Graphics Programs Reference
In-Depth Information
tive system of coordinates is denoted as . The vector defines the radar
location at time . The transmitting antenna consists of a linear real array
operating in the sequential mode. The real array is of size
O
OM
t c
N
, element spacing
d
, and the radiators are circular dishes of diameter
Dd
=
. Assuming that the
aircraft scans
M
NM
transmitting locations along the flight path, then a rectangular
array of size
×
is synthesized, as illustrated in Fig. 12.15.
Z
#N
D ob
t c
M
ρ t ()
β
#1
swath
h
v
O
X
(
000
,,
)
qt ()
footprint
Y
Figure 12.14. Geometry for DFTSQM imaging system.
Z
swath
v
X
Y
Figure 12.15. Synthesized 2-D array.
 
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