## 1.

## Introduction

Bistatic forward-looking synthetic aperture radar (BFSAR) has two platforms installed with a transmitter and receiver, respectively. Despite the separation of the two platforms, the BFSAR can still achieve a high azimuth resolution if a forward-looking geometry is used. Forward-looking imaging is highly desirable in some applications, but it has been a blind sector for monostatic synthetic aperture radar (SAR)^{1}2.^{–}^{3} for a long time. Therefore, BFSAR has recently received considerable attention.

The peculiarity and feasibility of BFSAR was studied in detail.^{4}5.^{–}^{6} Through the exploration of the limitation and potential of BFSAR, the best forward-looking geometry was proposed for achieving a high-resolution image. Moreover, some BFSAR experiments were carried out and the exciting imaging results were obtained.^{7}8.9.^{–}^{10} However, we can find that the imaging algorithms used in these experiments are mostly backprojection algorithms (time-domain algorithms). The time-domain algorithm can work well in arbitrary flight trajectories and no approximation is taken. However, it has a high computational cost and is not available for real-time imaging applications. Therefore, it is urgent to develop new frequency-domain imaging algorithms. Some theories of imaging algorithms for BFSAR have been reported. Based on the extended Loffeld’s bistatic formula (ELBF) method,^{11} a range-Doppler algorithm is developed.^{12} But the ELBF method has its limitations in representing the bistatic point target reference spectrum (BPTRS). A chirp scaling algorithm (CSA) based on the method of Legendre polynomial extension was also proposed.^{13} The accuracy of this imaging solution is decided by the reserved order of an expending Taylor series. With the keystone transform method, a nonlinear chirp scaling algorithm for one-stationary BFSAR was derived.^{14} In addition, a modified Omega-k algorithm was also reported.^{15}

To develop new frequency-domain imaging algorithms, we have to obtain the BPTRS of BFSAR first. The BPTRS derived by the method of series reversion (MSR)^{16} has a good focusing performance for the general bistatic configuration, even for extreme squint cases. Due to the series form, it is not easy for MSR to be used for imaging algorithm deduction, especially for chirp scaling and Omega-k algorithms.^{17} The Loffeld’s bistatic formula (LBF) was first introduced in Ref. 18. In LBF, the contributions of the transmitter and receiver to the total Doppler frequency are assumed to be the same. This assumption results in the failure of LBF in the extreme configuration (i.e., spaceborne/airborne configuration). The ELBF^{11} was proposed, but it cannot handle the large squint cases of bistatic SAR. The zeroth-order ELBF^{19} obtained two gradient equations to solve the Doppler contributions. However, the method would lead to some degradation when it is used in cases with extreme squint or with forward-looking cases to some extent.^{17}

In this paper, a modified Loffeld’s bistatic formula (MLBF) has been proposed. Compared to LBF^{18} and ELBF,^{11} it can precisely represent the bistatic point target reference spectrum of bistatic forward-looking SAR. Then, a CSA based on BPTRS was derived. Because CSA is free of interpolation, this algorithm has an obvious superiority in efficiency. Finally, numerical simulations were carried out to validate the focusing solution for BFSAR.

## 2.

## Modified Loffeld’s Bistatic Formula

The geometry configuration of BFSAR is shown in Fig. 1. The transmitter works in the side-looking mode and the receiver works in the forward-looking mode, respectively. The two platforms move along the $y$ axis. The mathematical symbols and their definitions used in Fig. 1 are given as follows:

$t$ and $\tau $: Time variables of range and azimuth.

${\tau}_{\mathrm{OT}}$ and ${\tau}_{\mathrm{OR}}$: Zero Doppler times of the transmitter and receiver.

${r}_{\mathrm{OT}}$ and ${r}_{\mathrm{OR}}$: The closest ranges from transmitter and receiver to the point target P.

${R}_{T}(\tau )$ and ${R}_{R}(\tau )$: Instantaneous slant ranges from the transmitter and receiver to the point target P.

${\theta}_{Tc}$ and ${\theta}_{Rc}$: The squint angle of the transmitter and the forward-looking angle of the receiver at the composite beam center crossing time.

${v}_{T}$ and ${v}_{R}$: Velocities of the transmitter and receiver, respectively.

The instantaneous slant ranges from the transmitter and receiver to the point target P at time $\tau $ are defined as

Hence, the echo data from target P after demodulation are

## (3)

$$g(t,\tau )={\sigma}_{p}{w}_{r}[t-\frac{{R}_{T}(\tau )+{R}_{R}(\tau )}{c}]{w}_{a}(\tau -{\tau}_{c})\mathrm{exp}\left\{j\pi {k}_{r}{[t-\frac{{R}_{T}(\tau )+{R}_{R}(\tau )}{c}]}^{2}\right\}\phantom{\rule{0ex}{0ex}}\xb7\mathrm{exp}[-j2\pi \frac{{R}_{T}(\tau )+{R}_{R}(\tau )}{\lambda}],$$Taking a two-dimensional FFT for Eq. (3), we get

## (4)

$$g(f,{f}_{\tau})={\sigma}_{p}{w}_{r}(f)\mathrm{exp}\{-j\pi \frac{{f}^{2}}{{k}_{r}}\}\int {w}_{a}(\tau -{\tau}_{c})\mathrm{exp}[-j{\varphi}_{b}(f,\tau )]\mathrm{d}\tau ,$$## (5)

$${\varphi}_{b}(f,\tau )=2\pi (f+{f}_{0})\frac{{R}_{T}(\tau )+{R}_{R}(\tau )}{c}+2\pi {f}_{\tau}\tau \phantom{\rule{0ex}{0ex}}=\frac{2\pi (f+{f}_{0})}{c}[\sqrt{{r}_{\mathrm{OT}}^{2}+{(\tau -{\tau}_{\mathrm{OT}})}^{2}{v}_{T}^{2}}+\sqrt{{r}_{\mathrm{OR}}^{2}+{(\tau -{\tau}_{\mathrm{OR}})}^{2}{v}_{R}^{2}}]+2\pi {f}_{\tau}\tau .$$From Eqs. (4) and (5), we can see that the bistatic phase term ${\varphi}_{b}(f,\tau )$ contains a double square root and is included in the integral. It is difficult to obtain the BPTRS from Eq. (4) by directly applying the stationary phase.^{20}^{,}^{21} Thus, we split the bistatic phase term, Eq. (5), into two components as follows:

^{18}it is assumed that the contributions of the transmitter and receiver to the azimuth modulation are the same. The assumptions are shown as follows:

However, the real azimuth modulations of the transmitter and receiver are not equal at all when the LBF is used in the extreme configuration (i.e., spaceborne/airborne configuration). Then, ELBF^{11} formulates ${f}_{\tau T}$ and ${f}_{\tau R}$ as follows:

The zeroth-order ELBF method^{19} makes the result of Eq. (12) as small as possible.

In this paper, we try to solve the instantaneous azimuth frequencies ${f}_{\tau T}$ and ${f}_{\tau R}$ directly. Here, we redraw the geometries of the flight tracks of the transmitter and receiver, as shown in Fig. 2.

In Fig. 2, ${\theta}_{T}$ and ${\theta}_{R}$ are the instantaneous squint and forward-looking angles at time $\tau $; ${R}_{Tc}$ and ${R}_{Rc}$ are the slant ranges of the transmitter and receiver at the composite beam center crossing time ${\tau}_{c}$. Suppose the transmitter and receiver both start flying at time ${\tau}_{c}$; after time $\mathrm{\Delta}\tau $ we can get the following relationship:

## (13)

$$\frac{{R}_{Tc}\text{\hspace{0.17em}}\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Tc}-{R}_{Tc}\text{\hspace{0.17em}}\mathrm{cos}\text{\hspace{0.17em}}{\theta}_{Tc}\text{\hspace{0.17em}}\mathrm{tan}\text{\hspace{0.17em}}{\theta}_{T}}{{v}_{T}}=\frac{{R}_{Rc}\text{\hspace{0.17em}}\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Rc}-{R}_{Rc}\text{\hspace{0.17em}}\mathrm{cos}\text{\hspace{0.17em}}{\theta}_{Rc}\text{\hspace{0.17em}}\mathrm{tan}\text{\hspace{0.17em}}{\theta}_{R}}{{v}_{R}}.$$Meanwhile, the two instantaneous Doppler frequencies satisfy the following relationship:

## (14)

$${f}_{\tau}=\frac{f+{f}_{0}}{c}({v}_{T}\text{\hspace{0.17em}}\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{T}+{v}_{R}\text{\hspace{0.17em}}\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{R})={f}_{\tau T}+{f}_{\tau R}.$$Solving the equations composed by Eqs. (13) and (14), we can get the analytic expression of the frequencies ${f}_{\tau T}$ and ${f}_{\tau R}$. We expand ${f}_{\tau T}$ and ${f}_{\tau R}$ in their Taylor series as follows:

## (15)

$$\{\begin{array}{c}{f}_{\tau T}={f}_{\tau TC}+{A}_{T1}({f}_{\tau}-{f}_{\tau C})+{A}_{T2}{({f}_{\tau}-{f}_{\tau C})}^{2}+{A}_{T3}{({f}_{\tau}-{f}_{\tau C})}^{3}\\ {f}_{\tau R}={f}_{\tau RC}+{A}_{R1}({f}_{\tau}-{f}_{\tau C})+{A}_{R2}{({f}_{\tau}-{f}_{\tau C})}^{2}+{A}_{R3}{({f}_{\tau}-{f}_{\tau C})}^{3}\end{array},$$## (16)

$$\{\begin{array}{l}{f}_{\tau C}={f}_{\tau TC}+{f}_{\tau RC}\\ {f}_{\tau TC}=({f}_{\tau}+{f}_{c}){v}_{T}\text{\hspace{0.17em}}\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Tc}/c\\ {f}_{\tau RC}=({f}_{\tau}+{f}_{c}){v}_{R}\text{\hspace{0.17em}}\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Rc}/c\end{array}.$$Combined with Eqs. (13) and (14), coefficients ${A}_{T1}\dots {A}_{T3}$, ${A}_{R1}\dots {A}_{R3}$ can be obtained, then we get the analytic expressions of the frequencies ${f}_{\tau T}$ and ${f}_{\tau R}$. Although the results in Eq. (15) are more precise than those in Ref. 19 due to the high-order term in Eq. (15), the complexity of the method is greatly increased. It would make present difficulties when we derive the chirp scaling algorithm later. Therefore, some linear approximations are used here to solve Eqs. (13) and (14). We expand $\mathrm{tan}\text{\hspace{0.17em}}{\theta}_{T}$ and $\mathrm{tan}\text{\hspace{0.17em}}{\theta}_{R}$ in their Taylor series at $\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{T}=\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Tc}$ and $\mathrm{sin}{\theta}_{R}=\mathrm{sin}{\theta}_{Rc}$, respectively, and only reserve the first-order term.

## (17)

$$\{\begin{array}{c}\mathrm{tan}\text{\hspace{0.17em}}{\theta}_{T}=\mathrm{tan}\text{\hspace{0.17em}}{\theta}_{Tc}+\frac{\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{T}-\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Tc}}{{\mathrm{cos}}^{3}\text{\hspace{0.17em}}{\theta}_{Tc}}\\ \mathrm{tan}\text{\hspace{0.17em}}{\theta}_{R}=\mathrm{tan}\text{\hspace{0.17em}}{\theta}_{Rc}+\frac{\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{R}-\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Rc}}{{\mathrm{cos}}^{3}\text{\hspace{0.17em}}{\theta}_{Rc}}\end{array}.$$Substituting Eq. (17) into Eq. (13) and combining Eq. (14), the equations are solved as follows:

## (18)

$$\{\begin{array}{c}\begin{array}{l}{f}_{\tau T}(f,{f}_{\tau})=\frac{{R}_{Rc}{v}_{T}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Tc}{f}_{\tau}}{{R}_{Tc}{v}_{R}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Rc}+{R}_{Rc}{v}_{T}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Tc}}\\ \begin{array}{c}+\frac{{v}_{T}(f+{f}_{0})({R}_{Tc}{v}_{R}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Rc}\text{\hspace{0.17em}}\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Tc}-{R}_{Rc}{v}_{T}{v}_{R}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Tc}\text{\hspace{0.17em}}\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Rc})}{c({R}_{Tc}{v}_{R}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Rc}+{R}_{Rc}{v}_{T}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Tc})}\end{array}\end{array}\\ \begin{array}{l}{f}_{\tau R}(f,{f}_{\tau})=\frac{{R}_{Tc}{v}_{R}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Rc}{f}_{\tau}}{{R}_{Tc}{v}_{R}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Rc}+{R}_{Rc}{v}_{T}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Tc}}\\ \begin{array}{c}+\frac{{v}_{R}(f+{f}_{0})({R}_{Rc}{v}_{T}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Tc}\text{\hspace{0.17em}}\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Rc}-{R}_{Tc}{v}_{T}{v}_{R}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Rc}\text{\hspace{0.17em}}\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Tc})}{c({R}_{Tc}{v}_{R}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Rc}+{R}_{Rc}{v}_{T}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Tc})}\end{array}\end{array}\end{array}.$$Although linear approximation is used, the max error made by this approximation (with Table 1 simulation parameters, which is discussed later in this paper, the forward-looking angle of the receiver is 45 deg) is $1.85\times {10}^{-3}\text{\hspace{0.17em}}\text{\hspace{0.17em}}\mathrm{rad}$. Therefore, the error can be ignored and Eq. (18) can precisely present the contributions of the transmitter and receiver to the total azimuth modulation. After obtaining the instantaneous azimuth frequency of the transmitter and receiver, we expand Eqs. (7) and (8) at their points of the stationary phase ${\tau}_{T}$ and ${\tau}_{R}$. The expanded series are truncated at the second-order term, given as

## (19)

$${\varphi}_{T}(\tau )\approx {\varphi}_{T}({\tau}_{T})+\frac{1}{2}{\varphi}_{T}^{\prime \prime}({\tau}_{T}){(\tau -{\tau}_{T})}^{2},$$## (20)

$${\varphi}_{R}(\tau )\approx {\varphi}_{R}({\tau}_{R})+\frac{1}{2}{\varphi}_{R}^{\prime \prime}({\tau}_{R}){(\tau -{\tau}_{R})}^{2},$$## (21)

$${\tau}_{T}={\tau}_{\mathrm{OT}}-\frac{c{r}_{\mathrm{OT}}{f}_{\tau T}}{{v}_{T}^{2}{F}_{T}}\phantom{\rule[-0.0ex]{2em}{0.0ex}}{\tau}_{R}={\tau}_{\mathrm{OR}}-\frac{c{r}_{\mathrm{OR}}{f}_{\tau R}}{{v}_{R}^{2}{F}_{R}},$$## (22)

$${F}_{T}=\sqrt{{(f+{f}_{0})}^{2}-{\left(\frac{c{f}_{\tau T}}{{v}_{T}}\right)}^{2}}\phantom{\rule[-0.0ex]{2em}{0.0ex}}{F}_{R}=\sqrt{{(f+{f}_{0})}^{2}-{\left(\frac{c{f}_{\tau R}}{{v}_{R}}\right)}^{2}},$$## (23)

$${\varphi}_{T}^{\prime \prime}({\tau}_{T})=\frac{2\pi}{c}\frac{{v}_{T}^{2}{F}_{T}^{3}}{{r}_{\mathrm{OT}}{(f+{f}_{0})}^{2}}\phantom{\rule[-0.0ex]{2em}{0.0ex}}{\varphi}_{R}^{\prime \prime}({\tau}_{R})=\frac{2\pi}{c}\frac{{v}_{R}^{2}{F}_{R}^{3}}{{r}_{\mathrm{OR}}{(f+{f}_{0})}^{2}}.$$## Table 1

System parameters in parallel tracks.

Parameters | Transmitter | Receiver |
---|---|---|

Carrier frequency | 9.65 GHz | |

Range bandwidth | 100 MHz | |

Velocity | 200 m/s | |

Pulse recurrence frequency sampling rate | 600 Hz 180 MHz | |

Position | (0,4,8) km | (10,0,4) km |

Squint angle | 0 deg | / |

Forward-looking angle | / | 45 deg |

Substituting Eqs. (6), (19), and (20) into Eq. (4), we get

## (24)

$$g(f,{f}_{\tau})={\sigma}_{p}{w}_{r}(f)\mathrm{exp}\{-j\pi \frac{{f}^{2}}{{k}_{r}}\}\mathrm{exp}\{-j[{\varphi}_{T}(f,{\tau}_{T})+{\varphi}_{R}(f,{\tau}_{R})]\}\phantom{\rule{0ex}{0ex}}\xb7\int {w}_{a}(\tau -{\tau}_{c})\mathrm{exp}\{-\frac{j}{2}[{\varphi}_{T}^{\prime \prime}(f,{\tau}_{T})(\tau -{\tau}_{T})+{\varphi}_{R}^{\prime \prime}(f,{\tau}_{R})(\tau -{\tau}_{R})]\}\mathrm{d}\tau .$$Applying stationary phase techniques to the last exponent in Eq. (24), we get the bistatic stationary phase ${\tau}_{b}$.

## (25)

$${\tau}_{b}=\frac{{r}_{\mathrm{OT}}{v}_{R}^{2}{F}_{R}^{3}{\tau}_{\mathrm{OR}}+{r}_{\mathrm{OR}}{v}_{T}^{2}{F}_{T}^{3}{\tau}_{\mathrm{OT}}}{{v}_{T}^{2}{F}_{T}^{3}{r}_{\mathrm{OR}}+{v}_{R}^{2}{F}_{R}^{3}{r}_{\mathrm{OT}}}-\frac{c{r}_{\mathrm{OT}}{r}_{\mathrm{OR}}({F}_{T}^{2}{f}_{\tau T}+{F}_{R}^{2}{f}_{\tau R})}{{v}_{T}^{2}{F}_{T}^{3}{r}_{\mathrm{OR}}+{v}_{R}^{2}{F}_{R}^{3}{r}_{\mathrm{OT}}}.$$Finally, we get the BPTRS of the BFSAR.

## (26)

$$g(f,{f}_{\tau})={\sigma}_{p}\text{\hspace{0.17em}}\mathrm{exp}\{-j\pi \frac{{f}^{2}}{{k}_{r}}\}\mathrm{exp}\{-j{\psi}_{\mathrm{QM}}\}\mathrm{exp}\{-\frac{j}{2}{\psi}_{\mathrm{BD}}\},$$## (27)

$${\psi}_{\mathrm{QM}}={\varphi}_{T}(f,{\tau}_{T})+{\varphi}_{R}(f,{\tau}_{R})\phantom{\rule{0ex}{0ex}}=2\pi ({f}_{\tau T}{\tau}_{\mathrm{OT}}+{f}_{\tau R}{\tau}_{\mathrm{OR}})+\frac{2\pi}{c}({r}_{\mathrm{OT}}{F}_{T}+{r}_{\mathrm{OR}}{F}_{R}),$$## (28)

$${\psi}_{\mathrm{BD}}={\varphi}_{T}^{\prime \prime}(f,{\tau}_{T}){({\tau}_{b}-{\tau}_{T})}^{2}+{\varphi}_{R}^{\prime \prime}(f,{\tau}_{R}){({\tau}_{b}-{\tau}_{R})}^{2}\phantom{\rule{0ex}{0ex}}=\frac{2\pi {v}_{T}^{2}{v}_{R}^{2}{F}_{T}^{3}{F}_{R}^{3}}{c{(f+{f}_{0})}^{2}({v}_{T}^{2}{F}_{T}^{3}{r}_{\mathrm{OR}}+{v}_{R}^{2}{F}_{R}^{3}{r}_{\mathrm{OT}})}\phantom{\rule{0ex}{0ex}}\xb7{[({\tau}_{\mathrm{OT}}-{\tau}_{\mathrm{OR}})-\frac{c}{{v}_{T}^{2}{v}_{R}^{2}{F}_{T}{F}_{R}}({r}_{\mathrm{OT}}{v}_{R}^{2}{F}_{R}{f}_{\tau T}-{r}_{\mathrm{OR}}{v}_{T}^{2}{F}_{T}{f}_{\tau R})]}^{2}.$$${\psi}_{\mathrm{QM}}$ can be considered as the quasi-monostatic phase term, and ${\psi}_{\mathrm{BD}}$ is defined as the bistatic deformation phase term. Before implementing an imaging algorithm, the bistatic deformation phase term should be compensated. The method proposed above can be considered as an MLBF.

## 3.

## CSA for the Bistatic Forward-Looking SAR Processing

Instead of interpolation, chirp phase multiplication is used in CSA to correct the range cell migration (RCM). It is an efficient algorithm. However, due to the unknown scaling factor, it is complex to derive CSA based on the BPTRS obtained by the MLBF.

After compensating the bistatic deformation phase term, we transform Eq. (26) into a range-Doppler domain and obtain the expression as

## (29)

$$g(t,{f}_{\tau})={\sigma}_{p}\text{\hspace{0.17em}}\mathrm{exp}[-j\frac{2\pi}{c}({r}_{\mathrm{OT}}{D}_{T}+{r}_{\mathrm{OR}}{D}_{R}){f}_{0}]\mathrm{exp}[-j2\pi (B\xb7{\tau}_{\mathrm{OT}}+E\xb7{\tau}_{\mathrm{OR}}){f}_{0}]\phantom{\rule{0ex}{0ex}}\xb7\mathrm{exp}[-j2\pi (A\xb7{\tau}_{\mathrm{OT}}+D\xb7{\tau}_{\mathrm{OR}}){f}_{\tau}]\mathrm{exp}\left\{j\pi {k}_{m}{[t-\frac{R({f}_{\tau})}{c}]}^{2}\right\},$$## (30)

$$A=\frac{{R}_{Rc}{v}_{T}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Tc}}{{R}_{Tc}{v}_{R}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Rc}+{R}_{Rc}{v}_{T}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Tc}},$$## (31)

$$B=\frac{{v}_{T}({R}_{Tc}{v}_{R}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Rc}\text{\hspace{0.17em}}\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Tc}-{R}_{Rc}{v}_{T}{v}_{R}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Tc}\text{\hspace{0.17em}}\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Rc})}{c({R}_{Tc}{v}_{R}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Rc}+{R}_{Rc}{v}_{T}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Tc})},$$## (32)

$$D=\frac{{R}_{Tc}{v}_{R}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Rc}}{{R}_{Tc}{v}_{R}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Rc}+{R}_{Rc}{v}_{T}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Tc}},$$## (33)

$$E=\frac{{v}_{R}({R}_{Rc}{v}_{T}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}{\theta}_{Tc}\text{\hspace{0.17em}}\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Rc}-{R}_{Tc}{v}_{T}{v}_{R}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Rc}\text{\hspace{0.17em}}\mathrm{sin}\text{\hspace{0.17em}}{\theta}_{Tc})}{c({R}_{Tc}{v}_{R}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Rc}+{R}_{Rc}{v}_{T}^{2}\text{\hspace{0.17em}}{\mathrm{cos}}^{2}\text{\hspace{0.17em}}{\theta}_{Tc})},$$## (34)

$${\mu}_{T1}=A\xb7\frac{c{f}_{\tau}}{{f}_{0}{v}_{T}}+B\xb7\frac{c}{{v}_{T}}\phantom{\rule[-0.0ex]{2em}{0.0ex}}{\mu}_{T2}=B\xb7\frac{c}{{v}_{T}},$$## (35)

$${\mu}_{R1}=D\xb7\frac{c{f}_{\tau}}{{f}_{0}{v}_{R}}+E\xb7\frac{c}{{v}_{R}}\phantom{\rule[-0.0ex]{2em}{0.0ex}}{\mu}_{R2}=E\xb7\frac{c}{{v}_{R}},$$## (36)

$${D}_{T}=\sqrt{1-{\mu}_{T1}^{2}}\phantom{\rule[-0.0ex]{2em}{0.0ex}}{D}_{R}=\sqrt{1-{\mu}_{R1}^{2}}.$$In Eq. (29), the frequency-modulated rate ${k}_{r}$ in range is changed by the coupling of the range and azimuth, and the new chirp rate ${k}_{m}$ in range-Doppler domain is given as

## (37)

$${k}_{m}=\frac{{k}_{r}}{1-\frac{c{k}_{r}{f}_{\tau}^{2}}{{f}_{0}^{3}}(\frac{{A}^{2}{r}_{\mathrm{OT}}}{{D}_{T}^{3}{v}_{T}^{2}}+\frac{{D}^{2}{r}_{\mathrm{OR}}}{{D}_{R}^{3}{v}_{R}^{2}})}.$$In Eq. (29), $R({f}_{\tau})$ is the range migration of a target and is defined as

## (38)

$$R({f}_{\tau})=c\xb7(B\xb7{\tau}_{\mathrm{OT}}+E\xb7{\tau}_{\mathrm{OR}})+\frac{(1-{\mu}_{T1}{\mu}_{T2}){r}_{\mathrm{OT}}}{{D}_{T}}+\frac{(1-{\mu}_{R1}{\mu}_{R2}){r}_{\mathrm{OR}}}{{D}_{R}}.$$We assume the range chirp scaling function for the BFSAR as follows:

## (39)

$${H}_{CS}=\mathrm{exp}\left\{j\pi {k}_{m}{C}_{s}{[t-\frac{{R}_{\mathrm{ref}}({f}_{\tau})}{c}]}^{2}\right\},$$## (40)

$${R}_{\mathrm{ref}}({f}_{\tau})=c\xb7(B\xb7{\tau}_{\mathrm{OT}}+E\xb7{\tau}_{\mathrm{OR}})+\frac{(1-{\mu}_{T1}{\mu}_{T2}){r}_{\mathrm{OT}\_\mathrm{ref}}}{{D}_{T}}+\frac{(1-{\mu}_{R1}{\mu}_{R2}){r}_{\mathrm{OR}\_\mathrm{ref}}}{{D}_{R}}.$$In Ref (41), ${r}_{\mathrm{OT}\_\mathrm{ref}}$ and ${r}_{\mathrm{OR}\_\mathrm{ref}}$ are the closest ranges from the transmitter and receiver to the reference target. (The target located at the middle of the imaging scene is usually chosen as the reference target.) We multiply Eq. (29) by Eq. (39) and implement FFT in the range direction, and then get

## (41)

$${G}_{1}(f,{f}_{\tau})={\sigma}_{p}\text{\hspace{0.17em}}\mathrm{exp}[-j\frac{2\pi}{c}({r}_{\mathrm{OT}}{D}_{T}+{r}_{\mathrm{OR}}{D}_{R}){f}_{0}]\mathrm{exp}[-j2\pi (B\xb7{\tau}_{\mathrm{OT}}+E\xb7{\tau}_{\mathrm{OR}}){f}_{0}]\phantom{\rule{0ex}{0ex}}\xb7\mathrm{exp}[-j2\pi (A\xb7{\tau}_{\mathrm{OT}}+D\xb7{\tau}_{\mathrm{OR}}){f}_{\tau}]\mathrm{exp}[-j\pi \frac{{f}^{2}}{(1+{C}_{s}){k}_{m}}]\phantom{\rule{0ex}{0ex}}\xb7\mathrm{exp}[-j2\pi f\frac{R({f}_{\tau})+{C}_{s}{R}_{\mathrm{ref}}({f}_{\tau})}{(1+{C}_{s})c}]\mathrm{exp}\left\{j\pi {k}_{m}\frac{{C}_{s}{[R({f}_{\tau})-{R}_{\mathrm{ref}}({f}_{\tau})]}^{2}}{(1+{C}_{s}){c}^{2}}\right\}.$$In Eq. (41), we can clearly see that the total RCM is

Because the translational invariant case is used in this paper, we make some linear approximations.^{12} The approximations are given as

## (45)

$$\mathrm{RCM}=c[B\xb7{p}_{0}+(B+E){\tau}_{\mathrm{OR}}]+\frac{(1-{\mu}_{T1}{\mu}_{T2}){p}_{1}}{{D}_{T}}+\frac{{C}_{s}{r}_{\mathrm{OR}\_\mathrm{ref}}}{1+{C}_{s}}[\frac{(1-{\mu}_{T1}{\mu}_{T2}){p}_{2}}{{D}_{T}}+\frac{1-{\mu}_{R1}{\mu}_{R2}}{{D}_{R}}]\phantom{\rule{0ex}{0ex}}+\frac{{r}_{\mathrm{OR}}}{1+{C}_{s}}[\frac{(1-{\mu}_{T1}{\mu}_{T2}){p}_{2}}{{D}_{T}}+\frac{1-{\mu}_{R1}{\mu}_{R2}}{{D}_{R}}],$$## (46)

$$\frac{{r}_{\mathrm{OR}}}{1+{C}_{s}}[\frac{(1-{\mu}_{T1}{\mu}_{T2}){p}_{2}}{{D}_{T}}+\frac{1-{\mu}_{R1}{\mu}_{R2}}{{D}_{R}}]=(1+{p}_{2}){r}_{\mathrm{OR}}.$$## (47)

$${C}_{s}=\frac{1}{1+{p}_{2}}[\frac{(1-{\mu}_{T1}{\mu}_{T2}){p}_{2}}{{D}_{T}}+\frac{1-{\mu}_{R1}{\mu}_{R2}}{{D}_{R}}]-1.$$Therefore, after substituting Eq. (47) into Eq. (41), we can rewrite Eq. (41) without unknown variables. Then, we use the following matching filters to complete the image focusing:

## (48)

$${H}_{\mathrm{RC}}=\mathrm{exp}\left[j\pi \frac{{f}^{2}}{(1+{C}_{s}){k}_{m}}\right]\xb7\mathrm{exp}\left\{j\frac{2\pi {C}_{s}{r}_{\mathrm{OR}\_\mathrm{ref}}}{c(1+{C}_{s})}\right[\frac{(1-{\mu}_{T1}{\mu}_{T2}){p}_{2}}{{D}_{T}}+\frac{1-{\mu}_{R1}{\mu}_{R2}}{{D}_{R}}\left]f\right\},$$## (49)

$${H}_{\mathrm{RES}}=\mathrm{exp}\{-j\pi {k}_{m}\frac{{C}_{s}{[R({f}_{\tau})-{R}_{\mathrm{ref}}({f}_{\tau})]}^{2}}{(1+{C}_{s}){c}^{2}}\},$$## (50)

$${H}_{\mathrm{AC}}=\mathrm{exp}[j2\pi (A\xb7{\tau}_{\mathrm{OT}}+D\xb7{\tau}_{\mathrm{OR}}){f}_{\tau}]\mathrm{exp}[j\frac{2\pi}{c}({r}_{\mathrm{OT}}{D}_{T}+{r}_{\mathrm{OR}}{D}_{R}){f}_{0}]\phantom{\rule{0ex}{0ex}}\xb7\mathrm{exp}[j2\pi (B\xb7{\tau}_{\mathrm{OT}}+E\xb7{\tau}_{\mathrm{OR}}){f}_{0}],$$## 4.

## Simulation Results

In order to verify the focusing solution for the BFSAR, two simulation experiments are carried out in this section. The first experiment is to determine whether the BPTRS obtained by the MLBF is appropriate for the BFSAR case and to simultaneously compare the performance of the MLBF with those of other proposed methods. The second experiment is to validate the effectiveness of the proposed CSA.

The simulation parameters are listed in Table 1. We use the analytical BPTRS to focus the BPTRS obtained by LBF,^{18} ELBF,^{11} MLBF, and the spectra derived from the MSR using the fourth-order expansion.^{16} The focusing results are shown in Fig. 4.

From Figs. 4(a) and 4(b), we can see that the LBF and ELBF have severe degradation in the azimuth direction. They are not appropriate for bistatic forward-looking SAR cases. In general, the LBF method and ELBF method reach their limit when the forward-looking angle is 30 and 40 deg, respectively. Figures 4(c) and 4(d) reveal that MLBF and MSR are all focused on the point target. Furthermore, Fig. 4(e) shows the azimuth profiles of the MLBF and MSR. It is clear that the method proposed in this paper agrees with the MSR. However, the resulting accuracy of the spectrum from the MSR is dependent on the number of terms in the expansion. Here, we use the fourth-order expansion of the MSR. However, the spectrum of the MLBF is a closed form with a second term and still has a good performance. In addition, it is not easy for the MSR to be used for imaging algorithm deduction.

The CSA imaging results are shown in Fig. 5.

Figure 5(a) shows the locations of the simulated targets, where the distances between two adjacent targets along the range and azimuth directions are, respectively, 400 and 300 m. Figure 5(b) represents the contours of the final imaging result. The dynamic range shown in this picture is 30 dB. In order to further evaluate the imaging quality, Figs. 5(c) and 5(d) present the impulse profiles of the target P9 in the azimuth and range directions, respectively. The peak sidelobe ratio (PSLR) of the azimuth profile is $-14.52\text{\hspace{0.17em}}\text{\hspace{0.17em}}\mathrm{dB}$, and the integrated sidelobe ratio (ISLR) is $-11.04\text{\hspace{0.17em}}\text{\hspace{0.17em}}\mathrm{dB}$. The PSLR of the range profile is $-12.96\text{\hspace{0.17em}}\text{\hspace{0.17em}}\mathrm{dB}$, and the ISLR is $-9.78\text{\hspace{0.17em}}\text{\hspace{0.17em}}\mathrm{dB}$. More image quality parameters are listed in Table 2. The ideal impulse response width (IRWs) of the azimuth and range are 6.04 and 1.52 ceils (or samples), respectively. We can find that all the targets are well focused.

## Table 2

Image quality parameters.

Targets | Range | Azimuth | ||||
---|---|---|---|---|---|---|

PSLR (dB) | ISLR (dB) | IRW (ceils) | PSLR (dB) | ISLR (dB) | IRW (ceils) | |

PT1 | −12.96 | −9.77 | 1.54 | −14.42 | −10.96 | 6.14 |

PT5 | −13.02 | −9.80 | 1.54 | −14.53 | −11.10 | 6.06 |

PT9 | −12.96 | −9.78 | 1.55 | −14.52 | −11.04 | 6.20 |

PSLR, peak sidelobe ratio; ISLR, integrated sidelobe ratio.

## 5.

## Conclusions

A focusing solution for bistatic forward-looking SAR was presented in this paper. First, an MLBF was proposed to obtain the BPTRS. Then, a chirp scaling algorithm based on the BPTRS was derived. Compared to other imaging algorithms, CSA is free of interpolation. Finally, two simulation experiments were carried out to validate the focusing solution. The simulation results showed that the BPTRS obtained by the MLBF was more precise than the LBF and ELBF, and that the focusing capability of the derived CSA is high.

## Acknowledgments

This paper is supported by the PhD programs foundation of Ministry of China (Grant No. 20113219110018), the Ministry Pre-research Foundation (Grant No. 9140A07010713BQ02025), National Natural Science Foundation of China (Grant No. 61302188), and Natural Science Foundation of Jiangsu Province (Grant No. BK20131005).

## References

## Biography

**Chao Ma** received his BS degree from Hubei Engineering University, Hubei, China, in 2010. He is currently working toward his PhD degree in information and communication engineering at the Nanjing University of Science and Technology, Jiangsu, China, and is trained in the Institute of Electronic Engineering and Optoelectronic Technology. His research interests include synthetic aperture radar (SAR) signal processing and short-range imaging.

**Hong Gu** received his MS degree from Nanjing University of Science and Technology, Jiangsu, China, in 1991 and his PhD degree from Xidian University, Shanxi, China, in 1995. He is currently a professor, a Chinese Institute of Electronics senior member, and a member of the radar branch of the Jiangsu Electronic Society. His research interests include noise SAR, radar signal processing and information systems.

**Weimin Su** received his PhD degree from Nanjing University of Science and Technology, Jiangsu, China, in 1998. He is currently a professor, a senior member of the Chinese Institute of Electronics, a member of the Signal Processing Society of China, and a liaison of Nanjing University of Science and Technology, Jiangsu, China. His research interests include advanced SAR systems and signal processing technology.

**Chuanzhong Li** received his BS degree from Nanjing University of Science and Technologu, Jiangsu, China, in 2010. He is currently working toward his PhD degree in information and communication engineering at Nanjing University of Science and Technology, Jiangsu, China. His research interests include radar signal processing and noise SAR imaging.

**Jinli Chen** received his PhD degree from Nanjing University of Science and Technology, Jiangsu, China, in 2010. He is currently working in the Nanjing University of Information Science and Technology as a lecturer. His research interests include multiple input multiple output (MIMO) radar signal processing and high-speed moving target detecting.