Transcript
Sensor and Simulation Notes Note 320
7 November
Diffraction-Free
1989
Microwave Propagation
Brenclan B. Godfrey Weapons Kirtland
Laboratory
(AFSC)
AFB, New Mexico 87117
Abstract The
properties
modes limited realizable
are
of
three
reviewed.
practical antennas.
value
mathematically It or
is
shown
exhibits
diffraction-free that the
each usual
of
microwave these
diffraction
modes r:ite
prop:lg:l[it)ll either (or
is
t)t
physic:tlly
.
I. Introduction Conventional beam
in
expands
a Rayleigh
optics
predicts
theory
cross-sectional
area
Here, z is the propagation
range.
that
a
well
(Lr/z) 2
as
col!; mateci
after
microw:l\e
propagating
beyond
distance, (1)
Lr = A/~ is
the
Rayleigh
wavelength.
As
launched high
from
a
times
at the antenna
years
i.
to
not
finite aperture The on
upper
bound
suggestion limit.
by the
energy that
proves
but T.
allow
a
T.
Although are the
the
is
the
barn
(~
requires
this
radiation =
0.1
Iluxes Air
model.
m)
Achievi]l:
range.
a
fc\\
breukd{ni 11
microwave
Wu’s
times.
known
wave
microwave
energy
transport
In fact, neither his calculations
nor his experiment ---?
obtain an
at
better support
w:iic ivi[ll
on
upper This
antenna.
indefinitely
concept not
carrying with
Iinli[td
oic r
propagation
do
Section fields
Il:ive
prop:lg:ltion
missile”
duration,
literature
renliztible
to
from
missiles
three
dit’frac[ion-free
diffraction-free
“electromagnetic
rise
or
the>c
the
scientific
principal cmnot
tr-ansverse
th:lt
physically
distances
preclude
in
t!le
p:l>[
revie~vs
find
research
not
the
without
correct
beam
electromagnetic
fast
in
Huygen’s large
during
p:iper
we
are
at
subnanosecond well
This
published
authors
not
studies
propag:~tion
mathematically
density
does
exceedingly that
to
appearing
employs
Section
distances.
requiring
km
of
wave
schemes
antennas.
they
tens
Unfortunately,
and risetime
sense,
Ray!eigh
propagation.
various
III.
~
a 3 km
experimenttil
free-space
the
microwave
Section
profiles
by
diffraction
limited
and
microwave
according
and
results.
following
bound without
show
Basically,
derived
many
theoretical
substantiated
value.
fields
at
has
antenna
propagation
are
area,
a 3 GHz
antenna
diffraction-free
e.,
antenna
the limiting factor in some applications.
exciting
practical
the
several
diffraction-free
usual
densities
purport
potentially
in
power
becomes
spreading,
either
radius
at
the
example,
10 m
greater
However, six
is
a numerical
microwave
hundred
A
range,
IV
is
difl’r;lct little
treats
J.
this
the
in
energy
Bessel-fllnctit)n than
an:~lyztd (Ilc and
Durnin’s radi:ll diffraction
,. 8 >, f,, ,; 1
I~~
J
.
m
The
conclusion. W.
Ziolkowski
central in
for
in
that
does
great
launching
these
waves
literature
V.
not
over
wave
to
of
While
diffract,
J.
a
most
lead
us;
Brittingham
focused-wave its
energy
concluding
references
in
is
finite
transport text
no
are
R.
has
:1
contained antennas
better
bibliography
the
and
mode
ent=rgy
Moreover,
to
The
N.
of
distances.
patterns.
known
modes”
Section
extend
conventional
relevant
“focused-wave
treated
packet
that
proposed for
are
wave
wings
intriguing
than
lists
by
first
al]
tiuthor
and date of publication. This The
paper
scalar
solutions
free-space
throughout
can
be
the
the
vector
antenna
size.
scalar
fields,
field if
Scalar
with
thought fields
electromagnetic
Additionally, of
deals
of can
pattern
characteristic waves
also
as be
Hertz a
are
of
[A.
good
wavelengths
than
vector
potentials,
derived
itself
is
rather
scalar
from
which
Sezginer,
1985].
approximation
are
short
compared
in
their
own
in
terms
interest
fields.
to
that
to
right,
the
e.
:.,
as acoustic waves in water.
II. Estimates Fields principle
generated
[Ziolkowski,
by
an
1989a],
of Microwave
antenna an
can
Diffraction
be
expressed
approximation
to
the
(2)
is
evaluated
and
located
scalar
of
Huyge II’s
wave
equu(io[l
at
positions
Green’s theorem.
R2 = (X - X’)2 + (y - y’)2 + The
wave
function
(x’,y’,z’) on the antenna
Then,
f
in
the
(Z - Z’)2
right
side
of
surface and at retarded
Let
the
antema
near
the
z-axis
be and
oriented far
from
time t - R/c.
along the
Eq.
the
antenna,
z-axis the
field
ctin be
near
z’
=
approximated
as (3)
().
From this follows an upper bound on the magnitude -. If(x,y,z,t) I ~
is evident
It z ‘2)
&
or
faster
at an
finite
(4)
that
must
The
fdl
off
is
impossible
does
to
rule
field
as
distances
infinity
bound,
distances.
f
large
to
upper
(4)
~..
sufficiently
Eq. over
I
%
Eq.
propagation
being
-$
from
Diffraction-free (4),
g
I
of&
pattern
z- * (and
from [Wu,
out
the
a
as
antenna.
1985 b].
I ioweve r,
diffraction-free
from
power
propagation
focusing
antenna
cun
increase with z over a limited range, for instance. The field
at
Rayleigh the
range
antenna
can
also
to
be
a
be
obtained
plane
from f
wave,
Eq.
=
(3).
Specify
foexp[i(kz
-
~t)]
the with
o/c = k. Then, in the far field region f(x,y,z,t) = f. uA/27rcz
With
the
(5)
substitution
=
u
becomes A/~, as desired.
Alternative,
211c/A,
the
more rigorous derivations
III. The Electromagnetic About frequency ‘? z -- 6 fi~r Zb-t Wu
from
the
the his
T. T.
antenna
wave easily
variation
implies
microwave
pulse
times,
and
by with
a
t~-%
the
simple
arguments
a
finite
rate
at
exceeding
the
frequency one-half
w:lve
of
A
-4-
leading
high
at
to
destroys Rayleigh
in
<
t
This
~.
w-%-’
integrand
O
the Eq. (4)
the
slow
range,
:IS
<
1.
can
be
result
is
frequency head
(3)
Eq.
:Ls
v:lries
Diffr:iction
of
~vi[ll
energy
:tml)litl]de
missile.” choice
the
in
19S9];
variation
temporal
wa~’e p:ickets
decay
[Shen,
(4).
Thus,
at
The
appropriate Eq.
wA/2Tc
exist.
transient o
“electromagnetic
1987].
distribution
that
large z-l
[Lee,
the
distances
as
the the
showed
1985a].
length
length
Missile Concept
for
[Wu,
packet
slow
Wu
W-%-’
pulse
arbitrarily
reconciled
early
ago
dependence
9 and dubbed
made
five years
scule
is
f:lil.
of sin:ular
[it
Truncating
spati:~] defined
the
fall-off in
terms
M
●
of the cutoff frequency
[Wu, 1989 b],
—
The
essence
by a simple
of
example,
the
electromagnetic
missile
considered
in the
domain.
a current pulse I(t) produces f(o,(),z,t) = I(t where
now
step
●
R2
function
=
AZ =R
-z.
steadily,
Az
does
not
diffract,
the
packet
for
more
tail
the
of
a2/2z.
Thus,
general [Lee,
whereupon
wave
Shen,
a
fast
radius
parabolic
about
4
ft.
the
width
at
49
ft. was
antenna
driven
by
z
out
radius is
shows
very
a
way
propagation to
a
front
that
~
less
than
be
the
pulse
energy
axis,
occur the
width
similar
the
a
decreasing
rota]
A
losses
of
of
the
from
Qualitatively,
AZ becomes
to
distance.
distance
wave
width
For
1%%].
square
the
the
such
a
[Shen,
picture has
only
pulse
in
been in
the
rise
time,
eats into the head as well. is
analysis rising
consistent
with
electromagnetic and
energy
found
to be
an
experiment
pulse
measured
transmitted
at
distances
decreased
about
wtis
very
50 psec,
[Shen,
launched
of
up
nearly
also
to as
from
1988]
in
a
f[.
2
Beyond 49 ft. -1 The pulse z .
in approximate
:lgreement
predictions. though
the
energy
instead
of
the
z ‘2
electromagnetic
missiles
of
long
over
do
not
would
decay
of an
decay
antenna
seem
be only
length
results
for a 10 m radius
at
km.
Moreover,
producing
electromagnetic
in
ordinary
practical
For
distances.
100 m radius 0.1
%), f
in
1989].
Even
energy
=
although with
until
antenna
with theoretical
antenna
large
and
valid
packet
simple
very
does
the 6
for
inversely
1987;
which
Z-l
tail
pulses,
diffraction
This
to.
R
the
illustrated
(6)
~ being
(analagous
decreases
derived
a2,
Expanding =
A disk
well
I(t - R/c)
-
+
pulse
is
the on-axis field,
Z/C)
Z2
time
concept
instance, 16 psec
antenna such
at
long
-5-
at
is of
diffracting transmitting
a wave
packet 1000 km.
requires
phasing
order
pulses, large
launched The the
amounts from
same
10 km or for a 1 m radius
a pulse
an accuracy of 16 psec or better.
for
missile
u
pulse
antenn:l
antenna
(o
n.
*
IV. The Bessel-Function Profile Beam Concept One exact solution
to the scalar wave equation
is
f = fO JO(~r) exp[i(kz - ~t)] k2
with
u 22= /c
zero.
The
2.4/K
surrounded
T/&.
Although
(~r)-%,
each
central
peak.
radial
+
~2.
pattern
Jo
of
by
is
Eq.
the
(7)
ring
Bessel
consists
concentric
the
ring
(7)
of
rings
about
the
same
of
central
peak
by
amount
of
corresponding
to
order
of
rtidius
approximately with
decrease
solutions
Nonaxisymmetric
a
spaced
amplitudes
contains
function
radius
energy
Eq.
as
as
(7)
the
:lIso
exist
but are of less interest. J. 1987a] to
Durnin
can
(7)
naaO/1.2~ Durnin
also to
this
This Durnin’s
waves
antenna,
Eq.
Rayleigh
range to
profile in
terms
is,
(l).
Doing by
obtain of
and
These =
J
profile
provided
waves
2mc/ti of
before
packets
propagate is
a
distance is
the
:10 .. :lnd
(o
1;
wavelength.
half-radius
profile
>>
:1~
the
beginning
simil:lr
tca/x
Here,
waves
Bessel-function
a
so
factor
course,
the
Eq.
is seen
however,
instead,
should,
Of
beam
wave
[Durnin,
found
011
diffr:lct.
beams
have
remtirkably
properties.
comparison
frequency.
bounded
antennas
face.
na02/J
that
comput:ltionaliy
significantly.
Gaussian only
that
finite
antenna peak,
concluded
good diffraction
used
central
generated he
from
diffracting
propagate
basis
the
demonstrated
1987b]
[Durnin,
across
the
of
have
generated
before
radius them
be
rings
many
i. e.,
coworkers
experimentally
and
Eq.
and
(l), to
be
diffraction-free
efficient in terms of antenna
be shows
of the a
to
that
waves
these
for require
ratio little
range
the
compared
2/~a
waves
The
misleading.
a
specified less
being
more per
area.
-6-
Rayleigh
less
antenn:l
2/nKa. than invested
than
size the
The the
length range
prop:uyte
energy
efficient energy
diffraction
of
of
the
th:ln
the
:lnd pl:lne
wat’e wa\cs
Bessel-function pl:lne
but
is
wwe much
beum less
It
has
been
by a finite-sized
pointed
antenna,
out
the
Bessel-function
profile
can be viewed as a line focus [DeBeer,
beam,
as
produced
1987].
V. The Focused-Wave Mode Concept Research Brittingham’s
on
diffraction-free
discovery of the focused-wave
f = fO exp[-ks]/[zO s = r2/[z0 It
propagates
at
from
peak
zo/k%,
complex
is
its
However, can
yield
Q in
central and
a
Nonaxisymmetric
Eq.
the
positive
at
length
difficulty:
waves
(8)
z
=
in
The
g
direction
ct.
Z
real
corresponding
has
a
serious
as
with
ordinary
a
finite
energy
The
is
width
in
is
Eq.
taken
(8)
PJIIs
off
in
of
the
centr:il
That
f
I
approximately
part to
and
20. as
also
the
are
physical
known
al] is
wave.
[Bela nger,
shortcoming,
plane
waves,
wave
infinite
a superposition
packet
[Ziolkowski,
energy of
1985].
[WU,
1984].
focused-wave One
modes
such
solution
1989a]
constant
focused-wave
~ mode
+ i(z - ct)][ks + b]
sets is
the largely
Another energy
difficulty components
[Heyman,
negative
component
lurge.
(The
validity
with
cut
in Eq. of
(9) this
off.
radius
at
also
sets
It
R.
in
modes
both
W.
can be claim
which the
the
tail
maximum
of
the
propag:l[ion
z = b/2k.
focused-wave
flowing
1987a].
(9)
spherical
distance for which there is no dispersion,
directions
1983] (8)
peak
the
f = f. exp[-ks]/[zo
with
by
1985].
is [Ziolkowski,
The
mode, [Brittingham,
triggered
+ i(z - et)]
speed
not
1984; Sezginer,
was
+ i(z - et)] - i(z + et)
directions is
propagation
the
is -7-
to
the
they and
argues,
exponentially
unclear
that
positive
Ziolkowski made
is
are
negative
however,
small author.)
acaus:ll, that
by choosing [n
any
axi:ll the k/1~ cast,
3
the
causality
launched
is
issue
subsidiary
from a realizable
Ziolkowski
numerically
used.
an
antenna
radius
the
central
pulse
Rayleigh
range
calculations
of was a
zfj
=
a
=
the
focused-wave
m,
found
the
mode
k
Eq.
also
=
can
(2)
to
Z.
that
is
0.1
103
the
m,
psec.
essentially
all
less
With
thun
radius only
the
b
distance
antenna
distance
and of the
in
his
linearly
energy
in
the
examples was in the pulse wings. focused-wave
performed
as
well
used
had
an
effective
the
Rayleigh
cm before
range showing
did
Ziolkowski
less
mode
[Ziolkowski, area
was
of
evidence well,
but
propagation
1989c].
In
36
and
cm2,
The
180 cm.
is preparing
experiments
1.5
this
case
the
Z.
was
about
focused-wave
cm with
mode
radius a
was
shorter
in
water
rect:tngu]ar 0.2
wave not
I{enct,
roughly
I ()()
from
tl~c
launched necessarily
Rayleigh
range
were untenn:t
cm.
propagated
A Gaussian
of diffraction. its
experiments
optimol.
in
order
to
put his models to a more incisive test.
VI. Acknowledgments
The and
H.
author
Zucker
and J. O’Laughlin
is indebted for
9
be
from
m-l,
propagation
be
Increasing
generation
1.6710-4
to
diffraction-free
Note
mode
diffraction-free
five.
the
m,
corresponding
from of
focused-wave
1.6710-5
scale
0.5
factor
1989a].
Acoustic
antenna
investigated
time
increased
[Ziolkowski, numerical
The
by
whether
antenna.
Parameters
disk antennas. = 101O were
to
to C. Baum,
informative
provided
background
discussions. material.
-8-
A.
Biggs, W.
H.
Baker
Brandt,
R. Ziolkowski,
suggested
this
study,
7) /1j .’Jh
i’; ,?, u
9
VII. Bibliography P.
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A.
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M.
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●
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e
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M. Lee,
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P. Hillion, “Spinor Focus Wave Modes,” J. Math. Phys. ~,
D.
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of Mellin
Trtinsforma(it]il
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“Evidence
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Energy Tech. Rev. (Nov., 1988), p. 24. H. E. Moses,
“The
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Time-Dependent
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in
the
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and Math.
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Prescribed
and
R.
T.
Time-Dependent
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Part
I:
The
Expanding
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“Initial
Presser,
Acoustic Inverse
Waves,
Conditions,
and
Initial
and
Sources,
and
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for
Three
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Antennm
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E.
Moses
Microwave
~
and
R.
Particle
T. Beam
“Acoustic
Presser, Sources
~
and
Directed
Electromagnetic Energy
Concellts,
Bulle Is,” SPIE
Vol.
1061, p. 403 (1989).
J.
M.
Myers,
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