.

ξAFΣ (kTs ) = ξAF (kTs ) + ζΣ (kTs ) = ξAF (kTs ) + ζ1(kTs ) + ζ2 (kTs )

(2.57)

is the noise forming at the AF output of DGD input linear system (additional or reference noise) [14,17–21], consisting of the normal Gaussian noise ξAF(kTs) with zero mean and the variance σ2n; the ­interference ζ1(kTs) with zero mean and the variance σ2ζ1, which is caused by quantization; and the

interference ζ2(kTs) with zero mean and the variance σζ22, which is caused by sampling. The noise ξAF(kTs) and the interferences ζ1(kTs) and ζ2(kTs) do not correlate to each other.

The probability density function of the total background noise forming at the DGD output is symmetric with respect to zero because the means of noises ξPF(kTs) and ξAF(kTs) and interferences ζ1(kTs) and ζ2(kTs) are equal to zero owing to the initial conditions. The probability density function of the total background noise forming at the DGD output is discussed in detail in Refs. [14, pp. 250–263,15].

Signal Processing by Digital Generalized Detector in Complex Radar Systems

39

Because the noise ξPF(kTs) and ξAF(kTs) and the interferences ζ1(kTs) and ζ2(kTs) do not correlate with each other, the variance of the total background noise and the interferences forming at the DGD output can be determined in the following form [18–21]:

σξ22AFΣ − ξ2PFΣ = 4σn4 + 4σζ4Σ .

(2.58)

SNR by energy at the DGD output is given by the following [14, pp. 504–508, 18–21]:

SNR =

Es

=

Es

=

 

Es

,

(2.59)

σξ22AF

− ξ2PF

n4 + 4σζ4Σ

2

σ4n + σζ4Σ

 

Σ

Σ

 

 

 

 

 

 

 

where σ2n is defined by (2.42) and σζ2Σ is given by (2.54).

Thus, the losses caused by the sampling period Ts are possible in digital signal processing subsystems employed by complex radar systems.

2.3  CONVOLUTION IN TIME DOMAIN

Target return signals employed by CRSs typically have a narrowband. It is for this reason the DGD must use two channels for signal processing: in-phase and quadrature channels. The narrowband target return signals coming in at the input of DGD linear systems can be presented by the in-phase xI[k] and quadrature xQ[k] constituents at discrete sampling instants kTs. In this case, the complex envelope of the input signal can be presented in the following form:

 

(2.60)

X[k] = xI[k] jxQ[k].

By analogy with (2.60), the complex envelope at the output of the MSG can be presented in the following form:

 

 

 

 

[k].

(2.61)

S

[k] = SI

[k] + jSQ

The process at the DGD output accurate within the factor 0.5Ts can be determined in the following form [19]:

out

 

 

 

2

2

(2.62)

ZDGD[k] = 2X[k]S

[k] − X

[k]+ ξAF[k],

where ξAF[k] is the noise forming at the AF output (the input linear filter of DGD). We can discard the third term in (2.62) and will consider it in the end result. Based on (2.61) and (2.62), the process at the DGD output can be written as follows:

 

 

{

 

 

}

{xI[k] − jxQ[k]}2

ZDGDout

[k] = 2

 

xI[k]

jxQ[k] SI [k] + jSQ[k]

 

n0

1

{ xI[k l] − jxQ[k l]][SI [n0 l] + jSQ[n0 l] }{xI[k l] − jxQ[k l]}2 }.

 

= {2

l = 0

(2.63a)

40 Signal Processing in Radar Systems

Replacing n0 l by i in (2.63a), we obtain

n0 1

{{xI[k (n0 i)] jxQ[k (n0 i)]}{SI [i] + jSQ[i]}}

 

ZDGDout [k] = {2

 

l = 0

 

 

{xI[k (n0 i)] jxQ[k (n0 i)]}2 }.

(2.63b)

According to the analysis carried out in [15, pp. 269–282] and following the main functioning DGD condition, that is, in the considered case

SI (i) = SI[k (n0 i)] and SQ (i) = SQ[k (n0 i)],

(2.64)

the in-phase and quadrature constituents of the process at the DGD output can be presented in the following form:

 

ZDGDout

I = ZDGDout

II + ZDGDoutQQ = SI (i)SI[k (n0 i)] − ξ2I [k (n0 i)]

 

 

 

 

+ SQ (i)SQ[k (n0 i)] + ξQ2 [k (n0 i)],

(2.65)

ZDGDout

Q = ZDGDout

IQ + ZDGDout

QI = − 4SI (i)SQ[k (n0 i)] 4SI (i)ξQ[k (n0 i)]

 

 

 

 

 

 

+ 4SQ (i)SI[k (n0 i)] + 4SQ (i)ξI[k (n0 i)]

 

 

 

 

 

 

+ 2ξQ[k (n0 i)]ξI[k (n0 i)],

(2.66)

where the factor 2 in the second line is caused by the presence of amplifier (see Ref. [15, pp. 269– 282]). Moreover, the corresponding terms in the first and second lines of (2.66) are compensated in the statistical sense. As a result, the quadrature constituent of the process at the DGD output is caused by the autocorrelation function of the in-phase and quadrature constituents of the narrowband noise. Thus, we can write

R out

(τ) = σ22

2

F sinc( Fτ),

(2.67)

ZDGDQ

ξAFΣ − ξPFΣ

 

 

where the variance of the total background noise at the DGD output σ22

2 is given by (2.58);

ξAFΣ − ξPFΣ

the DGD input linear system (PF and/or AF) bandwidth is defined by (2.43); and sinc(x) is the sinc function [1].

Further specification of digital signal processing algorithms is defined by type of convolved sig-

nals. For example, in the case of chirp modulation of the signal with rectangular envelope

 

S(t) = sin 2πfct + γt2

 

,

(2.68)

 

 

 

 

where 0 < t ≤ τ0 and γ = πΔF0/τ0 = const; F0 is the target return signal frequency deviation. The complex envelope can be presented in the following form:

 

2

j cos γt

2

.

(2.69)

S(t) = sin γt

 

 

Signal Processing by Digital Generalized Detector in Complex Radar Systems

41

Consequently, the in-phase and quadrature constituents of the target return signal at discrete instants [k − (n0 i)]Ts can be presented in the following form:

xI[k (n0 i)] = sin γ [k (n0 i)]2 + ξI[k];

 

(2.70)

 

xQ[k (n0

i)] = cosγ [k (n0 i)]2 + ξQ[k],

where ξI[k] and ξQ[k] are the constituents of the narrowband noise forming at the PF (the DGD input linear system) output.

In this case, the complex envelope of the model signal forming at the MSG output takes the following form:

 

 

t)

2

] + j cos[γ (τ0 t)

2

],

(2.71)

S

(τ0 t) = sin[γ (τ0

 

 

and the in-phase and quadrature constituents at discrete instants iTs are given by

 

 

SI [i] = sin γ[i]2

and

 

SQ [i] = cos γ[i]2.

 

 

(2.72)

The flowchart of the generalized signal processing algorithm given by (2.62) is shown in Figure 2.7. There are eight convolving blocks and six summators to calculate all in-phase and quadrature constituents of the process forming at the DGD output. Each in-phase and quadrature components can be presented in the following form taking into account (2.68) through (2.72):

 

 

 

 

 

n0

 

 

 

 

 

 

n0

 

 

 

 

 

 

 

 

 

 

 

 

ZDGDout

II = 2sin γ[i]2 xI[k (n0 i)] = 2sin γ[i]2 sin γ[k (n0 i)]2

 

 

 

 

 

i=1

 

 

 

 

 

 

i=1

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

n0

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

+ 2sinγ [i]2 ξI[k (n0 i)]2;

 

 

 

 

 

 

 

 

 

 

 

(2.73)

 

 

 

 

 

 

i=1

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

xI

 

 

 

 

 

 

 

 

 

II

 

 

 

 

 

 

 

 

+

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

I

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

QI

 

 

 

 

 

 

Σ

 

 

 

>

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

MSG I

 

 

 

 

 

 

 

 

 

 

 

 

+

 

 

+

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Q

 

 

 

 

 

 

 

IQ

Σ

 

 

 

 

 

>

 

 

 

 

+

out

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

xQ

 

Q

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

+

 

Σ

ZGDI

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

QQ

 

 

 

 

 

 

 

 

 

 

 

 

Σ

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

out

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

+

 

 

 

 

 

 

 

 

 

 

 

ZGDQ

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

II

 

 

 

Σ

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

QI

Σ

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

IQ

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

QQ

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

FIGURE 2.7  Convolution in time using the digital generalized detector.

42

out

ZDGDII

 

 

 

 

Signal Processing in Radar Systems

 

 

 

n0

n0

ZDGDout

QQ

= 2cos γ[i]2 xQ[k − (n0 i)] = 2cos γ[i]2 cos γ[k − (n0 i)]2

 

 

 

i=1

i=1

 

 

 

n0

 

 

 

 

+ 2cos γ[i]2 ξQ[k − (n0 i)]2;

(2.74)

 

 

 

i=1

 

 

 

 

n0

n0

ZDGDout

QI

= 2cos γ[i]2 xI[k (n0 i)] = 2cos γ[i]2 sin γ[k (n0 i)]2

 

 

 

i=1

i=1

 

 

 

n0

 

 

 

 

+ 2cos γ[i]2 ξI[k (n0 i)]2;

(2.75)

 

 

 

i=1

 

 

 

 

n0

n0

ZDGDout

IQ

= 2sin γ[i]2 xQ[k (n0 i)] = 2sin γ[i]2 cos γ[k (n0 i)]2

 

 

 

i=1

i=1

 

 

 

n0

 

 

 

 

+ 2sin γ[i]2 ξQ[k (n0 i)]2;

(2.76)

i=1

=xI[k (n0 i)]xI[k (n0 i)]

i=1n0

n0

 

n0

= {sin γ[k (n0 i)]2 + ξI[k (n0 i)]}× {sin γ[k (n0 i)]2 + ξI[k (n0 i)]}

i=1

 

i=1

n0

n0

n0

= sin2 γ[k (n0 i)]2 + 2sin γ[k (n0 i)]2 ξI[k (n0 i)]+ ξ2I [k (n0 i)];

i=1

i=1

i=1

(2.77)

out

n0

 

 

= xQ[k − (n0

i)]xQ[k − (n0 i)]

 

ZDGDQQ

 

 

i=1

 

 

 

n0

 

n0

 

= {cos γ[k − (n0 i)]2 + ξQ[k − (n0 i)]}× {cos γ[k − (n0 i)]2 + ξQ[k − (n0 i)]}

 

i=1

 

i=1

 

n0

n0

n0

 

= cos2 γ[k − (n0 i)]2 + 2cos γ[k − (n0 i)]2 ξQ[k − (n0 i)]+ ξQ2 [k − (n0 i)];

 

i=1

i=1

i=1

(2.78)

Соседние файлы в папке Diss