01.09.2014 Views

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 ...

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

azimuth _) has a delay (2a/c)sin 0 greater than the far<br />

point (at azimuth _b+ 7r). For radiation arriving at zero<br />

elevation (0 = n/2). The delay difference is 2a/c, the<br />

propagation time across the array (Fig. 10-10). The delay<br />

plane is the tilted ellipse, <strong>and</strong> the delay for an element at<br />

A is ra = z_ + 2a/c while that tbr an element at B is<br />

T b = T_.<br />

= rmi n -7"0 = _'_ + 7"2<br />

a<br />

r<br />

= (r_ + _) (1 - _-) (15)<br />

<strong>and</strong> a variable part having a delay range<br />

T<br />

A<br />

2O<br />

rl+-- C-<br />

2r<br />

_'v = _'max - rmin = (16)<br />

¢<br />

vl<br />

For an array 10 km in diameter, ale = 16.67/asec <strong>and</strong><br />

r_ _ 20 /asec. Thus, the fixed delay needed for the<br />

center element is 36.67 /.tsec <strong>and</strong> the variable delay<br />

needed for an element at the rim is 33.3/asec. The total<br />

delay (rl + _'2 + rv) needed for any IF line is thus about<br />

37 #sec <strong>and</strong> must be accurate to -+1/8 nsec, an accuracy<br />

<strong>of</strong> about 3.4 parts per million. Clearly the delay system<br />

is going to require stabilization <strong>of</strong> some sort to achieve<br />

this accuracy.<br />

SIGNAL<br />

The average value <strong>of</strong> zf is one third the sum <strong>of</strong> the<br />

altitudes <strong>of</strong> the lower two cones:<br />

1<br />

rf =-_ (r_ +-_-ac) (17)<br />

while the average value <strong>of</strong> r v is<br />

Figure 10-10. IF delay requirements.<br />

2 2a 4a<br />

7u = 7" c - 3c (18)<br />

As 4_ is varied from 0 to 2rr, the tilted delay plane<br />

rotates around the central axis <strong>and</strong> is always tangent to<br />

two cones having their common vertex at P. If we<br />

arrange to pivot the delay plane at P, then for greater<br />

elevation angles it will always lie between these two<br />

cones. The required delay for any element is never<br />

greater than that defined by the upper cone <strong>and</strong> never<br />

less than that defined by the lower cone <strong>of</strong> the pair. For<br />

an antenna element at azimuth a <strong>and</strong> radius r from the<br />

center<br />

<strong>of</strong> the array<br />

The total amount <strong>of</strong> delay required for n antennas<br />

therefore is<br />

n 5a<br />

T = ff (r£ + "c-') (19)<br />

Taking r£ = a/c gives the minimum possible total delay<br />

for a fully steerable array<br />

r = 7"_+ a + r sin 0 cos(_ - a)<br />

e e<br />

a-r<br />

e<br />

Thus the delay compensation can conveniently consist<br />

<strong>of</strong> two parts-a<br />

fixed part<br />

a+t<br />

c<br />

_a3)<br />

2a<br />

T = n -- (20)<br />

e<br />

If the delay is obtained with additional transmission<br />

line the total length needed is vT, where v is the velocity<br />

(14) <strong>of</strong> propagation. Thus Lmi n = 2ha(v/c). Since the total<br />

length <strong>of</strong> line used in the IF transmission system is about<br />

(2/3) na (<strong>and</strong> 2/3 < vie < 1), we see that about two to<br />

three times as much line would be needed for the delay<br />

115

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!