I. Introduction
Since its inception, synthetic aperture radar (SAR) has proven to be a reliable technology for spaceborne remote sensing of high-resolution global imaging under all weather conditions, day and night. A SAR system consists of a side-looking radar mounted on a moving platform, which forms an equivalent synthetic aperture via motion [1]. To obtain an image of a given region of interest (ROI), the SAR system measures the ROI with pulses transmitted at a set of azimuth sampling positions. The bandwidth of the transmitted pulses dictates the range resolution of the system [2], given by \begin{equation*} \delta _{r}\approx \frac {c}{2B}\tag{1}\end{equation*}
where denotes the speed of light. The azimuth resolution is likewise determined by the Doppler bandwidth, which is proportional to the observation integration angle in the azimuth direction, and the relationship between and can be given by
\begin{equation*} \delta _{a}\approx \frac {\lambda }{4\sin \frac {\bigtriangleup \theta }{2}}\tag{2}\end{equation*}
where is the wavelength of the carrier frequency. And the synthetic aperture length is expressed as
\begin{equation*} L\approx \frac {R_{0}\lambda }{2\delta _{a}}\tag{3}\end{equation*}
where is the reference slant range. Note that the integration angle is related to the equivalent synthetic aperture length given the nominal range from radar to target and the nominal azimuth incident angle.