Project Cyclops, A Design... - Department of Earth and Planetary ...
Project Cyclops, A Design... - Department of Earth and Planetary ...
Project Cyclops, A Design... - Department of Earth and Planetary ...
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where0ma x is the maximum value <strong>of</strong> 0 we can allow<br />
(see Figure 11-18) <strong>and</strong> 6ma x is the corresponding value<br />
<strong>of</strong> 6 (see Figure 11-16). We can consider using electromagnetic<br />
waves because 0ma x can be much greater than<br />
5ma x <strong>and</strong> therefore the scale factor o can be very small.<br />
Let us assume we wish to image over the tuning range<br />
from l to 3 GHz. Then kmax = 0.3 m. If we choose<br />
s = 2_.ma x = 0.6 m, then for a 1000-element array<br />
a _ 10 m. We can easily space the receiving antennas at s/2<br />
so we choose b/a = 1 in equation (66) <strong>and</strong> find £ _ 40 m.<br />
Whereas the array dimensions in acoustic imaging were<br />
very small, the dimensions involved in microwave imaging<br />
are larger than we would like, but not impractically<br />
large.<br />
A great advantage <strong>of</strong> microwave imaging over delay<br />
line or acoustic imaging is that we can vary the image<br />
size by changing £, thus allowing us to match the useful<br />
field size to the image array size as we vary the operating<br />
frequency. At 3 GHz, for example, we can use the same<br />
arrays as in the above example but increase _ to 120 m.<br />
But to realize this advantage we must be able to keep the<br />
image focused as I_is changed.<br />
One way to focus a microwave imager is with an<br />
artificial dielectric lens in front <strong>of</strong> the signal plane <strong>and</strong> a<br />
similar lens in front <strong>of</strong> the image plane to flatten the<br />
field. This allows both arrays to be plane, but requires<br />
several pairs <strong>of</strong> lenses to cover the frequency range. The<br />
cost <strong>and</strong> practicality <strong>of</strong> artificial dielectric lenses 20 m or<br />
more in diameter have not been evaluated.<br />
The use <strong>of</strong> concave arrays causes great mechanical<br />
complications since the iadii <strong>of</strong> curvature must be<br />
changed as the separation is changed. The following<br />
possibilities were explored<br />
aberrations within tolerable limits over a plane image<br />
surface.<br />
Figure 11-19 shows two plane arrays separated a<br />
distance _. The signal delay is shown symbolically as a<br />
curved surface a distance z/c behind the signal array. Let<br />
us assume this surface is a paraboloid given by<br />
"r_) c - k (1 _ _-)(X/_+a p2 2- _) (69)<br />
Then the total distance d from a point on this surface to<br />
Vi is d = (r(p)/c + r, <strong>and</strong> the change in d with respect to<br />
the axial value do measured in wavelengths is<br />
__ =__ -i--- --m +-- --<br />
X ;_ _2 as _2<br />
(70)<br />
Plots <strong>of</strong> e versus p[a are shown in Figure 11-20. We see<br />
that for all cases the spherical aberration for 0 < p/a < 1<br />
is small if k = 1, <strong>and</strong> is tolerable for the other values <strong>of</strong><br />
k.<br />
a, /,""<br />
I p ,+<br />
C<br />
I_IQ s<br />
r<br />
I<br />
Vi<br />
Case rs ri Signal Delay?<br />
SIGNAL<br />
PLANE<br />
IMAGE<br />
PLANE<br />
1 oo £/3 yes<br />
2 _ _/2 no<br />
3 _/2 oo yes<br />
The radii rs <strong>and</strong> ri are as shown in Figure 11-18. The<br />
signal delays are those needed to make the wave front<br />
for an on-axis source be spherical with its center at Vi.<br />
Although cases 1 <strong>and</strong> 3 permit one array to be plane,<br />
they require delays <strong>and</strong> the other array must be concave<br />
<strong>and</strong> adjustable.<br />
Probably the most satisfactory solution is to make<br />
both arrays plane, <strong>and</strong> obtain focusing by the use <strong>of</strong><br />
delay alone. If we accept a small amount <strong>of</strong> spherical<br />
aberration on axis (by making the radiated wavefront<br />
paraboloidal rather than spherical), we can keep the<br />
Figure 11-19. Radiative imaging with plane arrays.<br />
Now an important property <strong>of</strong> a paraboloid is that<br />
adding a constant slope everywhere merely shifts the<br />
vertex; its shape remains unchanged. Thus, an <strong>of</strong>f-axis<br />
signal, which is to be imaged at Pi, adds a delay slope<br />
that shifts the vertex <strong>of</strong> the paraboloidal radiated<br />
wavefront to Ps rather than V s. We can therefore use the<br />
curves <strong>of</strong> Figure 11-20 to estimate the <strong>of</strong>f-axis aberrations<br />
by simply noting that at Ps the abscissa #/a now<br />
is zero, at Vs the abscissa p/a is 1 <strong>and</strong> at Qs the abscissa<br />
p/a is 2.<br />
At 1 GHz <strong>and</strong> with k = 0.97 we see that, if the image<br />
plane is moved to increase £ by about 0.077_ as indicated<br />
by the dashed line, the peak error in the wavefront is<br />
149