Paraboloidal Reflectors
Antennas useful for radio astronomy at
short wavelengths must have
collecting areas much larger than the collecting area $\lambda^2 / (4
\pi)$ of an isotropic antenna and much higher angular resolution than a
short dipole provides. Since even rather large arrays of dipoles are
inadequate at wavelengths $\lambda < 1$ m or so, most radio
telescopes use large reflectors
to collect and focus
power onto simple feed
antennas such as waveguide horns or dipoles
backed by
small reflectors that are connected to receivers. The most common
reflector
shape is a paraboloid of revolution because it can focus a the plane
wave from a distant point source
onto a single focal
point.
The reflector shape that can focus plane waves onto a single point must preserve the phases of all waves reaching the focal point. Thus the total path lengths traversed by all portions of the reflected wave must be the same, and this requirement determines the shape of the desired reflecting surface. Clearly the surface must be rotationally symmetric about its axis. In any plane containing the axis, the surface looks like:

A plane containing the axis of a
paraboloidal
reflector with focal length $f$.
The requirement of constant path
length can be written by equating
the on-axis path length $(f + h)$ with the off-axis path length:
$$(f +
h) = \sqrt{(r^2 + (f - z)^2} +(h - z)~.$$
We need to extract the
reflector height $z$ as a function of radius $r$:
$$ \sqrt{r^2 + (f
-z)^2} +h - z = f + h$$ $$ r^2 + f^2 + z^2 - 2fz = f^2 + z^2 + 2fz $$
The result is
$$\bbox[border:3px blue solid,7pt]{z = {r^2 \over 4 f}}\rlap{\quad \rm
{(3B1)}}$$
This is the equation of a paraboloid with
focal
length $f$. If the reflector is truncated at some radius
$r_0$, the ratio of the focal length $f$ to the diameter $D = 2r_0$ is
called the $f/D$
ratio or focal
ratio. In principle it
is a free parameter for the telescope designer. In practice it is
constrained. If $f/D$ is too high, the support structure needed
to hold the feed or subreflector at the focus becomes unwieldy.
Thus most large radio telescopes have $f/D \approx 0.4$, an unusually
low focal ratio by optical standards. The drawback of a low $f/D$
is a small field of view. The focal
ellipsoid is the volume around the exact focal point that
remains in reasonably good focus. Only a small number (e.g.,
seven) feeds can fit inside the focal ellipsoid of an $f/D \approx 0.4$
paraboloid. Large arrays of feeds or imaging cameras require
larger $f/D$ ratios, obtained either by flattening the paraboloid or by
using magnifying subreflectors.
Consequently, most radio telescope
reflectors are circular
paraboloids or sections thereof. Their advantages are:
The Far-field Distance
How far away must a point source
be for the received waves to
satisfy our assumption that they are nearly planar? The answer depends
on both the wavelength $\lambda$ and the reflector diameter $D$.
Consider the spherical wave emitted by a point source a distance $R$
from the reflector:
The spherical wave emitted by a point
source at distance $R$ deviates from a plane by $\Delta$ at the edge of
an aperture whose size is $D$.
The maximum departure $\Delta$ from a
plane wave occurs at the edge
of the reflector. Conventionally, we define the
far-field distance
$R_{\rm ff}$ by requiring that $\Delta < \lambda /2$. Using
the
Pythagorean theorem, at the aperture edge
$$R^2 = (R - \Delta)^2 + \biggl({D
\over 2}\biggr)^2~,$$
and substituting $\Delta = \lambda / 2$ at $R = R_{\rm
ff}$ gives
$$R_{\rm ff}^2 = R_{\rm ff}^2 - R_{\rm ff} \lambda +
{\lambda^2 \over 4} + {D^2 \over 4}$$
$$R_{\rm ff} = {\lambda \over 4}
+ {D^2 \over 4 \lambda}$$
If $D \gg \lambda$, then $\lambda/4 \ll
D^2/(4 \lambda)$ and
$$\bbox[border:3px blue solid,7pt]{R_{\rm ff} \approx {D^2 \over 4
\lambda}}\rlap{\quad \rm {(3B2)}}$$
Unless $R \gg R_{\rm ff}$, the path-length errors will introduce
significant phase errors in the waves coming from the off-axis portions
of the
reflector, reducing the effective collecting area and degrading the
antenna pattern.
Example: What is the far-field distance of the Green Bank Telescope ($D = 100$ m) observing at $\lambda = 1$ cm?
$$R_{\rm ff} = {(100\,{\rm m})^2 \over
4 \times 1\,{\rm cm}} =
{10^4\,{\rm m}^2 \over 0.04\,{\rm m}} = 2.5 \times 10^5\,{\rm m} =
250\,{\rm km}$$
Such a large far-field distance makes ground-based measurements of the GBT antenna pattern impractical. To measure the shape of the GBT reflector surface using radio holography, we can observe a geostationary satellite having an orbital height $R \gg 250$ km. Similarly, to determine the transmitting power pattern for a large radar antenna such as the $D = 305$ m Arecibo reflector, we can passively observe a celestial point source in the far field and use the reciprocity theorem to equate the transmitting and receiving patterns.
Patterns of Aperture Antennas
In optics, the term aperture
refers to the opening
through which
all rays pass. For example, the aperture of a paraboloidal reflector
antenna would be the plane circle, normal to the rays from a distant
point source, that just covers the paraboloid. The phase of the plane
wave from a distant point source would be constant across the aperture
plane when the aperture is perpendicular to the line-of-sight.

Another example of an aperture is the
mouth of a
waveguide horn antenna.

How can we calculate the beam
pattern, or power gain as a
function of
direction, of an aperture antenna? For simplicity, we first consider a
one-dimensional aperture of width $D$ and calculate the electric
field
pattern
at a distant ($R \gg R_{\rm ff}$) point.

Treating this as a transmitting
antenna, we imagine that the feed
illuminates the aperture with a sine wave of fixed frequency $\nu =
\omega /
(2 \pi)$ and electric field strength $g(x)$ that varies across the
aperture. The
illumination induces currents in the reflector. The current densities
$J$ will vary with both position and time:
$$J \propto g(x)
\exp(-i\omega t)~.$$
We don't need to worry about the constant of
proportionality yet; it can be calculated later from energy
conservation. Although we are interested only in electromagnetic
radiation, we use
Huygen's principle
that applies to waves of
any type (sound waves for example). It asserts that the aperture can be
treated as a collection of small elements which act individually as
small antennas.
The electric field produced by the whole aperture at large distances is
just the vector sum of the elemental electric fields from these small
antennas. The field from
each element extending from $x$ to $x + dx$ is:
$$df \propto g(x)
{\exp(-i2\pi r / \lambda) \over r} dx~.$$
At large distances compared
with the aperture size ($r \gg D$) we can make the
Fraunhofer
approximation
$$r \approx R
+ x \sin\theta = R + x l~,$$
where
$$\bbox[border:3px blue solid,7pt]{l \equiv \sin\theta}\rlap{\quad \rm
{(3B3)}}$$
At large
distances, the quantity
$$ {1 \over r} \approx {1 \over R}$$
varies slowly with
distance, but the periodic term cannot be ignored at any distance:
$$df
\propto g(x) \exp(-i 2 \pi R / \lambda) \exp( -i 2 \pi x l / \lambda) d
x$$ Note that $\exp(-i 2 \pi R / \lambda)$ is a constant since $R$ is
fixed, so this factor can be absorbed by the constant of
proportionality. If we define
$$\bbox[border:3px blue solid,7pt]{u \equiv {x \over
\lambda}}\rlap{\quad \rm {(3B4)}}$$
to express position along the aperture in
units of wavelength, then
$$\bbox[border:3px blue solid,7pt]{f(l) = \int_{\rm aperture} g(u)
e^{-i 2 \pi l u} du}\rlap{\quad \rm {(3B5)}}$$
In words, this very important equation says:
See
Appendix B of Rohlfs & Wilson for a review of Fourier transforms.
Example: What is the electric-field
pattern
of a uniformly illuminated
one-dimensional aperture of width $D$ at wavelength $\lambda$? Uniform
illumination means that the strength of the illumination is
independent of position across
the aperture:
$$g(u) = {\rm ~constant}, \qquad {-D \over 2
\lambda} < u < {+D \over 2 \lambda}$$
We will solve this problem in two
steps, first finding the far-field pattern of
a unit aperture ($D = \lambda$) and then using the similarity
theorem (below) for Fourier transforms to scale the first result to our
particular aperture.
First we calculate the Fourier
transform of the unit
rectangle
function:
$$ \Pi (u) \equiv 1\,, \qquad -1/2 < u < +1/2~,$$
$$
\Pi (u) \equiv 0 {\rm ~otherwise}\qquad\qquad\qquad$$
Notice that the function
symbol (upper-case pi) is similar in shape to the function graph,
making it easy to
remember. [Beware: Rohlfs &
Wilson appendix B mislabels $\Pi(u)$ as II$(u)$, an entirely different
function.]

The Fourier transform of $\Pi(u)$ is
defined as
$$F(l) =
\int_{-\infty}^{\infty} \Pi(u) e^{-i 2 \pi l u} du$$
Thus $$F(l) =
\int_{-1/2}^{+1/2} e^{-i 2 \pi l u} du$$
$$F(l) = {e^{-i 2 \pi l u} \over -i 2 \pi l u}\vert_{-1/2}^{+1/2} =
{e^{-i \pi l} - e^{- i \pi l} \over -i 2 \pi l}$$
Recall the mathematical identities
$$e^{i \pi l} = \cos(\pi l) + i
\sin(\pi l)$$
$$e^{- i \pi l} = \cos(\pi l) - i \sin(\pi l)$$
so
$$e^{i
\pi l} - e^{-i \pi l} = 2 i \sin(\pi l)~.$$
Substituting into the
equation for $F(l)$ gives
$$F(l) = {-2 i \sin(\pi l) \over -2 i \pi l}
= {\sin(\pi l) \over (\pi l)} \equiv {\rm sinc}(l)$$
The useful sinc
function defined above looks like this:

Next we use the powerful similarity theorem (proof) for Fourier transforms:
If $f(l)$ is the
Fourier transform of $g(u)$, then
$${ 1 \over
\vert a \vert} f\biggl({l \over a}\biggr)$$
is the Fourier transform of
$g(au)$, where $a \neq 0$ is a constant.
In words, the similarity theorem states that making a function $g$ wider or narrower makes its Fourier transform $f$ narrower and taller or wider and shorter, respectively, always conserving the area under the transform. For our application, it implies that the beamwidth of an aperture antenna is inversely proportional to the aperture size in wavelengths.
Thus for our uniformly illuminated
one-dimensional aperture of width
$D$ operating at wavelength $\lambda$, the electric field pattern is
$$f(l) \propto \int_{u = -D/(2\lambda)}^{+D/(2\lambda)} e^{-i 2 \pi l
u} d u$$
$$f(l) \propto {\sin(\pi l D / \lambda) \over (\pi l D /
\lambda)} \propto {\rm sinc}(l D / \lambda)$$
For a large ($D/\lambda \gg 1$) aperture, the relevant angles $\theta$ are small ($\theta \ll 1$ radian) so $l = \sin\theta \approx \theta$, the angular offset from the center of the main beam.
Since the radiated power per unit area
is proportional to the square
of the electric field strength, the power pattern
$P(l)$ is
$$P(l) \propto {\rm sinc}^2 \biggl( {l D \over \lambda} \biggr)$$
and
if $\theta \ll 1$ radian,
$$\bbox[border:3px blue solid,7pt]{P(\theta) \propto {\rm sinc}^2
\biggl(
{\theta D \over \lambda} \biggr)}\rlap{\quad \rm {(3B6)}}$$

What is the angular width of the main
beam? Radio astronomers
conventionally specify the angle between the half-power points, calling
it the half-power
beamwidth
(HPBW) or the full
width between
half-maximum points (FWHM). For
our example of a one-dimensional
uniformly illuminated aperture, the beamwidth $\theta_{\rm HPBW}$
satisfies
$$P(\theta_{\rm HPBW} / 2) = {1 \over 2} = {\rm sinc}^2
\biggl( { \theta_{\rm HPBW} D \over 2 \lambda} \biggr)$$
$$ 0.443
\approx {\theta_{\rm HPBW} D \over 2 \lambda}$$
$$\bbox[border:3px blue solid,7pt]{\theta_{\rm HPBW}
\approx 0.89 {\lambda \over D}}\rlap{\quad \rm {(3B7)}}$$
The similarity theorem implies the
general scaling relation
$$\theta_{\rm HPBW} \propto {\lambda \over
D}~.$$
The constant of proportionality varies slightly with the
illumination taper.
The weak reciprocity theorem says that this analysis of the transmitting power pattern also yields the receiving power pattern, or the variation of $A_{\rm e}$ with orientation, of an aperture antenna. In receiving terms, the power pattern represents the point-source response. For a uniformly illuminated aperture, scanning a radio telescope beam across a point source will cause the antenna temperature to vary as sinc$^2$, and the half-power response width will equal the transmitting HPBW. The receiving HPBW is sometimes called the resolving power of a telescope because two equal point sources separated by the HPBW can just be resolved by the Rayleigh criterion that the peak response to one source coincides with the first minimum response to the other, so the total response has a slight minimum midway between the point sources.