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11URAL MATHEMATICAL JOURNAL, Vol. 3, No. 2, 2017
NEW METHOD OF REFLECTOR SURFACE SHAPING TO PRODUCE A PRESCRIBED CONTOUR BEAM1
Boris V. Semenov12t, Nikolai I. Chernykh12tt, Viktor M. Pleshchev1"^
1Krasovskii Institute of Mathematics and Mechanics, Ural Branch of the Russian Academy of Sciences, Ekaterinburg, Russia;
2Ural Federal University, Ekaterinburg, Russia, [email protected], [email protected], [email protected]
Abstract: In this paper a simple iterative synthesis method is presented for the formation of the shape of the reflector surface with a single feed element to produce the desired contour beam. This is the method of the optimal phase synthesis of the appropriate field in the reflector aperture similar to other works. But unlike them, we solve the problem in a very simple way using the properties of complex-valued functions and Fourier transforms and not applying complicated methods of numerical minimization theory.
Key words: Antenna, Shaped reflector, Radiation pattern, Contour beam, Synthesis.
Introduction
We consider the problem of synthesis of antenna reflector surface with a single feed. Such surfaces are constructed to generate a desirable far-field pattern available for the reflector aperture.
There are antennas with a single feed that form contour beams by means of appropriate profiled reflector surfaces for serving separated districts from spacecraft. They have a very simple construction, are reliable in exploitation, and optimally solve problems of electromagnetic compatibility.
Several synthesizing methods are known for the problem. They proved themselves to be efficient but are related to the minimization problems of multi-parameter goal functions. Some of these methods are direct methods for optimal modification of the basis reflector surface represented by polynomials, splines, and wavelets [1-4]. Other methods are related to preliminary synthesizing the electromagnetic fields in the reflector aperture which generate the assembly of narrow partial beams with subsequent optimization of the disposition of their maximums and selection of their superposition parameters. After that, the computation of the reflector surface form is carried out to generate the synthesized optimal aperture field [5-10]. The developed methods are very efficient for the synthesis of the reflector surface with the diameter of several tenth of the wavelength.
In this paper, another method is presented for contour beam synthesizing by antenna with a single feed element and a special reflector shape. It is also related to solving optimization problems but without the application of multi-parameter nonlinear optimization theory. The method is entirely based on the specific setting of the reflector surface synthesizing problem and on the properties of complex-valued functions and Fourier transforms. It is possible to adapt the method to the problem of phase control of large radiating arrays in real time.
The computation of the electric field in opening of the initial reflector (for example, parabolic revolution with focus at the phase center of the feeding element) is carried out in the knots of the uniform lattice at very close aperture. It is implemented by means of a vector radiation model of
1This work was supported by the Program for State Support of Leading Scientific Schools of the Russian Federation (project no. NSh-9356.2016.1) and by RAS Presidium programm "Mathematical Problems of Modern Control Theory".
the array, which has a sufficiently dense set of points on the initial reflector surface. Dimensions of the lattice cells must guarantee the exact calculation of the Kirchhoff integral for the far zone field.
Our method, like many others, is iterative. The phase synthesis of a given pattern for the minimization of the amplitude distribution deviation from the desired far-field pattern is performed in L2(R2) space. We apply (here, perhaps, for the first time) the iterative methods alternately using direct and inverse Fourier transforms. It does not require any classic ways of numerical differentiation and solutions of large systems of linear equations. The mentioned iteration procedure is implemented until a completely suitable phase distribution at the reflector aperture is found. Moreover, the procedure may be accompanied by a proper shaping of the reflector surface at every step of the iteration. To represent intermediate variants of the constructed surface, we make it "scaly". Every "scale" is a fragment of a parabolic surface having the same focus as the initial one. Of course, we do not consider the diffraction at the edges of these (virtual) "scales", because, at the final stage of optimization, the weakly discontinuous surface will be changed by a continuous and smooth one.
1. Physical and phenomenological basis of the method
Bellow, the size and contour of the aperture, the pattern of the feed element, and model D(d, <p) of the required far-field radiation pattern are supposed to be given. The latter can be a model of different beams, including contour ones, whose parameters conform to the reflector opening.
Getting to the problem, we assume that the initial reflector surface is cut off from a paraboloid of revolution by a plane orthogonal to its axis. The corresponding part of the plane is assumed to be its aperture A containing the origin O and the axes OX and OY of the Cartesian coordinate system, whose axis OZ coincides with the axis of the parabolic surface and contains its focus F coincident with the phase center of the feed element.
At first, it is necessary to the calculate electric field at the aperture A (more exactly, its component E(x,y) on the chosen polarization). It should be done very precisely, because it is possible (although not necessary) do not change the amplitude distribution E(x,y) = |i?(x,y)| in the aperture A in future (neglecting the weak influence of local shifts of primary reflector surface cells). The phase S0(x,y) = argE(x,y)/(2n) will be the initial functional "parameter" which we are going to change in the course of the reflector surface synthesis. The electrodynamic problem of searching the field E(x, y) is not considered in this article, since it can be solved by other known methods. We found that the computation according to the vector model formulas (see, for example, [13]) is very efficient.
2. Model of the algorithm
First we expound a continuous version of the algorithm for the synthesis of the reflector surface, which will be necessary to carry out numerically. Knowing E(x, y) in the reflector aperture A, we have a representation of the electric field expected in the far zone as the Kirchhoff integral
E(u, v) = jj E(x, y)e-2ni(ux+vy) dxdy, (2.1)
A
where u = k sin d cos <p, v = k sin d sin <p, (9,<p) are the angles of the spherical coordinate system, k = 1/A, and u,v are dimensionless variables, because x, y are measured in wavelengths. The function S0(x,y) is determined from the condition E(x,y) = E(x,y) exp(2niS0(x,y)). Although it involves the phase component of the feed, it can be interpreted as the length of the optical path from a point (x, y) € A through the corresponding point on the reflector surface and then up to
the phase centre of the feed (also measured in wavelength). Disregarding diffraction at the edge of the reflector, we suppose that the antenna radiation extends only to the half-space z > 0 and E(x,y) = 0 under the condition (x,y) € R2\A. Thus, from the previous reasoning and (2.1), we have
E(u, v) = E(u, v, S) = f j E(x, y)e2niS(x,y)e-2ni(ux+vy) dxdy, S = S0, (2.2)
R2
that is the Fourier transform of the predetermined function F(x, y). If needed, we smoothly extend the given contour model D(u, v) of the radiation pattern a little outside the domain of interest and, denoting the new domain by Q, we set D(u, v) = 0 for (u, v) € R2\Q. We can define the mean square deviation by the formula
( \ 1/2 A(D,F)=: ||D(u,v) — |E(u, v; S)||| = ( //(D(u,v) -|F(u,v; S)|)2 dudv ) , (2.3)
and formulate the following problem of antenna phase synthesis: to find a function S(x,y) = S(x, y; D) for which the value
5 =: inf A(D(u, v), F(u, v; S)) (2.4)
is attained. Here, S belongs to the class of all measurable real-valued functions. It should be noted that only a part of R2 (the ball u2 + v2 < 1) really lies in the physical space. But, in problem (2.4), we also minimize the energy flow
2 r f 2
dudv
E(u, v; S) dudv = J J D(u, v) — E(u, v; S)
in the antenna reactive zone. Further, we apply the usual iterative procedures for phase synthesis worked out for hybrid reflector antennas (HRA) (see, for example, [11, 12]), but here they are especially clear because do not use a finite-dimensional approximation of the antenna radiation E(u, v; S).
Obviously, we have
52 = inf inf yI D(u,v)e^(u'v) — F-(E(x,y)e2niS(x'y))(u,v)
2
dudv =
R2 (2.5)
= inf inf
^ S
R2
F+(D(u, v)ei^(u'v) )(x, y) — E(x, y)e2niS(x'y)
2
dxdy,
where ^(u, v) is a real-valued measurable function like S(x,y) and functions (F±g)(s,t) are inverse (with +) and direct (with —) Fourier transforms defined for a function g € L(R2) by
(F±g)(s,t) = JJg(C,C)e±2ni(s«+iZ) d£d(,
and then extended to L2(R2) in a reasonable well-known way. To represent 5 defined by (2.4) as like (2.5), we have used the following considerations:
1) from the properties of complex-valued functions, it follows that the first integrand in (2.5) is minimal for ^ equal to defined
^S(u, v) =: arg E(u, v; S) = arg(F-(Ee2niS))(u,v) = arg F-(E)), (2.6)
so the inner infimum over ^ coincides with A2(D, E) (see (2.3)) in view of formulas (2.2)-(2.4) and the definition of F-g;
2) it is easy to see that, for any positive functional G(S, on the spaces of real-valued measurable
functions S(x,y) and ^(u,v), the following formula inf inf G(S,^) = infinf G(S,^) holds;
s ^ ^ s
3) the equality of integrals in (2.5) follows from the Parseval equality.
Reasoning as in 1), we see that the inner infimum in the last part of (2.5) is attained for 2nS equal to
2nS(x, y) = 2nS^(u, v) =: arg(F+ (De^))(x, y). (2.7)
From these considerations, it follows that the solution S(x, y) ((x, y) € A) of problem (2.4) together with the solution ^ of the problem
inf
E(x,y) - F+(De^)(x,y)
dxdy
R2
must be connected by the nonlinear equations (2.6) and (2.7). Except for special cases, this system can be solved only approximately by a numerical method.
To construct such a method, we use the obvious fact that, for every above mentioned functions S(x,y) and ^(u,v), we have the following inequalities for the norms in the space L2(R2) hold:
De^s - F— (Ee2niS) < De^ - F— (Ee2niS)
„2niS\
F+(De^) - Ee
J2niS
F+(De^) - Ee
_2niS,
<
F+(De^) - Ee
_2niS
L2(R)
(2.8)
(2.9)
where ^S and S^ are defined in (2.6) and (2.7). Further, beginning with the function S0(x,y) and alternately using formulas (2.6) and (2.7), we construct the following chain of functions:
^Sc(u,v), S^ (x,y) =: Si(x,y), ^Sx(u,v),
S2(x,y) =: S^ (x,y),.. (u,v), Sn =: S
Denoting
Sn(x,y) - Sn-i(x,y) =: An-i(x,y) (n € N, (x,y) € A), Sn = 11De^Sn - F—(Ee2niSn)|| = ||F + (De^sn) - Ee2niSn, On = ¡F+(Dei^Sn) - Ee2niSn+1 H = ¡De^Sn - F—(Ee2niSn+1 )|
(2.10)
and assuming that S = Sn(x,y) and ^ = (u,v) in (2.8) and S = Sn(x,y) and ^ = ^Sn (u,v) in (2.9), we deduce the inequalities
^ On—l ^ o ^ On ^
Since the formulas ^Sn = arg F (Ee2mSn) and F (Ee2mSn) = E(u,v; Sn) hold, we have that
(n = 1,2,...).
2niSn
on =
D - \E(u, v; Sn)|
is the distance between the desired radiation pattern and the realizable
pattern |E(u,v;Sn)|. This distance decreases to some value 5^(S0) as n ^ ro, which cannot be zero, because the finitely supported function D(u,v) is not an entire function. For different S0(x,y), the sequences {Sn(x,y)} may differ too, since problem (2.4) is a set-valued extremal one (for example, \E(u, v; S)| = \E(u, v; S+const)|). Nevertheless, for large n, the function |E(u, v; Sn)| inherits the main features of D(u,v). We verified this fact in many computing experiments.
2
3. Computation procedures
It is natural to begin the construction of the sequence {Sn(x,y)} with calculating So(x,y) = argF(x,y) = F(x, y)/|F(x, y)| over the nodes of a chosen lattice and stop it when the replacement of by negligibly changes the value max |An-1(x,y)| or the value
max |F(u, v; Sn-1) — E(u, v; Sn)|.
In practice, the range of values (ux + vy) is not large, so oscillations of the function exp(—2ni(ux + vy)) are also not large. Therefore, an approximate computation of the integral in the Fourier transforms over any dense lattice does not cause any difficulties and the construction of the sequence {Sn} almost does not need any additional calculations.
4. Synthesis of the reflector surface
x2 + y2
The initial parabolic reflector surface z = ——--zo (zq > 0, x2+y2 < 4/zo) can be corrected
after each step of replacement of Sn-1(x,y) by Sn(x,y). It is possible to do this more rarely or at the end, i.e., immediately after the computation of SN based on the difference Sn(x,y) — So(x,y). Below, we use the first strategy.
Let cells of the chosen lattice over the aperture A be the squares with size h x h and midpoints Mj with coordinates x, = ih, yj = jh (i, j = 0, ±1,..., ±k, where (k + 1/2)h =: r, and r is the radius of A) and with the conditions (xi, ijj) € A. Here, we have r = ^JAfzo, F{0,0, /, — zo) is the focus of the paraboloid, the cells m,j of the lattice are framed by the lines (x = x, ± h/2, z = 0) and (y = yj ± h/2, z = 0). Replacing the condition z = 0 by z < 0, we obtain, instead of the cells, the set of tubes tj in the half-space z < 0 of the space R3 whose orthogonal cross-sections are the squares
h h h h
-- + Xi < x < Xi + -, --+Uj<y<yj + -, Z = const < 0
Every tube tj cuts off an initial scale from the initial paraboloid which is part of the paraboloid
X2 + y2 ( x2 + y2 \
z =----zo, (x, y) € rriij, intersecting the axis at tij at the point Xi, yj, ———— — zo .
4/ V 4f /
Further, we use analogous "scales" which are cuttings of any other paraboloid Pj with the same axis of symmetry OZ and focus F. The cuttings are embedded in the tubes tij and contain any given point M(xi,yj- ,zij) on their axes. It is easy to verify that the equation of the paraboloid Pj for the given zj is
x2 + y2 „
z = ^jT.--(x>y) ^ mij> (4-n)
where the focal distance /¿j and the zth vertex coordinate zj are defined by the relations
{4/jj(zjj + zjj) = x2 + y2, /¿j — zjj = / — zo, /¿j > 0, zjj > 0} . (4.12)
Since the function exp(—2niS(x,y)) of S is A-periodic, it is quite possible to locally change the function S(x, y) in the Kirchhoff integral (2.2) by (S(x, y) — n) with an arbitrary integer n up to [S(x,y)]. Hence, taking into account the first notation in (2.10) and determining S1(x,y), we can compensate the difference A1 (x,y) by small shifts and simultaneously change all initial scales o0j by a,1,- whose coordinates z0,- are determined from the conditions
|FMj | + |Mj M,j | = So (M,j) + Ao(M,j) — Ao(0,0) + (n0j )A. (4.13)
Here, we assume that n°0 = 0, so, the location of is not changed. The other numbers n0j determining the points M0 must be chosen layerwise around M00(0,0, — z0) to minimize the distance \z®j — z01j1 \ between the neighbouring points Mj and Mixjx.
The further steps of the iteration procedures are implemented according to the same principles: using (2.6) and (2.7), we find the recurrent phase distribution S0(Mj) (Mij € A) and compensate the differences An-1(Mij) by numerical construction of the corresponding new scaled surface of the reflector as explained above in the case n = 1. Just in this construction, we must replace the set of points M0j by Mfj and perform all calculations for n = 1,2,... according formulas (4.11)-(4.13).
In this section, we described how to choose a number N to stop the iterations. In the final stage, it will be necessary to smooth the constructed weakly discontinuous surface z = fN(x,y) built of little scales nNj. A fairly good result could be obtained as a close solution of the approximation problem
\\fN(x,y) — S2(x,y)|| + a ||S2(x,y)|| ^ inf
for the function fN(x,y) by using quadratic or cubic splines S(x,y). This problem was completely investigated in [14]. Perhaps it would be useful to recompute the amplitude distribution on the aperture A after each next version of the modified reflector surface and to change the function E(x, y) in the corresponding Fourier transforms (2.2).
Fig. 1 shows an example of a far-field pattern of the cosecant type for the antenna with a single feed element and the reflector surface shaped by the described method. The results of the synthesized contour beam for Europe and the corresponding reflector surface form are presented in Fig. 2. Other examples can be found in [15].
5. Conclusion
In this work, we describe a new iterative method for numerical shaping of the locally curved shape of the reflector surface for the antenna with a single feed element. The antenna must generate a beam with a prescribed contour of its cross-section. The method has some common features with other known methods, in particular, stated in the papers from the list of references. Our method mainly differs by the technique of minimization in the problem of aperture phase synthesis, which makes it possible to shape reflectors of large diameter. The method was tested in many computing experiments and showed itself as efficient.
6. Acknowledgments
The authors are grateful to N.A.Baraboshkina for collaboration in the work on this paper.
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Figure 1. Example of the synthesized far-field pattern of double cosecant type
A
Figure 2. Example of the synthesized contour beam for Europe and the corresponding reflector surface form (contour plot of a deflection of a of the synthesized reflector surface from an initial paraboloid are shown with a step 0,01 wavelength A)
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