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Synthesis of Antenna Systems According to the Desired Amplitude Radiation Characteristics

Written By

Mykhaylo Andriychuk

Submitted: 18 November 2011 Published: 19 September 2012

DOI: 10.5772/46164

From the Edited Volume

Numerical Simulation - From Theory to Industry

Edited by Mykhaylo Andriychuk

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1. Introduction

The problems of antenna synthesis, which use the amplitude RP as input information, are often used in the process of antenna design for many practical applications [4, 16, 27, 31]. In spite of the fact that the respective mathematical problems are ill-posed [32] and they have the branching solutions [29], the antenna synthesis according to the desired amplitude characteristics is very useful and perspective.

As a rule, the branching of solutions depends on the properties of prescribed amplitude RP, geometrical and physical parameters of the considered antenna. The methods of nonlinear functional analysis [23] allowing to localize the branching solutions are applied for investigation of solutions and determination of their number and qualitative characteristics. Such approach too much simplifies determination of the optimal solutions by the numerical methods. The iterative processes for the numerical solving of the corresponding non-linear equations were elaborated in [3, 8, 11].

The Chapter is organized as follows.

In Section 2 we derive the main formulas for RP of antennas and introduce the objective functionals for the synthesis problem. Also in Section 2 we consider the variational statement of problems and derive the fundamental nonlinear equations of the synthesis.

Section 3 contains the application of the proposed approach to several types of antennas. Depending on the restrictions which are imposed on the sought distribution of current or field in the antenna elements and type of antenna, the problems of amplitude-phase, amplitude, and phase synthesis are considered for the specific antennas. The methods of successive approximations are applied for solving the derived non-linear integral equations; the convergence of the elaborated methods is discussed. The direct optimization of the proposed functionals by the gradient methods is performed and successfully applied to solving the amplitude and phase synthesis problems.

In Section 4 conclusions are formulated.

2. The theoretical background of the synthesis problems

In this Section, we present the necessary information about the properties of the electromagnetic (EM) field in far zone, introduce the variational approach to the antenna synthesis problems, as well as discuss the arising nonlinear integral and matrix equations.

2.1. RP of electromagnetic field

The EM field in the non-limited homogeneous medium satisfies the Maxwell equations [25]

rotH=ikϓE+4ϞcI,E1
rotE=-ikϚH,E2
divE=ϟ/ϓ,E3
divH=0,E4

where E is a component of electric field, H is a component of magnetic field, I is the extrinsic current density, ϟ is the volume density of electric charge.

The scalar and vector potentials are used for solving the equations (1)-(4). Introducing the vector potential Ae as [34]

H=rotAe,E5

we satisfy the equation (4). Substituting (5) into (2), we receive the equation

rot(E+iϧϚAe)=0,E6

which testifies that the vector field in the parenthesis of (6) is potential. This yields the equation

where Ϥe is the scalar potential. Substituting (5) and (7) into (1), we receive the following equation for I:

Using Lorentz lemma [15]

divAe+iϧϓϤe=0,E9

we receive the inhomogeneous Helmholtz equation for the vector potential

2Ae+k2Ae=-I,E10

where k=ϧϓϚ is a propagation coefficient. For a free space, the values ϓ and Ϛ are real and related with the light velocity as c=1/ϓϚ, and coefficient k=ϧ/c=2Ϟ/ϙ is the wavenumber, ϙ is the length of wave.

The vector potential Ae in the arbitrary observation point Q(x,y,z) is determined by formula [26]

Ae(x,y,z)=14ϞVI(x',y',z')-eikRPQRPQdV,E11

where RPQ=(x-x')2+(y-y')2+(z-z')2 is the distance between the observation point Q(x,y,z) and integration point P(x',y',z'), I(x',y'z') is the density of current in the domain V.

Using formulas (5), (7), and (11), we receive the solution to system (1)-(4) in the term of electric vector potential

H=rotAe.E13

In the process of solving the synthesis problem, the representation of field in far zone is of interest. Using the approximate representation of distance RPQ in far zone, we receive the formula for vector potential in this region

Ae(Q)=-eikr4ϞrVI(x',y',z')eikr'cosϏdV+O(1r2),E14

where Ϗ is the angle between the vectors, directed into observation and integration point, r' and r are the radius-vector of the points P and Q, respectively.

Substituting (14) into (13) and neglecting by terms of O(1r2) order, we receive the formulas for components of magnetic field H in term of vector potential Ae. These formulas in the spherical coordinates have form

Hr=0, Hϖ=ikAϤe, HϤ=-ikAϖe.E15

Consequently, the formulas for E are the following

Er=0, Eϖ=-iϧϚAϖe, EϤ=-iϧϚAϤe.E16

Using formulas (15), (16) and relation

E=-1ϧϓrotH,E17

we receive the formulas for non-zero E components of EM field

Eϖ(r,ϖ,Ϥ)=-iϧϚe-ikr4Ϟrfϖ(ϖ,Ϥ),E18
EϤ(r,ϖ,Ϥ)=-iϧϚe-ikr4ϞrfϤ(ϖ,Ϥ).E19

Function e-ikr4Ϟr is a spherical wave and it depends on r only. The second terms in (18) and (19) are the functions of angular coordinates of the observation point and are determined by the current I(x',y',z')

fθ(θ,φ)=V[Ix(x',y',z')cosθcosφ+Iy(x',y',z')cosθsinφIz(x',y',z')sinθ]eik(x'sinθcosφ+y'sinθsinφ+z'cosθ)dV,E20
fφ(θ,φ)=V[Iy(x',y',z')cosφIx(x',y',z')sinφ]×eik(x'sinθcosφ+y'sinθsinφ+z'cosθ)dV.E21

The functions (20) and (21) characterize the angular distribution of E components in far zone.

In such a way, the vectors E and H in far zone are expressed by formulas [Andriychuk et al., 1993]

E(r,ϖ,Ϥ)=-iϧϚe-ikr4Ϟr{ 0,fϖϖ,Ϥ,fϤϖ,Ϥ},E22
H(r,ϖ,Ϥ)=ike-ikr4Ϟr{0,fϤϖ,Ϥ,-fϖϖ,Ϥ}.E23

The functions fϖ(ϖ,Ϥ) and fϤ(ϖ,Ϥ) are defined as the RPs. Function

N(ϖ,Ϥ)=|fϖϖ,Ϥ|2+|fϖϖ,Ϥ|2E24

is the power RP and it characterizes the angular distribution of power intensity radiation. The functions fϖϖ,Ϥ, fϤϖ,Ϥ, and N(ϖ,Ϥ) are used in the process of formulating and solving the synthesis problems for various antennas.

2.2.Variational. statement of the synthesis problems

Abstracting of the specific type of antenna, we present the functions fϖ and fϤ in the formulas (22)-(24) by the linear operator A={Aϖ,AϤ}:

f=AI, (fϛ=AϛI, ϛ=ϖ,Ϥ),E25

acting from some complex Hilbertian space HI, to which the distribution functions of current or field belong, into the complex space Cf2=Cχ Cχ of vector-valued continuous functions on the compact χ̣ R2 (or χ̣ R1) [29]. The form and properties of the operators Aϛ depend on a type and geometry of antenna. In many practical applications, one can reduce the synthesis problem to separate consideration of the fϖ andfϤ components. This allows to reduce the synthesis problem to the scalar one. In that way, we will use more simple formula

f=AIE26

for operator expression of the RP f.

The specific form of the operator A depends on the antenna type. This operator is integral for the continuous antennas. As an example, for a cylindrical antenna with curvilinear generatrix and with current polarized along the cylinder axis, the RP in the transversal plane has form [21]

f=AI:=SI(S)eikr(Ϥ')cos(Ϥ-Ϥ')dSϤ',E27

where fand I are nonzero components fϖ and Iz respectively; Ϥ is the angular coordinate of the point in far zone, Ϥ' is the angular coordinate of the point in antenna, r=r(Ϥ') describes the generatrix in polar coordinates, dSϤ'=r2+(dr/dϤ')2 is an element of arc. In the case of array, the operator A is described by a finite sum.

In the previous subsection, we consider the direct external problem of electrodynamics consisting of determination of the asymptotic (RP) of EM field in far zone. The inverse problem, namely determination of such a current I that create EM field with the desired RP f, is of specific interest in the antenna design. The characteristic parameters of antenna can be fixed or be subject to determination in process of solving this problem. In such interpretation, the inverse problem is defined as the synthesis problem, namely the problem of determination of the current according to the desired RP.

The RPs are due to satisfy a series of requirements for the main lobe and sidelobes. In one case, the RP with narrow main beam is required, another time, this beam should have the specific wide (for example, cosecant) form; the sidelobes be as low as possible.

The angular distribution of the radiation power is characterized by the amplitude of RP, but not the whole RP. Therefore, only amplitude |f| of function f is interesting in the process of statement and solving the synthesis problem. In this case, the freedom of choice of the phase argf of function f is used for better approximation to the amplitude RP. In the synthesis theory, function |f| is amplitude RP, and function argf is phase RP.

In this way, in the process of synthesis we prescribe not the whole complex function f, but only its amplitude. We denote this function as F, the created (synthesized) by antenna amplitude RP is denoted by |f|. The both functions are real and positive. Of course, these functions can not coincide in any real-world situation. This fact yields to use the variational statement of the synthesis problem. In such statement, one requires not the whole coincidence of the functions |f| and F, but the better approximation of function |f| to F in a certain sense only. The mean-square deviation of both RPs is used as the criterion of optimization.

Let us introduce the Hilbertian spaces of radiation patterns Hf and currents HI. Let (,)f be an inner product in Hf, and norm of f is defined as [4]

||f||2=(f,f)f.E28

The functional

ϡ=(F-s|f|,F-s|f|)fE29

is used in most cases as optimization criterion. Dependence of ϡ on the sought distribution of the current I in antenna is determined by formula (26). The additional multiplier s in (29) can be either prescribed (for example, s=1) or determined from the condition ϡ/s=0. In the latter case

s=(F,|f|)f/(f,f)f.E30

Let us introduce the normalization (F,F)f=1, then (29) can be written as

ϡ=1-QϘ2,E31

where

Q=||I||2/||f||2,E32
Ϙ=(F,|f|)f/||I||,E33
and ||I|| is the norm of current, determined by inner product (,)I in the Hilbertian space HI of currents: ||I||2=(I,I)I. The factor Q characterizes the goodness (reactivity) of antenna, and Ϙ determines its power efficiency, namely the part of power radiated by the RP.

The generalized functional, allowing to diminish the mean-square deviation of RPs and relative norm of current, has the form

ϡt=(F-|f|,F-|f|)f+t||I||2.E34

Choosing the weight multiplier t, one can regularize the value of mean-square deviation of the RPs and norm of current. Similar functional appears when the method of Lagrange multipliers [16] is used to solving the conditional extremum problems. Simultaneously, one can use some weight function p0 in the definition (28) and to improve the approximation to prescribed amplitude RP F in the appointed angular range.

2.3. The fundamental equations of synthesis

Let us demonstrate how one can receive the respective Lagrange-Euler’s equation [17] in the process of minimization of functional ϡ. Let s=1. It is known [30] that the equality to zero of functional’s gradient is requirement of its extremum. This yields determination of the maximum of the following value

ϡz=1||z||limϓ0ϡ(I+ϓz)-ϡ(I)ϓ.E35

In order to determine the derivative ϡz, one requires to factorize ϡ(I+ϓz) in series relatively to ϓ

ϡ(I+ϓz)=ϡ(I)+ϓϒϡ(I,z)+O(ϓ2)E36

and to extract the linear term ϒϡ. Evidently, ϡz=ϒϡ||z||. The increment of amplitude RP |f| should be known in order to calculate ϒϡ. This increment has the form [4]

|A(I+ϓz)|=|f|+ϓRe[A(z)e-iargf]+O(ϓ2).E37

Substituting this expression into (35), we receive

ϡz=-2(F,Re[A(z)e-iargf])f+2Re(f,Az)f,E38

or

ϡz=-2Re[(A*(f-Fe-iargf),z)I],E39

where A* is an operator adjoint to A in the following sense:

(AI1,f2)f=(I1,A*f2)I.E40
If A is an integral operator then A* is the same with the complex conjugate kernel and integration with respect to the second argument.

Using the Cauchy-Bunyakovsky-Schwarz inequality [10] and maximizing ϡz, we receive the expression for gradient of ϡ:

z=A*(f-Fe-iargf),E41

which is used usually for the numerical minimization of ϡ. In order to receive the Lagrange-Euler’s equation one should equate to zero the function z (condition of ϡ minimum)

A*(f-Fe-iargf)=0.E42

The equation (42) contains f as an unknown function. One can turn out that its solutions represent the unreliazable patterns [20]. In order to avoid such solutions, it is necessary to substitute formula (26) into (42) instead of f. In this way, we receive the integral equation for the optimal current distribution

A*AI=A*A(Fe-iargAI).E43

If operator A is integral (consequently, A* is also integral) then (43) is the nonlinear Hammerstein equation [38].

One can receive the similar expression for z in the process of Ϙ maximization:

z=A*(Fe-iargf)-I.E44

Equating the right part of (44) to zero, we receive the explicit expression for I:

I=A*(Fe-iargf).E45

Equations (26) and (45) yield the system of nonlinear integral equations for the optimal current I and RP f created by it.

System of nonlinear equations (26), (45) can be reduced to one nonlinear equation

f=AA*(Fe-iargf).E46

Since right hand side of (46) is a result of acting by the operator A on some function, any solution to this equation represents the realizable RP. Once this equation is solved, the optimal distribution of current is determined by formula (45). The equation (46) is more simple than system (26), (45) because determination of its solution does not require additional operation of A and A*.

Taking into account the above considerations, we receive the following nonlinear Hammerstein equation of the second kind for the RP f

tf+AA*f=AA*(Fe-iargf)E47

in the case of functional ϡt minimization. As in the case of (46), the solution to this equation (at t0) represents the realizable RP. Having the solution to (47), we determine the optimal current distribution by formula

I=-1/tA*(f-Fe-iargf).E48

The integral equations (43), (46), and (47) are the fundamental equations for the synthesis problems according to the prescribed amplitude RP F.

2.4. The numerical solution of the integral equations

The equations (43), (46), and (47) are solved numerically by the method of successive approximations. The new approximation is determined by explicit formula

fn+1=AA*(Fe-iargfn)E49

in the process of Ϙ maximization. The equation

A*AIn+1=A*A(Fe-iargAIn)E50

is solved when the synthesis problem is formulated in the term of functional ϡ minimization. If functional ϡt is minimized then the respective iterative procedure has form

tfn+1+AA*fn+1=AA*(Fe-iargfn).E51

In the last case, one can use the iterative process

fn+1=-1/tAA*(fn-Fe-iargfn),E52

but the convergence domain of this process is limited.

In accordance with the procedure used in Subsection 2.3, the solutions to the nonlinear equations (43), (46), and (47) are the stationary points of the respective functionals. Since the used functionals are nonconvex, the several solutions can appear, what corresponds to existence of several local minima or saddle points. The number of solutions can vary depending on the physical parameters of the problem what requires the special careful analysis of the obtained solutions [11].

3. Application to specific antennas

3.1. Amplitude-phase synthesis of cylindrical antenna

In this Subsection, we consider the application of variational approach to the synthesis problem of cylindrical curvilinear antenna. Functional (34) is used as criterion of optimization, complex function I is optimizing function. Since both the amplitude and phase of complex function I are optimizing parameters, the considered problem is the amplitude-phase synthesis problem.

3.1.1. The integral equation approach

Let the generatrix of the antenna has the length 2l and be parallel to Oz axis, and form of cross-section be determined by close curve S which be described by formula r=r(Ϥ'), where Ϥ' is the angular coordinate on S.

In many practical applications, the antennas with currents linearly polarized along Oz axis are of interest. For such case, the RP has only the component fϖ(ϖ,Ϥ), denote it as f(ϖ,Ϥ). On account of formula (18):

f(ϖ,Ϥ)=S-llI(r(Ϥ'),z)sinϖeik[r(Ϥ')sinϖcos(Ϥ-Ϥ')+zcosϖ]dSϤ'dz.E53

Let the current distribution in antenna surface be determined as

I(r,z)=I1(r(Ϥ'))I2(z),E54

then the spatial RP is completely determined by the RP f1(ϖ,Ϥ), created by the distribution of current I1(r(Ϥ')) in S, and RP f2(ϖ) in the longitudinal plane, created by the current distribution in the generatrix of cylinder

f(ϖ,Ϥ)=f1(ϖ,Ϥ)f2(ϖ).E55

Function f2(ϖ) is the RP of a linear antenna with length 2l. Function

f1(ϖ,Ϥ)=SI1r(Ϥ'),z)sinϖeik[r(Ϥ')sinϖcos(Ϥ-Ϥ')]dSϤ'E56

is the RP of a plane curvilinear antenna with form S. Consequently, one can reduce the synthesis problem of cylindrical antenna to two independent problems for synthesis of linear and plane curvilinear antennas.

There is a many literature sources on the synthesis problem of linear antennas (see, e.g. [9] and references there). Therefore we consider here the synthesis problem for plane curvilinear antenna.

It is easily seen from formula (53) that the angle ϖ determines effective electrical scale of antenna. Therefore one can suppose ϖ=Ϟ/2. Omitting the indices "1"’ in the distribution of current and RP, we represent the RP (56) in form

f(Ϥ)=AI:=02ϞI(Ϥ')eik[r(Ϥ')cos(Ϥ-Ϥ')]r2+(dr/dϤ')2dϤ',E57

that is, RP is determined due to action of linear bounded operator A.

The amplitude-phase synthesis problem for closed plane curvilinear antenna according to desired amplitude RP F consists of determination of such distribution of the current I(Ϥ'), that the amplitude RP |f(Ϥ)| created (synthesized) by it, is the most close to F(Ϥ). The functional (34) is used as the criterion of optimization. The inner products in the spaces of the RPs and currents are defined as

(f1,f2)f=02Ϟp(Ϥ)f1(Ϥ)f2*(Ϥ)dϤ,E58
(I1,I2)I=02ϞI1(Ϥ')I2*(Ϥ')r2+(dr/dϤ')2dϤ'.E59

Using (47), (57), and definitions (58) and (59), we receive the nonlinear equation with respect to RP f

tf(Ϥ)+02Ϟp(Ϥ1)K(Ϥ,Ϥ1)f(Ϥ1)dϤ1=Bf,E60

where K(Ϥ,Ϥ1) is the kernel of operator AA*

K(Ϥ,Ϥ1)=02Ϟeikr(Ϥ')[cos(Ϥ-Ϥ')-cos(Ϥ1-Ϥ')]r2+(dr/dϤ')2dϤ',E61

and nonlinear operator B is determined as

Bf=02Ϟp(Ϥ1)K(Ϥ,Ϥ1)F(Ϥ1)eiargf(Ϥ1)dϤ1.E62

The methods of successive approximations are applied for solving the nonlinear equation (60). The simplest of them

fn+1=1/t(B-AA*)fnE63

has the limited region of convergence determined by formula

t>22Ϟl(02Ϟp2(Ϥ)dϤ)1/2,E64

where l is the length of contour S. Once the function f is found, the optimal current I is determined by formula (48).

The iterative process (51) is more preferable, it yields the converging sequence of functional ϡt which satisfies the condition

ϡt(fn+1)<ϡt(fn)E65

for arbitrary t.

3.1.2. The gradient methods of optimization

Above we mentioned the methods of successive approximations for solving the arising nonlinear equations. The direct optimization of ϡt functional by the gradient methods can be also applied for solving the synthesis problem. The simplest gradient method is defined by the formula

In+1=In+ϒnzn,E66

where ϒn is an optimizing multiplier, zn is a gradient of functional ϡt (34) on the function In:

zn=A*(fn-Feiargfn)+tIn,E67
and
ϒn=||zn||/an,E68

where an is a number determined by known values in the n+1-th iteration [4].

The disadvantage of method (66) is that only the information about optimizing function from previous iteration is used, in addition it has the slow convergence at the end of iterative process. The method of conjugate gradients [28]

In+1=In+ϒnhn,E69

and proposed in [3] generalized gradient method

In+1=m=1Mϒn(m)rn(m),E70

do not have such disadvantage. Here hn is a combination of zn from previous iterations, and rn(1)=In,rn(2)=zn,rn(3)...,rn(M) is a set of some orthogonal functions, ϒn and ϒn(m) are the coefficients subject to determination.

For method (70), the problem of minimization of ϡt is reduced to the solution of nonlinear algebraic system

m=1M[t(rn(m),rn(j))I+(Arn(m),Arn(j))f]ϒn(m)=(Feiargfn+1,Arn(j))f,(j=1,...,M)E71

with unknown ϒn(m). This system is solved effectively by the method of successive approximations substituting in its right hand side the function argfn from previous iteration. Such iterative process is converging and similarly to iterative process (51) yields the converging sequence of ϡtn which satisfies the condition (65).

3.1.3. The numerical results

The numerical results are shown for the prescribed amplitude RPs F(Ϥ)=sin2(Ϥ/2) and F(Ϥ)=sin128(Ϥ/2) (Fig. 1a and Fig. 1b respectively). The influence of the parameter t in the functional (34) on the quality of synthesis is investigated. One can see that decrease of t improves the proximity of given F and synthesized |f| RPs. But the norm ||I|| of currents grows if t decreases. In the case of narrow F it is necessary to diminish t in order to decrease the mean-square deviation of the RPs. The detailed information about the synthesis quality is shown in Table 1.

 F(Ϥ)=sin2(Ϥ/2) F(Ϥ)=sin128(Ϥ/2) t ϡ Ϙ t ϡ Ϙ 0.1 0.0024 0.3419 0.01 0.0411 0.3450 1.0 0.1437 0.4367 0.10 0.0612 0.3581 10.0 1.2744 1.1065 1.0 0.0977 0.4272

Table 1.

The values of ϡ and Ϙ for two desired RPs F(Ϥ)

3.2. The problem of amplitude synthesis for resonant antennas

Resonant antennas are a new type of antennas [24], which allow to form the radiation characteristics satisfying a wide spectrum of practical requirements. Such antennas are formed by several surfaces, one of which is semitransparent. Antennas with one semitransparent and other metal boundary are considered here.

The synthesis problem consists of determination of such parameters of antenna (the geometry of inner boundary and transparency of the outer boundary), which form the amplitude RP or front-to-rear factor (FRF) the most close to the prescribed ones.

3.2.1. Generalization of variational statement

The generalized method of eigen oscillations [1] is the mathematical basis for solving the analysis (direct) problem of resonant antennas. The two-dimensional model of antennas (the case of E- polarization) is considered.

The main constructive parameter of resonant antennas is the cophased field in the outer surface. This field can be considered quite real (i.e., only its amplitude can be considered) since the constant phase shift of field does not change the amplitude RP. In this connection, the synthesis problem for resonant antennas is formulated as the amplitude synthesis problem.

The direct problem consists of determination of the RP f(Ϥ) by the known field v(S) in the outer boundary S of the given form. The RP created by this field can be presented similarly to (26). The operator A in the case of circular external boundary has form [37]

Av=02ϞK(Ϥ,Ϥ')v(Ϥ')dϤ',E72

where kernel

K(Ϥ,Ϥ')=n=0incosn(Ϥ-Ϥ')(1+ϒ0n)Hn2(ka),E73
ϒ0n is the Kronecker delta, function Hn2(ka) is the Hankel function of second kind, a is the circle radius.

In the case of resonant antenna with arbitrary outer boundary, the method of auxiliary sources [2, 12, 18] is used for determination of the RP f by the field v. In this method, the field u(r,Ϥ) outside of antenna is represented approximately by the finite sum

u(r,Ϥ)=n=1NanH02(kRn),E74

where Rn=r2+rn2-2rrncos(Ϥ-Ϥn) is the distance between an observation point and n-th auxiliary source; r,Ϥ and rn,Ϥn are the polar coordinates of a point of observation and n-th source, respectively; an are the unknown coefficients subject to determination in the process of solving the synthesis problem.

The RP is given by

f(Ϥ)=2ϞeiϞ/4n=1Naneikrncos(Ϥ-Ϥn).E75

Solving the synthesis problem, we determine the field in outer boundary S of the antenna and transparency of this boundary. The form of inner boundary S0 is determined as a curve of constant phase of the field u(r,Ϥ) [37].

Additionally, the restrictions on a field in some areas of a near zone can be prescribed. The functional

ϡt=02Ϟp(Ϥ)[F(Ϥ)-|f(Ϥ)|]2dϤ+i=1MSipi(Si)[Ui(Si)-|ui(Si)|]2dSi+t02Ϟv2(Ϥ)dϤ,E76

which is generalization of (34), allows to take into account these requirements. Here Ui(Si) are prescribed values of the field’s amplitude in the areas of restriction, ui(Si) are the obtained values of the field. Functions p(Ϥ), pi(Si) are the weight functions, allowing to adjust a degree of proximity of the given and received values of RP and field, t is the parameter limiting norm of the field v.

In the first step of solving the synthesis problem, the field v on the outer boundary S is determined from a condition of minimum of the functional (76). Minimization of functional can be carried out by the gradient methods, or by solving the respective Lagrange-Euler’s equation. In the first case, the generalized gradient method [3]

vn+1=ϒn(1)vn+ϒn(2)zn+ϒn(3)hnE77

is used. The gradient z of the functional (76) (by virtue of the requirement of real field) has form

z=tv-ReA*[Fexp(iargf)-f]-i=1MReBi*[Uiexp(iargui)-ui],E78

where A* and Bi* are the operators adjoined to A and Bi, respectively [4]. Each step of iterative process (77) reduces ϡt. Since ϡt is limited from below (ϡt0), the process (77) is converging.

In the second step, the transparency ϟ of the outer boundary S and the form of inner metal boundary S0 are determined.

For the antenna with circular outer boundary, the transparency distribution can be presented in the explicit form

ϟ(Ϥ)=Ϟkv(Ϥ)/(2n=0NancosnϤJn2(ka)+Nn2(ka)),E79

where Jn and Nn are the Bessel and Neumann functions, respectively.

In the case of antenna with arbitrary outer boundary, similarly to [37], the distribution of transparency is determined by the formula

ϟ(Ϥ)=1/[Ϧ(S(Ϥ))N].E80

3.2.2. The numerical results

The numerical calculations are carried out for the resonant antenna with a given outer elliptic boundary. The prescribed amplitude RP is: F(Ϥ)=sin8(Ϥ/2). In Fig. 2, the results are presented for the antenna with parameters kb=15 and different ka: ka=12.75,ka=14.25, where b and a are the big and small semiaxes of ellipse. For such antenna the level of side lobes in the synthesized amplitude RP |f| is smaller than –20 dB, and distribution of transparency is smoother in the area of main radiation (the continuous lines in Figs. 2a, 2b correspond to ka=12.75, and the dashed ones correspond to ka=14.25). The outer elliptic boundaries (dashed lines), the found form of inner metallic boundaries (continuous lines), and the inner contour Sa of placement of the auxiliary sources (dash-and-dot lines) are shown in Figs. 3a, 3b. The auxiliary sources are distributed uniformly on the Sa.

The distribution of transparency ϟ in the area opposite to direction of main radiation has a spasmodic character. Such distribution cannot be realized by the physical reason. Therefore the values of ϟ are averaged in this range in order to receive the smooth distribution of ϟ. This leads to some change of field v on S, but the numerical calculations show small change of the synthesized amplitude RP |f|. The more smooth distribution of ϟ in the area mentioned above can be achieved by increasing the number of auxiliary sources here.

The numerical results for solution of the synthesis problem with restrictions on the field in a near zone are given for the antenna with circular outer boundary. The prescribed amplitude RP is: F(Ϥ)=sin8(Ϥ/2); ka=15. Minimization of a field was carried out in two points Ϥ=Ϟ/2,3Ϟ/2 on the additional circle with radius kb=20. These points were allocated in the second summand of the functional (76) using the weight function p1(Ϥ)=ϒ(Ϟ/2,3Ϟ/2); p(Ϥ)1, t=0.01. In Fig. 4a, the prescribed RP F (thick continuous line) and synthesized |f| (thin continuous line) amplitude RP are shown. The amplitude |u1| of obtained field on the circle of restrictions is marked by dashed line.

It can be seen that the field at restriction points is reduced up to level -37 dB. The synthesized field v (continuous line) and transparency ϟ (dashed line) are presented in Fig. 4b. The form of the inner synthesized metallic boundary is more complicate than in the previous example.

3.3. Waveguide resonant antenna

Synthesis of resonant antenna with waveguide excitation is carried out according to the FRF. The optimizing functional enables to take into account a various requirements to the FRF of antenna in the operating frequency range, as well as outside this range.

3.3.1. The physical description of problem

The geometrical parameters of resonant antenna with waveguide excitation are shown in Fig. 5. In order to create RP enough narrow, the width L of antenna should be much larger than the wavelength ϙ. The height d is of the order of ϙ/2. Excitation is carried out by a metal single-mode waveguide with semitransparent grid at its end; the width l of waveguide is of the order ϙ/2, and both its length and the length D of the antenna along the Ox axis are of the order of L.

The RP of antenna has form

f(ϖ,Ϥ)=Su(x,y)exp[ik(xsinϖcosϤ+ysinϖsinϤ)]dxdy.E81

The direct (analysis) problem on determination of the electromagnetic field components in the semitransparent aperture is reduced to two separate problems in the planes xOz and yOz respectively. We consider here the case of E-polarization. The unknown function u is the Ey component of electromagnetic field. In the region over the antenna this component satisfies the Helmholtz equation and the boundary conditions

u=0E82

on the all metallic walls;

u+=u-, u-x-u+x=uϟ(S)E83

on the semitransparent upper boundary, the same conditions in the aperture of the exciting waveguide; the condition of radiation on the infinity

u|rx>0=exp(ikr)krf(φ),E84

and asymptotical condition in the exciting waveguide

u|xy+<a=cosπy2a(exp(iβ1x)+R1exp(iβ1x)).E85

The problem of determination of the field u(x,y) in the semitransparent boundary S is solved in three steps [37]. In the first step, the field in the irregular region of antenna is determined using the cross-section method [19]. In the second step, the field over the exciting waveguide is sought for, and the matching of field in the regular and irregular regions of antenna is fulfilled. The reflection coefficient R1 is determined by the fulfillment of the adjoint boundary conditions (85) in the third step.

Under condition of the linear polarization of field in the aperture of exciting waveguide, the RP (81) can be represented as product of two functions, namely the RP of plane antenna with variable height d(y) of the upper wall and transparency ϟ(y) of the lower wall, and RP of the linear antenna in the xOz plane.

In such a way, the RP in the yOz plane can be written down in the form [37]

f(ϖ,Ϥ)=ksinϖ-L/2L/2u(y,0)exp(ikysinϤ)dy.E86

Numerical calculations can be essentially simplified, if one assumes that the field above the antenna is represented approximately in the form [37]

u||y|<L/2z+0u(y,0)exp(ikz).E87

3.3.2. The objective functionals

In the process of statement of the synthesis problem one requires to provide the best approximation to the prescribed FRF in the operating frequency range [k1,k2] and the minimal values of the FRF outside this range, that is for k[k0,k1) and k(k2,k3].

The variational approach for solving this problem was developed in [37]. Modification of variational statement of the synthesis problem is proposed. The problem consists of determination of functions d(y) and ϟ(y), which maximize FRF ϕ1 in the operating range [k1,k2]. In this case, the least value of FRF in this range is specified as a criterion of optimization, and this value is maximized by a choice of functions d and ϟ. That is, the functional is maximized

ϕ1=maxmink1kk2ϕ(k).E88

The additional parameter of optimization 1-|R1(k)|2, where R1(k) is the reflection factor of the main wave in exciting waveguide, with some weight multiplier can be included into functional (88). In this case, the transparency of waveguide aperture can be also used as an additional parameter of optimization.

Minimization of FRF outside the operating frequency range is one of requirements of electromagnetic compatibility for radiating systems [36]. Thus, the value of FRF should remain the largest in the main frequency range. Under these requirements, the following generalization of the variational statement of problem is considered: to find functions d and ϟ, maximizing the functional ϕ1, and, at the same time, minimizing additionally the following functional [6]

ϕ2=minmaxk0k<k1,k2<kk3ϕ(k),E89

that is, minimization of the maximal FRF value outside the [k1,k2] range is required. Of course, it is necessary to take into account the restrictions on the functions d(x) and ϟ(x) owing the physical reason:

d0<d(y)<dm, ϟ0<ϟ(y)<ϟm.E90

For example, d0,dm are the boundary values of height, which provide the single-mode conditions in antenna, and ϟ0,ϟm are the boundary values of transparency, which provide a good quality of antenna in the required ranges. Moreover, the received functions should satisfy the additional conditions of smoothness, which can be formulated as restriction on the second derivatives

|d''(y)|M1, |ϟ''(y)|M2.E91

3.3.3. The modeling results

The numerical results are shown in Fig. 6. Calculations were carried out for the problem of ϕ maximization in range ±5.0% in neighborhood of the central frequency (kc=6.0). It is necessary to minimize the FRF outside of this range for 5.2<k<5.6 and 6.4<k6.8. Parameters of antenna are the following: the length of antenna L=6.0, half-width of excited waveguide l/2=0.3L, number of considered reflected waves in waveguide N1=5, number of waves in a background N2=20.

The optimized values of FRF are marked by solid line in the basic and additional ranges; the dashed line corresponds to not optimized values of ϕ in the main and additional ranges.

Process of additional optimization is carried out on the simplified procedure, that is the control of decrease of the FRF in the basic range is omitted [Andriychuk Zamorska, 2004]. Therefore, the values of FRF in the basic range are slightly decreased in comparison with the FRF values for initial problem.

The optimal form d(y) of the lower boundary of antenna and transparency ϟ(y) of the upper boundary are slightly different for the both cases of optimization.

In Fig. 7, the change of the FRF values at three points of main and additional ranges of frequency (two extreme points and middle one) is shown. The width of main range is equal to 8.33%, and width of additional range is equal to 10.0%. In Fig. 7a, curve 1 corresponds to the central value of frequency k=12.0, and curves 2 and 3 correspond to the extreme points k=11.0 and k=13.0 respectively. In Fig. 7b, curve 1 corresponds to the central frequency k=14.0, and curves 2 and 3 correspond to the frequency values k=13.01 and k=15.0. One can see that the main optimization takes place in the first iterations; there is the improvement only in low-order digit in the next steps. Therefore, it is enough to make 3-5 steps for the main range and 9-11 steps for the additional range, in iterative procedure to receive the practically interesting results.

The total number of iterations also depends on the width of the considered frequency ranges.

3.4. Phase synthesis problem for cylindrical array

The phase distributions of excitation currents in the array’s elements are the optimizing parameters in the problem of phase synthesis. The optimization of considered functionals is reduced to the solution of the corresponding system of nonlinear equations. The gradient methods for direct optimization of functionals are used in practical applications.

3.4.1. The RP of array

A series of simplifications in process of synthesis of the cylindrical array is used in order to reduce the computing time [9, 22]. Separation of variables onto the vertical and horizontal components for the distributions of currents in the array elements, as well as for the RPs, is one of the simplifications.

Thus, the expressions for current Inm(x,y) in radiators and RP f(ϖ,Ϥ) have the form [4]

Inm(x,y)=Inm1(x)Inm2(y),E92
f(ϖ,Ϥ)=f1(ϖ)f2(Ϥ).E93

It is assumed that the radiating elements are flat apertures, for example, end of open waveguide. The RP depends on the angular coordinates ϖ and Ϥ. From the practical point of view, the consideration of such models of the arrays is justified by the fact that they allow to receive the values of required radiation characteristics with the accuracy of 2% - 5%, while the time of solution for the respective problems of analysis (determination of the RP of array), considerably decreases. Such approach to the solution of direct electrodynamic problems is effective especially for the arrays with constant coordinate surfaces, e.g., for the plane, cylindrical and conical arrays. Proceeding from the above assumptions, we separate the synthesis problem of such arrays into two synthesis problems for the linear and circular arrays.

The spatial RP of cylindrical array [9] is:

f(ϖ,Ϥ)=m=1Mn=1NInmfnm(ϖ,Ϥ)exp(ik(zmcosϖ+asinϖcos(Ϥ-Ϥn))),E94

where N is the number of radiators in circular subarray (identical for all subarrays), M is the number of circular subarrays, a is radius of cylinder. The currents Inm are complex numbers, by means of which choice the approximation to the given amplitude RP F(ϯ,Ϥ) is carried out.

The functions fnm(ϯ,Ϥ) are the RPs of separate radiators, (zm,a,Ϥn) are the coordinates of radiators. The RP of separate radiators is identical and can be presented in the following form

fnm(ϖ,Ϥ)=fn(Ϥ-Ϥn)fm(ϖ).E95

Following the above assumptions, the RP (94) can be written as

f(ϖ,Ϥ)=fl(ϖ)fc(Ϥ),E96

where

fl(ϯ)=A1I:=m=1MImfm(ϯ)exp(ikzmcosϯ)E97

is the RP of linear array, and

fc(ϖ,Ϥ)=A2In=1NInfn(Ϥ-Ϥn)exp(ikasinϖcos(Ϥ-Ϥn))E98

is the RP of circular array for each ϖ. Below we consider the synthesis problem for the circular array.

3.4.2. Optimization criteria

The complex currents in the array elements are determined by their amplitudes and phases. We denote these values |In| and Ϧn, respectively. The amplitudes |In| of currents are prescribed together with the amplitude RP F in the problem of phase synthesis. The phases Ϧn are the optimizing parameters. We use the functionals (29) and (33) for optimization.

The equalities

ϥ=argA(|I|eiϦ),E99
Ϧ=argA*(Feiϥ).E100

should be satisfied at the points of functional (33) maximum. This set yields the system of transcendental equations for the phases Ϧ of current and phase RP ϥ.

Using normalization of the current I values: ||I||=1, we write down the functional (33) in two equivalent forms

Ϙ=(Feiϥ,A(|I|eiϦ))f=(A*(Feiϥ),|I|eiϦ)I,E101

where ϥ=argf is the phase RP. The operator A* is adjoint to A and determined similarly to [Andriychuk et al., 1993].

At first, we consider the problem of Ϙ maximization. Substituting (99) into (100), we receive the system of nonlinear algebraic equations for optimal phase distribution of currents

Ϧn=argA*(Fexp(iargA(|I|eiϦ))),n=1,2,...,N.E102

In practice, the system (99), (100) is more convenient for the numerical solution. For this reason, we use the following iterative process

argf(k)=argA(|I|exp(iϦ(k))),E103
Ϧ(k+1)=argA*(Fexp(iargf(k))E104

to find the phases Ϧ(k+1).

The gradient methods are more convenient to solve the minimization problem for the functional ϡ. The method of conjugated gradients [28] is the most suitable for this purpose. In this method the next approximation of phase vector Ϧ={Ϧn,n=1,...N} is calculated by the formula

Ϧ(k+1)=Ϧ(k)+ϒ(k)h(k).E105

Here

h(k)=z(k)+ϑ(k)h(k-1),E106
z(k) is the gradient of ϡ with respect to the phases of currents in the "point" Ϧ(k). The components of vector z(k) are the following
zn(k)=-Im{(A*((F-s|f(k)|)exp(iargf(k))))nIn(k)},n=1,2,...,N.E107

Parameter ϒ(k) is determined from minimum of ϡ being a function of this parameter.

In practice, it is necessary to solve the problem of discrete phase synthesis [9, 22], because the arbitrary phase distributions cannot be realized in the array radiators. These distributions are prescribed as a set of discrete values, which are multiple to the given phase discrete value β, that is Ϧn=ϙnβ, the integers ϙn are unknown in this case [5, 7].

The algorithm consisting of two enclosed iterative processes is used for the solution of this problem. The value of phase Ϧn is improved in the n-th step of the internal iterative process, the phases in other radiators remain fixed. At the same time, the mean-square deviation of the synthesized RP and function Fexp(iargf(k)), where argf(k) is the phase RP, which is received in the previous step of external iterative process, is minimized. The phase RP argf is improved in the external iterations.

The internal cycle consists of the successive improvement of phases in the separate radiators changing their number from 1 up to N. The value of ϡ decreases in each step of internal cycle.

The new phase RP argf(k+1) is calculated by the found values of {Ϧ} in external cycle. The values of ϡ corresponding to new phase RP also decrease, what provides the convergence of the whole algorithm. In view of the step-type behavior of Ϧn values, this convergence exists not only for a sequence of ϡ, but also for the phase distributions. The iterative process is considered completed, if there is no change of Ϧn in the internal cycle.

The problem of discrete phase synthesis is solved in two steps. In the first step, the synthesis (with small accuracy) without the account of phase discrete values is carried out. After that, the found phases are approximated up to the nearest discrete values. In the second step, the described above algorithm of discrete synthesis is used. As a rule, one is enough to make several external cycles in the latter algorithm.

3.4.3. The results of numerical modeling

The numerical results are given for the sector array. The RPs of separate radiators have a cosine form, and mutual coupling of separate radiators is not taken into account [35]. The number of radiators N=32, the radiators are placed in active sector ϐ=90o.

The synthesis results are shown in Fig. 8 for the bi-directional RP

F(φ)={|sin18φ,|φ|<5.00,0,|φ|5.00.E108

The thick line corresponds to the prescribed amplitude RP F, and thin line corresponds to the synthesized RP |f|. The prescribed F and synthesized |f| RPs coincide in the main lobe up to level –20 dB, the level of side lobes does not exceed -20 dB (see Fig. 8a).

In the practical applications, the problem of phase scanning [35] is considered for arrays. The array alongside with creating the amplitude RP which is more close to the desired one should provide the moving this RP along the angular coordinate in the scanning process. This moving is carried out by the change of the phase distribution {Ϧn} only; the amplitudes {|In|} of current remain constant. In fact, the problem of phase synthesis is solved for each scanning angle Ϥs separately.

The difference between the results of continuous and discrete synthesis depends on the value of phase discrete β. The smaller the difference, the smaller this value. In Fig. 8b the values of ϡ for two types of synthesis are shown for the process of scanning, Ϥs is changed in range from 10 up to 90. Solid line corresponds to the case of continuous synthesis, and dashed line correspond to the case of discrete synthesis, the value of β=22.50. This value of β gives not big difference for two types of synthesis. So, the difference between F and |f| in main lobe of RPs does not exceed 1dB, and this difference does not exceed 10dB in the side lobes. Such difference is satisfactory for the engineering practice. Of course, the above mentioned difference grows if the scanning angle Ϥs approaches to the left or right border of the active sector ϐ.

3.5. Investigation of branching solution

The problem of the non-uniqueness of solutions for phase synthesis problem is investigated on the example of linear array.

The various modifications of the Newton method have been developed for solving the nonlinear equations in [13], and have been detailed for the synthesis problems in [11]. We consider here the above approach for determination of the number of solutions and investigation of its properties by the example of the nonlinear equation (46), corresponding to functional Ϙ (33).

Let the operator A describe the RP (array factor) of linear array [4].

f(Ϝ)=Av:=c2Ϟn=-MMvnexp(icnϜ),E109

where c=kasinϏ, a is the radius of array, Ϗ is the angle in which the RP F is non-zero, N=2M+1 is a total number of array elements, Ϝ is the generalized angular coordinate. The operator A*acts in the following way

A*f=c2Ϟ-Ϟ/cϞ/cf(Ϝ)exp(-icnϜ)dϜ,E110

In this case, the functional (33) can be presented as

Ϙ(Ϧ)=-Ϟ/cϞ/c|f(Ϝ)|F(Ϝ)dϜ.E111

3.5.1. The numerical results

The numerical calculations are carried out for the prescribed amplitude radiation pattern F(Ϝ)=cos(ϞϜ/2) and are shown in Figs. 9 and 10. In Fig. 9a, the values of Ϙ and ϡ are shown for various types of initial approximation of the current’s phase Ϧ(0)(x). For this case, the maximization problem of Ϙ is equivalent in some sense to minimization problem of ϡ [Andriychuk et al., 1993].

The solid lines correspond to values of Ϙ, and the dashed lines correspond to values of ϡ. The number of array elements N=11, parameter c changes from c=0 up to c=2. For the values of Nc which do not exceed Nc=5 all types of solutions give the same values of Ϙ and ϡ. At Nc2Ϟ the branching of solutions appears, and optimal value for Ϙ and ϡ functionals gives the solution with even phase Ϧ. The prescribed amplitude radiation pattern F and synthesized |f| are shown in Fig. 9b. The amplitudes |f| in the considerable extent differ from the amplitude F because of small value of c parameter (c=1.6).

The optimal values of sought phase distributions Ϧ are shown in Fig. 10a, the given current amplitude distribution is |I|1. The optimal phase distributions Ϧ keep the parity properties of corresponding initial approximations Ϧ0. The optimal values of Ϙ and ϡ provide the solution with phase distribution Ϧ0(x)=cos(x) (see Fig. 9).

The quality of approximation to prescribed amplitude pattern F too much depends on the parameter c (see Fig. 10b). At c=3.14 the Ϙ and ϡ values are noticeably smaller than for c=1.6, although the value of N is larger in case of Fig. 9.

3.6. Synthesis of waveguide array

The mutual coupling of the separate elements of array is taken into account in the process of solution of a direct problem (analysis problem) [7, 14].

3.6.1. Statement of synthesis problem

The objective functional is formulated as [4]

ϡ=χ(F(ϖ,Ϥ)-|f(ϖ,Ϥ)|)2dϖdϤ+tn=1NSn|In(xn,yn)|2dxndyn,E112

where N=2M+1 is a number of exciting waveguides, F(ϖ,Ϥ) is the prescribed amplitude RP, |f(ϖ,Ϥ)| is the amplitude of synthesized RP, In(xn,yn) are the currents in the waveguide apertures. Geometry of waveguide array is shown in Fig. 11.

The determination of the currents In(xn,yn) in the waveguide apertures (the solution of analysis problem) results in solution of the integral equation system [14].

The RP (array factor) [9] of array is:

f(ϖ,Ϥ)=n=1Nanexp[ik(xn0sinϖcosϤ+yn0sinϖsinϤ)],E113

where xn0 and yn0 are the coordinates of central points of apertures, an is the complex excitation coefficient for n-th waveguide.

Introducing the generalized angular coordinates Ϝ1 and Ϝ2, we receive the expression for the RP

f(Ϝ1,Ϝ2)=n=1Nanexp[ik(xn0Ϝ1+yn0Ϝ2)],E114

where

Ϝ1=sinϖcosϤ, Ϝ2=sinϖsinϤ,E115

and finally

f(Ϝ1,Ϝ2)=Aa:=n=1Nanfn(Ϝ1,Ϝ2),E116

where a={a1,a2,...aN}, fn(Ϝ1,Ϝ2) are the RPs of separate waveguides.

The expression (116) indicates that the calculation of array factor f(Ϝ1,Ϝ2) using the excitation coefficients an is realized by the linear operator A. The coefficients an will be the optimization parameters in the synthesis problem. Solving the synthesis problem, we minimize the functional ϡt (34).

3.6.2. The modeling results

The results of numerical calculations are presented for the waveguide arrays consisting of 15 and 31 radiators; kl=1.2, kL=18.75, k is wavenumber, l and L are width and length of waveguide aperture respectively. The prescribed amplitude RP is: F(ϖ,Ϥ)=F1(ϖ)F2(Ϥ), where

F1(θ)={1,|θ|π/200,|θ|>π/20,F2(φ)=(cosφ)64.E117

In Fig. 12, the dependence of the synthesis results on the value N of waveguides is shown. It is easy to see, that the synthesized amplitude RP has narrower main lobe if N increases. The level of the first sidelobe is -30.26dB and -30.71dB respectively. The low level of sidelobes and velocity of its decrease is very important characteristic of the synthesized amplitude RPs. As rule, one requires the level of first sidelobe not greater than -20dB and not very slow decreasing the next sidelobes. The above mentioned characteristic for the synthesized amplitude RP in the plane Ϝ2Oz are shown in Table 2. The amplitude RP |f| at N=31 has lower first sidelobe -30.71dB and faster decrease of the far sidelobes.

 Sidelobe: 1st 2nd 3rd 4th 5th N=15 -30.26 -40.43 -46.25 -50.63 -53.27 N=31 -30.71 -40.83 -47.52 -52.45 -56.33

Table 2.

The level of sidelobes (in dB) corresponding to array with various N

4. Conclusions

In the process of solving the amplitude-phase synthesis problem, the influence of weight multiplier t on the synthesis results was investigated. It turned out that the mean-square deviation of the prescribed F and synthesized |f| amplitude RPs diminishes if t decreases. At the same time the norm ||I|| of current grows. This testify that one should take into account the above fact in order to receive the solution with smaller mean-square deviation of the RPs or with small norm of current. The elaborated iterative procedures guarantee convergence of the successive approximation methods for numerical solving the arising non-linear equations.

The proposed approach for solving the synthesis problems of resonant antennas is universal, and it provides the possibility to synthesize antennas with the arbitrary form of external boundary. The calculation time of the RP of antenna is small enough what it is very important in the process of solution of the synthesis problem. The used variational statement of the synthesis problem also allows to take into account restrictions on the field at the given points (areas) of a near zone.

The synthesis of the resonant antenna with waveguide excitation gives the possibility to take into account the various requirements to the FRF in the operating frequency range. The developed algorithms enable to optimize the values of FRF in the single range, as well as in the several frequency ranges. The values of the objective parameters d and ϟ, which are received in the process of numerical calculations, are constructive characteristics of resonant antenna and they can be directly used in the antenna design.

The variational approach for solving the phase synthesis problem can be applied effectively for the plane, cylindrical and conical arrays. It allows to decrease the computational time, at the same time the accuracy of determination of the array characteristics is sufficient for practice. The branching solutions are investigated for the case of linear array. It is shown that one can receive the solutions with various properties starting the iterative process with different initial approximations.

The considered optimization problems of waveguide array give the possibility to take into account the requirements to the amplitude RP and amplitude-phase distribution of field in the aperture of exciting waveguides. The developed algorithms enable to achieve the minimal mean-square deviation ϡ of the prescribed and synthesized amplitude RPs, and to optimize simultaneously the restrictions on the phase or amplitude characteristics of the excited fields.

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