Graphics Programs Reference
In-Depth Information
For an X-band radar, choose
f o
=
9 GHz
, then
3 0 8
×
9 0 9
λ
=
-----------------
=
0 . 0 3 3 3 m
(8.90)
×
2.25 m 2
Assume an aperture size
A e
=
; thus
A e
λ 2
4
×
0.0333
π 2.25
×
G
=
------------
=
-----------------------------
=
25451.991
G
=
44 dB
(8.91)
) 2
(
Assume square aperture. It follows that the aperture 3-dB beamwidth is cal-
culated from
π 180 2
θ 3 db
×
25451.991
4
×
G
=
----------
θ 3 dB
=
-------------------------------------
=
. °
(8.92)
2
π 2
×
The number of beams required to fill the search volume is
n b
=
k p
-----------------------------------
n b
=
399.5
choose n b
=
400
(8.93)
) 2
(
1.3
57.296
k p
=
1.5
Note that the packing factor is used to allow for beam overlap in order to
avoid gaps in the beam coverage. The search scan rate is 2 seconds. Thus, the
minimum PRF should correspond to 200 beams per second (i.e., ).
This PRF will allow the radar to visit each beam position only once during a
complete scan.
k p
f r
=
200 Hz
It was determined in Chapter 2 that 4-pulse non-coherent integration along
with a cumulative detection scheme are required to achieve the desired proba-
bility of detection. It was also determined that the single pulse energy for the
missile and aircraft cases are respectively given by (see page 118)
E m
=
0.1147 Joules
(8.94)
E a
=
0.1029 Joules
(8.95)
However, these values were derived using and . The
new wavelength is and the new gain is . Thus,
the missile and aircraft single pulse energy, assuming the same single pulse
SNR as derived in Chapter 2 (i.e.,
λ
=
0.1 m
G
=
2827.4
λ
=
0.0333 m
G
=
25451.99
SNR
=
4 dB
) are
0.1 2
2827.4 2
×
0.0333 2
E m
=
0.1147
×
------------------------------------------
=
0.012765 Joules
(8.96)
25452 2
×
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