ABSTRACT

Remember that for spaceborne SAR, the maximum range is limited by the earth curvature [6,7], depending on the satellite height and elevation angle. If the transmitted signal is of the form given by Equation 1.54, the received signal as a function of fast time is the output of the matched filter:

s A s A t s t dt

A p

( ) ( ) ( ) ( )τ τ τ= ⊗ = −

=

τ pi τ pi τ−  

  −

 

  + −

 

 

2 2

2 2 2

R

c f

R

c a

R

cc r cos 



(3.3)

where A0 is the scatter amplitude [4] and, without loss of generality, is assumed constant. Equation 3.3 is indeed also dependent on the slow time because the slant range R is varying with the sensor position within the target exposure time. Referring to Figure 1.6, the slow time-dependent slant range can be expanded about R(ηc), with the beam center crossing time, ηc:

R R u

R

u

( ) ( ) ( )

( ) cos

( ) (,η η η

η η η θ

η η= + − + −

ηc )2 +… (3.4)

where θc is look angle to the scene center and

η θ η θc c c c R

u

R

u = =

0 tan ( )sin . (3.5)

Due to the time variation of the range, a point target response will continuously appear along the path according to Equation 3.4 within the synthetic aperture length. A coherent sum of these responses during the course of the target exposure time will be out of focus if no range-induced phase variation is corrected. Figure 3.2

schematically illustrates data collection and mapping from the target (object) to the SAR data domain.