base, 4 28 057 · 2011. 5. 14. · ad-a278 788 rl-tr-93-265 interim report december 1993...
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AD-A278 788
RL-TR-93-265Interim ReportDecember 1993
GREEN'S FUNCTIONS FOR ANANISOTROPIC MEDIUM: PART II. TWO-LAYER CASE
ARCON Corporation
Saba MudalarTIC
I ELECTEMAY 0 2 19941
APPROVED AVR PUM, RELEASE, DIS TRIBUrTON UNLIM//ED.
Rome Laboratory
94-12985 r Force Materiel Commandllll , ~ ~ ' ,,Hiss Air Force Base, New York
"94 4 28 057
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This report has been reviewed by the Rome Laboratory Public Affairs Office(PA) and is releasable to the National Technical Information Service (NTIS). AtNTIS it will be releasable to the general public, including foreign nations.
RL-TR-93-265 has been reviewed and is approved for publication.
APPROVED:
ZACHARY 0. WHITEProject Engineer
FOR THE COMMANDER
JOHMN W.sHTNDLEVRDirectorElectromagnetics & Reliability Directorate
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REPORT DOCUMENTATION PAGE o. proveMBNo. 0704-0188
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1. AGENCY USE ONLY (Leave B* 2. REPORT DATE 3. REPORT TYPE AND DATE$ COVERED
December 1993 Interim Jan 93 - Oct 93
4. TITLE AND SUBTrTLE 5. FUNDING NUMBERS
GREEN'S FUNCTIONS FOR AN ANISOTROPIC MEDIUM: PART II. C - F19628-89-C-0186TWO-LAYER CASE PE - 62702F
8. AUTHOR(S) PR - 4600TA - 14
Saba Mudaliar WU - 26
7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) 8, PERFORMING ORGANIZATION
ARCON Corporation REPORT NUMBER
260 Bear Hill Road N/AWaltham MA 02154
9. SPONSORINGJMONITORING AGENCY NAME(S) AND ADDRES(ES) 10. SPONSORING/MONITORINGAGENCY REPORT NUMBER
Rome Laboratory (ERAA)31 Grenier Street RL-TR-93-265Hanscom AFB MA 01731-3010
11. SUPPLEMENTARY NOTESRome Laboratory Project Engineer: Zachary 0. White/ERAA/(617) 377-3191
12a. DISTRIBUTION/AVALABUTY STATEMENT 12b. DISTRIBUTION CODE
Approved for public release; distribution unlimited.
13. ABSTRACT(Ma*-2 ad!nI
The Dyadic Green's Functions (DGF) of a two-layer biaxially anisotropic medium arederived. The principal coordinate system of the anisotropic medium is allowed tohave arbitrary orientation with respect to the layer geometry. The formulation isbased on the unbounded Dyadic Green's Function derived in Part I of the sequel.Using the matrix method the coefficients of the two-layer DGF are expressed in termsof half-space Fresnel reflection and transmission coefficients. To complete thisprocedure the various relevant half-space Fresnel coefficients are derived. Theform in which the results are presented has a physically meaningful and compactstructure. A numerical example is provided where we have computed the reflectivities.
14. SUBJECT TEFMS 11 UMBER OF PAGES
Green's Functions, Electromagnetic Waves, Anisotropic Medium, 36
Layered Medium Ia PRCE COoE
17. SECURITY CLASSIFICATION 18. SECURITY CLASSIFICATION 19, SECURITY CLASSIFICATION 20. LIMITATION OF ABSTRACTOF REPORT OF THIS PAGE OF ABSTRACT
UNCLASSIFIED UNCLASSIFIED UNCLASSIFIED ULNSN 75403,6t-2005" St.no5 Form 2% t m e. - E
Prensabed by ANSI Sm Z;' a• ¢ ,•, " ,, ..... .. ... . . ... .. 2 We 02
S... . . . =,,, ,,,ra m mll 1 • I1•1 • • 4
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TABLE OF CONTENTS
1. Introduction ............................................ 2
2. Geometry of the problem ................................. 2
3. Formulation ............................................. 3
4. Matrix method ............................................. 6
5. Half-space Fresnel coefficients .......................... 10
6. Numerical example ........................................ 16
7. Conclusion ............................................... 17
References .............................................. 19
Appendix A ............................................... 20
Appendix B ............................................... 21
Appendix C ............................................... 23
ILLUSTRATIONS
Figure 1. Geometry of the problem .......................... 25
Figure 2. Amplitude vectors of
waves in two layer medium ................. 26
Figure 3. Reflectivities versus incident angle ............. 27Accesion ForNTIS CRA&I
DTIC TABUnannounced 0Justification
By .......Dist, ibution /
Availability Codes
Avail and I orDist Special
1I
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1. INTRODUCTION
In Part I [Mudaliar, 1993]1 we obtained the dyadic Green's
function (DGF) of a biaxially anisotropic medium for the unbounded case.
It may be noted that the results obtained there are in a form very
convenient for deriving the DGF's for anisotropic layered structures.
Indeed that was one of the underlying motives of Part I. We consider in
this report the two-layer case.
The plan of the report is as follows. In Section 2 we briefly
describe the geometry of the problem. We formulate the solutions of the
problem in Section 3. In order to facilitate the evaluation of the
coefficients of the DGF's we introduce amplitude vectors and adopt a
matrix method in Section 4. The procedure is completed in Section 5 by
deriving various half-space Fresnel coefficients. Finally the report
concludes in Secion 6.
2. GEOMMETRY OF THE PROBLEM
The geometry of the problem is shown in Figure 1. It consists of three
regions: Region 0 ( z > 0 ) is an isotropic medium with permittivity co,
Region 1 ( 0 > z > - d ) is the biaxially anisotropic medium with
permittivity 7 and Region 2 ( z < - d ) is an isotropic medium of
permittivity c 2" All the three regions have the same permeability A. In
this coordinate system the permittivity 7 is represented by the following
symmetric matrix.
- 2
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[£11 12 13]
1 - Vl2 £22 £23 (1)
L 13 £23 33J
where the elements c J are explained in (3) of Part I.
3. FORMULATION
We have a unit impulse electric current source in Region 0 away from
the boundary. Our interest is to find the DCF's: U 00, (r,) and
U2 0 (rr). Here as usual the second subscript denotes the region where
the source is located while the first subscript denotes the region
containing the observation point. In order to obtain the above DGF's we
need to solve the system of equations given in Appendix A. Based on the
knowledge about the structure of the DGF for the unbounded case obtained
in Part I and that of the DGF's for the layered isotropic media2 we can
now construct solutions for our two-layer problem as follows.
3
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G00 (r~r2j A- iR fF~~I {~e A+ 1k 0of
-hv vJh 0 e ]h
•- i•0• A+ ko.?
100 e + R v 0 e 0
+ Rvh h0v+ e ]0- h v 0
(2)
1i0-,) f k • { a e + B ha e
A- ixb.orhA+ ib -f h+ Ahbb e Bhbe 0
._a .-a
A_ A r .r A+ ik.y[ a e + B a eva va
-b . -
+ Avb b e + B vb e
(3)
"4
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"- I "-•20(,)- 8 2 k Oz 2+Xv2
+[ A- A- A- ];ei2"r -ei0"r'+ [ vv V 2 + Xvh h 2 ]V0
(4)
where for n - 0,2
Ah 1. A (Sa)hn k nX z
p
v xi- k h (bn k n n
n
1 - (5c)V n i P- n xhnni
A (6a)-=k +zkn p nz
-k A-n - z k (6b)n p nz
k - (k 2 - k 2 )1/2 (7a)n p
k2 2 (7b)n n
A+ A+ - a -b b A
and a ,b, v ,a ,k, X are defined in Appendix B. Here h and v denote
5
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the horizontal and vertical polarizations, which are two characteristicA A
linear polarizations in an isotropic medium. a and b denote the
polarizations of the a-wave and the b-wave, which are two characteristic
(extraordinary) waves in a biaxially anisotropic medium. Note that the
superscripts + and - indicate the upward and downward propagating waves,
respectively. The task here is to determine the sixteen reflection and
transmission coefficients: R's, A's, B's and X's.
4. MATRIX METHOD
The unknown coefficients appearing in (2), (3) and (4) can be
evaluated by using (A4) and (AS). But this is at best a tedius procedure;
moreover, the results thus obtained are in a very complicated form. We
therefore follow an alternative method 3 in which we first express the
unknowns in terms of half-space Fresnel coefficients. Later in the next
section we evaluate the various half-space Fresnel coefficients.
In this procedure we denote the amplitude vectors of various waves as
p, q, P, Q, s (see Figure 2). These are two-element vectors whose
elements are the characteristic components of the corresponding wave. For
example
S" Pv
where ph and pv are the amplitudes of horizontally and vertically
polarized components of the p-wave in an isotropic medium. Similarly
" Pb
- - • i • m m m m l m m m m m I ,6
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where P and Pb are the a- and b- components of the P-wave in a biaxially
anisotropic medium and so on. Accordingly these amplitude vectors satisfy
the following equations
R 10121
where F01' 501' ý10' 710' ý12 and 712 are the various half-space
reflection and transmission matrices defined as follows
0• R01Rvh
Svhi (10a)01 0 RJ0
Xhb Xvb
910 _ F::: ((la)
R ab b7
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10 X ah Xbh(1bXI0 " (llb)
X av Xbv
R 1 2 exp i(kad+kau)d ] 2 exp [ i +kau)daa z zaz (1a12 R, [ exp [i(-k.d+,ku)d 12 , x, ,bd+b)u, d] (12
[ 12 exp [(ka -k )d ] 2 exp [ (kb z2)d I12 u 12 exp ad 2z ] bd 2z bud
Lav 'kz k2ý Ozdkz
Note that the exponential terms are included in (12) to take into account
the phase shift at the boundary, z - -d. For a given incident wave
corresponding to f, Equations (8) and (9) represent four equations for
four unknowns -, F, Q and '9. The solution is readily obtained and is given
as follows.
. •(13a)
8
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P - (13b)
Q -B~(13c)
I -(13d)
where
] R1 + o i 1 2 ( T - RlO '12 )I R0 1 (14a)
Rha A va 1 0 F12 ) 01 (14b)
- Ahb Awh X(1b
B12 ( T - 110 112 R01 (14c)B b B vb
- x12 ( T - R1 10 12 ) 0 1 (14d)Xhv Xv
We note that through (14) we have represented all the unknown coefficients
in the two-layer DGF's in terms of half-space Fresnel coefficients. In the
uniaxial limit, i.e. when c - c and 2- 0, our results agree with those
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3of Lee and Kong . We shall take up the task of deriving explicit
expressions for these half-space Fresnel coefficients in the next section.
5. HALF-SPACE FRESNEL COEFFICIENTS
We notice that for our two-layer problem there are three situations
to consider.
SITUATION 1
Here we have free space in the region above the interface z - 0 and
the biaxially anisotropic medium in the region below (Figure 2). A plane
wave from above is incident on the interface. Depending on the
polarization of the incident wave there are two cases to consider.
(i) h-wave incidence
For this case the electric fields in the two regions may be
formulated as follows.
E0(Y) - e + R hoe + v eO z > 0 (15a)
A_ iiia.Y A- iK b.-Er(Y) - Xha a e + Xhb b e 9 z < 0 (15b)
The associated boundary conditions are given as follows.
10
U•I ][ n•l h l ]I lIig
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z x E0(7) - zA x E( at z - 0 (16a)
A A- AzxV E0 () - zx Vx E() at z - 0 (16b)
On substituting (15) in (16) we obtain the following solutions for the
Fresnel coefficients.
01 + + b(1a
01 I xh v.+ h b (17a)
01 + - +
" -2 k h- +b- h- + 'I (17c)
Xhb-- 2 koz hb x+ - h 1 (17d)ya- xYa- }/(1d
where all the unknown quantities are defined in Appendix C.
(ii) v-wave incidence
Here the electric fields in the two regions are formulated as follows.
- AFA+ iko"FE() - v e + v e + vh(18a)
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-- b-A- ir.- A-- ic YX1(Y)- XV&a e +Xb b e , z<0 (18b)
By substituting (18) in (16), we obtain the following solutions.
Rl I- + X h+ + Xvb (19a)vv va a- v
01 + +Rv Xa Va_- + Xb vb_ (19b)
v va - vb ) + b-+yb- T +Xva -b [ (T x b IK (19c)
Xb [ Tv+x VT )y a-(T y -. )x ]a- (19d)
SITUATION 2
Here we have the biaxially anisotropic medium above the boundary z - 0
and the isotropic medium 2 below it. A plane wave from above impinges on
the interface. There are two cases to consider depending upon the type of
the incident wave
(i) a-wave incidence
12
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The electric fields E1 and E2 in the two regions are formulated as
follows.
-a -bE1(•)"a ei a + R 2a a e +R ab z > 0 (20a)
12 A- X1 .ir y 12 A-_ ic2yE2(y) - Xah h 2 + av v2 , z < 0 (20b)
Substituting (20) in (16) we obtain the following solutions.
R,12 - - $- ( , K..++ (21a)
R12 " - - (21b)
12 12 - 12- -Xah - Raava+ + RabVb+ + Va- (21c)
av _ R hi +R 1 2 hb + -(21d)X1 Ra abb + a
where
i- T + k h- T (22)
for t-(x,y], C-(a,b],(i,j]- (+,-]
All other quantities are given in Appendix C; but we have to replace
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kOz by k2z.
(i) b-wave incidence
The electric fields E and E2 in the two regions are formulated as
follows.
A-.. i•b, 12 A+ ik b-r . 1 2 A+ -iVa- + %bb e + %aa z > 0 (23a)
- 1 2 A- i,~R '-A iR-Y(7)- Xhh 2 e 2 12v 2 e 2 z < 0 (23b)
From (23) and (16) we obtain the following solutions.
12 R1%bb aa
12 12R ab Replacements
a "'b (24)
12 x12bXah baa
12 12v av
SITUATION 3
In this situation the geometry is the same as in Situation 1; the
only difference is that the wave is incident from below. Once again
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there are two cases to consider.
(M) a-wave incidence
The electric fields in the two regions are formulated as
-A+ ik -F A+ ik -YE0 (7) - X ah 0 e + Xav v 0 e , z > 0 (25a)
A i-af /ý i-aYA r -r- e + Raa e + Rab e , z < 0 (25b)
Applying the boundary conditions (16), we have the following solutions.
R -R12aa aa
Rab ab Replacement of
Superscripts (26)
Xh X 12+"ah ah
-4+
x - x12av av
Besides the above replacements, also note the following changes: is
here defined by (A2) and in other equations k2z is replaced by k 0 z.
(ii) b-wave incidence
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The electric fields in the two regions are formulated as
- ei 0"YA ik Y-Eo(Y) - Xbh + Xbv Vo e , z > 0 (27a)
.b -b -a,1 bA.+ ik-Y' A im-c*r A- ixY"e + Rbb b e + Raa e , z < 0 (27b)
From (27) and (16) we have the following solutions.
Rbb - Raa
Ra - Rab Replacements
a -1 b (28)
Xbh - Xah b -a
Xbv - Xav
It is to be noted that in the uniaxial limit, our results (17), (19),
(21), (24), (26) and (28) agree with corresponding results of Lee and
3Kong
6. NUMERICAL EXAMPLE
One quantity of interest in our results is the reflection coefficient
of the two layer medium. To illustrate its characteristics we have taken
the following example. Region 0 is free space with permittivity c0 while
16
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Region 2 has permittivity (6.0+i.006)cO. The anisotropic medium is
characterised by the following permittivities: cx - ( 2 . 8+i.001)0o , -Y
( 3 .O+i. 0 0 2 )c0, Cz - (3.2+i.003)c 0. The tilt angles are 01 - 20* and #2 -
40". The azimuthal angle of incident wave is 45". The thickness of the
layer is 1.0 m and the frequency is chosen as 10 GHz. In Figure 3a we have
plotted the reflectivities, rh - IRhhI 2 + 1Rhvj2 and rv - IRvv12 + IRvh12.
The behaviour here appears to be a familiar one. For small angles on
incidence we notice that rh -rv and there is a null (Brewster angle!) at
around 60° for rv. The anisotropic nature of the medium is not very
evident by looking at this reflectivity plot. This is perhaps the axis of
symmetry is very close to the incident plane. Next we consider the case
when #2 - 80°. Since the axis of symmetry is well away from the incident
plane the anisotropic behaviour is very apparent in Figure 3b. Just to
illustrate the contributions of like-polarised and cross-polarised
reflectivities to rv we have plotted IRvv1 2 and JRvhJ2in Figure 3c.
Perhaps in this example the cross-polarised reflectivity is rather small
compared to the like polarised reflectilvity. But the fact that there
exists cross-polarization is significant.
7. CONCLUSION
We have derived in this report the dyadic Green's function of a two
layer biaxially anisotropic medium. The formulation is based on the
solution for the unbounded case obtained in Part I. But the evaluation of
the various coefficients required the use of a matrix method which
expresses these two-layer coefficients in terms of half-space reflection
and transmission coefficients. This procedure is completed by deriving
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explicit expressions for the various half-space Fresnel reflection and
transmission coefficients. To illustrate the computational simplicity we
have provided a numerical example where we have plotted the reflectivities
versus the incident angle.
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REFERENCES
1. Mudaliar, S., "Green's Functions for an Anisotropic Medium:
Part I. Unbounded Case", Rome Laboratory Technical Report, 1993.
2. Tsang, L, Njoku, E. and Kong, J.A., "Microwave thermal emission from a
stratified medium with nonuniform temperature distribution",
J. Appl. Phys., vol.46, 5127-5133, 1975.
3. Lee, J.K. and Kong, J.A., "Dyadic Green's functions for layered
anisotropic medium", Electromagnetics, vol.3, 111-130, 1983.
19
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APPENDIX A
The DGF's satisfy the following equations
V o-,f) WpC0 00 r' T 6(y YE) (AI)
2 •
x V x G(0 R ') - 2 ; a O(Y,') - 0 (A2)
V x V x t2 0 (or') - 42 G 2 0 (Yr) - 0 (A3)
where w is the angular frequency. The boundary conditions associated
with these DGF's are given as follows:
Sx 0 0 (i,?') - x G1 0 (Y,V) at z - 0 (A4a)
A -Aat 0z x V x G0 0 (Y,i') - z x V x G10 (Y,r) at z - 0 (A4b)
A ~ -A
z x G1 0 (rr') - z x a2 0 (Y,I') at z - -d (A5a)
A -A-z x V x G1 0 (Y,Y') - z x V x G20 (Y,Y?) at z - -d (A5b)
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APPENDIX B
A+ 12 A+a - (u) -1/2 * A (Bla)
- [ -1/2 - (ia - •ya') - -A (Bib)
--- (¶ vl-1/2 -A (B2b)
tu A~-2 A+' - x • , t-aorL, (B3a)
Xd A- -2 A-X - x • " , t- a or b (B3b)
where
A a A Aa A
A+ 1 2 xa -- +A (B4a)hau a A
^Ab Ab A Ab Ab A
1 kx(kx 1) + kx(kx 2) (B4b)
+hbu ibx 1 1 Ikx 2 .21
k - k +aU , -aorb (B5)p z
h( J + -x -).-- • .... / (B6)A A.
1 k x O0 1k x o 2 1
21
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k k• (B7)
A " (± siin2 + 2 sin#1 eosi 2 A
0z cos 02 (B8)
- L (L- ) (B9a)•y (cz- c x)
[ x(c z- cy) ]1/21/2" (B9b)
2 cy (cz- c x)
For definiteness we have assumed in the above equations that c < c < tx y
Aa A Aa A
A- 1 [ c X 01 Ic x IC (BlOa)h Ic x olI lIc x 0 21
Ab Ab A Ab Ab A17 [K x(ic x 01) +~ x(X x 02) (BlOb)
-hd I Ab11 AbI A
A -pk +A id, -a orb (Bll)p zh d -h u -- d} (B12)
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APPENDIX C
jjii ii 6j17 17 - 7 C" ) / 61(cl)
x y y x
wheref f
Ij f I
Jf -h\, v II f
I' a, b I
f h - +"1 -
1V "- --
h T + vTi kOz h- T (C2)
f xwhere I-\X, Yf
6 hi v- _ i (C3)x y y x
T k k i - ki (C4)
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T k kvj jC5Tv z ~ 0 Vf CS
A -x 8 ~~ (C6)
~ ~A { -~- 1.(C7)
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z
1E0 REGION 0
z=O
REGION I
z= -d
REGION 2
Figure 1. Geometry of the Problem
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43-C
Figure 2. Amplitude Vectors of Waves in Two-Layer Medium
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Ai
*L 0
Z 4-
wi w 0
I c.
.j.w Ua
cc ,
II oo~,, 07
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:0~04.
do
Alto 0""- - C," .
* / 3 1.Ž. • .
SIm) l .0
00
@0 B
&mn
1100.
U, 4* d4
28
joe-. t
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o 04
3m. sa03ý 0d
Ca, %woo
~bow
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MISSION
OF
ROME LABORA TORY
Mission. The mission of Rome Laboratory is to advance the science andtechnologies of command, control, communications and intelligence and totransition them into systems to meet customer needs. To achieve this,Rome Lab:
a. Conducts vigorous research, development and test programs in allapplicable technologies;
b. Transitions technology to current and future systems to improveoperational capability, readiness, and supportability;
c. Provides a full range of technical support to Air Force MaterielCommand product centers and other Air Force organizations;
d. Promotes transfer of technology to the private sector;
e. Maintains leading edge technological expertise in the areas ofsurveillance, communications, command and control, intelligence, reliabilityscience, electro-magnetic technology, photonics, signal processing, andcomputational science.
The thrust areas of technical competence include: Surveillance,Communications, Command and Control, Intelligence, Signal Processing,Computer Science and Technology, Electromagnetic Technology,Photonics and Reliability Sciences.