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# Comparison and analysis of point target reference spectrum of FMCW synthetic aperture imaging sensor

- Yue Liu
^{1}, - Yun-Kai Deng
^{1}, - Robert Wang
^{1}Email author, - Xiao-Xue Jia
^{1}and - Xiao-Dong Han
^{1}

**2012**:210

https://doi.org/10.1186/1687-6180-2012-210

© Liu et al.; licensee Springer. 2012

**Received:**26 November 2011**Accepted:**3 September 2012**Published:**3 October 2012

## Abstract

Frequency-modulated continuous-wave (FMCW) synthetic aperture imaging sensor (SAIS) combines FMCW technology and SAIS techniques which makes a lightweight, high-resolution, and cost-effective imaging sensor. FMCW SAIS systems are going to play an important role in airborne and spaceborne earth observation fields. However, the stop-and-go approximation used in conventional pulsed SAIR (e.g., synthetic aperture radar—SAR) is no longer valid due to the long signal duration time or low wave propagation speed. To exploit the potentialities of an accurate signal model under FMCW SAIS circumstances, this article presents the relationship and remarkable differences between the analytical FMCW SAIS point target reference spectrum model and the traditional ones in pulsed SAR and Synthetic Aperture Acoustic imaging system, and validates the significance of the additional range–azimuth coupling term and range walk term in FMCW SAIS spectrum introduced by the variation of slant range during the long pulse durations, and highlight the limitations of other two spectra. Finally, the simulation experiments are carried out to compare the performance of the aforementioned spectrum formulations.

## Keywords

- Frequency-modulated continuous wave (FMCW)
- Synthetic aperture imaging sensor (SAIS)
- Synthetic aperture radar (SAR)
- Synthetic aperture acoustic (SAA) imaging system
- Range–azimuth coupling

## Introduction

Frequency-modulated continuous-wave (FMCW) synthetic aperture imaging sensor (SAIS) combines FMCW technology and SAIS techniques which makes a lightweight, high-resolution, and cost-effective imaging sensor [1]. Different from conventional synthetic aperture radar (SAR) system which requires high peak transmission power [1–3], FMCW SAIS system operates on constant low transmission by extending the pulse duration without degrading either the resolution or SNR. This peak power reduction simplifies the transmitter design, increasing both performance and reliability as well as reducing the risk of breakdown or arcing in the high power cables [4]. FMCW SAIS has been developed with both acoustic source and electromagnetic wave in airborne remote sensing fields, such as reconnaissance, concealed target detection, robotic sensing, non-destructive testing, gas flow measurements, mine detection, surveillance, and so on [5]. The advantage of small size, light weight, and low peak power also makes FMCW SAIS possible to be developed for spaceborne remote sensing fields, like microsatellites. FMCW SAIS systems are going to play an important role in airborne and spaceborne earth observation fields.

The point target reference spectrum (PTRS) is an important basis to focus the SAIS signal in the frequency domain where the time-consuming superposition integrals in the space time domain is substituted by the fast convolution in the frequency domain [6, 7]. Thus, the processing efficiency can be highly improved. The focus of this article is to exploit the potentialities of an analytical spectrum model for FMCW SAIS system with both acoustic source and electromagnetic wave. Unlike conventional pulse SAR system, the signal PTRS model is based on the stop-and-go approximation, which assumes that the instantaneous slant range remains constant during the pulse duration time [6]. The analytical FMCW SAIS PTRS generally expresses FMCW SAIS signal by accurately addressing the variation of the instantaneous slant range during the pulse duration time [2]. This variation introduces a range-invariant range walk and a range–azimuth coupling term [2, 7] (range–azimuth coupling term is a spectrum phase term which is dependent on both range and azimuth frequency variables at the same time). In [5], the author developed a signal model under synthetic aperture acoustic (SAA) imaging system, where the invalidation of stop-and-go approximation is taken into account. It is assumed that the time from the transmitter to the reflector equals to half of the round-trip delay. In this article, we concentrate on the differences and relationship between the analytical FMCW SAIS PTRS model and the traditional ones, and validate the significance of the differences, in order to present a principle of choosing proper signal models in different configurations.

This article is organized as follows. In “Signal models” section, we compare the analytical FMCW SAIR PTRS with the conventional ones. “Validating method” section gives a way to validate the accuracy of the signal spectrum model. Simulation experiments are carried out in “Simulation experiment” section to show the significance of the special terms (i.e., the additional range–azimuth coupling term and range walk term) in FMCW SAIS PTRS by comparing with the other two models in SAA imaging systems, broadside FMCW SAR, and high-squint FMCW SAR circumstances. Finally, conclusions are reported.

### Signal models

The mathematical symbols and their definitions used in this article are given as follows.

$t,\tau $ Range and azimuth time variables

$f,{f}_{\tau}\phantom{\rule{0.25em}{0ex}}$ Range and azimuth frequency variables

${K}_{r}\phantom{\rule{0.25em}{0ex}}$ Chirp rate

$\text{R}$ Slant range variable

$P\left({\tau}_{0},{r}_{0}\right)$ Point target located at $\left({\tau}_{0},{r}_{0}\right)$

${\tau}_{0}$ Zero-Doppler time of the target $P\left({\tau}_{0},{r}_{0}\right)$

${r}_{0}$ Shortest slant range from the target $P\left({\tau}_{0},{r}_{0}\right)$ to the sensor

$\sigma \left({\tau}_{0},{r}_{0}\right)$ Backscattering coefficient of the point target $P\left({\tau}_{0},{r}_{0}\right)$

$c\phantom{\rule{0.25em}{0ex}}$ Wave propagation speed

$v$ Platform velocity

$\lambda ,{f}_{c}$ Carrier wavelength and carrier frequency of the transmitted signal

${r}_{c}$ Reference range for dechirp-on-receive operation

The stop-and-go approximation is commonly used in conventional-pulsed SAR focusing algorithms, where the instantaneous slant range from the antenna to the target is assumed to remain constant during the pulse duration time. However, for FMCW imaging mode, in fact, the variation of instantaneous slant range during each pulse could not be neglected due to the long signal duration, thus the stop-and-go approximation used in conventional SAR PTRS is no longer valid.

By representing the accurate instantaneous slant range during the pulse duration time on the transmitted and received signal [2], the authors developed an analytical signal model for the FMCW SAR imaging system. As it is developed analytically without any approximation, it could be used as a general expression for FMCW SAIS system. The brief derivation is outlined as follows.

- 1)
The main difference between the FMCW SAIS spectrum and the pulsed SAR spectrum is the square root of the previous one contains the additional range–azimuth coupling term $\left({f}_{0}+f\right)v/c$, which is not presented in the pulsed SAR PTRS [2, 6]. The additional term of FMCW SAIS is introduced by the variation of the slant range during the long pulse duration, and results in the skewness of the 2D spectrum along the range frequency direction [2, 6]. In (7), the author also realized the inaccuracy of stop-and-go assumption and introduced a range–azimuth coupling term, but in a different expression from the analytical one as it is developed with approximation. This coupling term is the dominant difference between the aforementioned three spectrums.

- 2)
The term $-2\pi {f}_{\tau}f/{K}_{r}$ exists in both (4) and (7). It is a range-invariant range walk term, which is also caused by the variation of the slant range during the pulse duration.

- 3)
The three spectra share a common term $2\pi {f}_{\tau}{\tau}_{0}$, which is linearly dependent on the zero-Doppler time of the target. Thus, it determines the azimuth registration position of the target after azimuth compression.

- 4)
$-4\pi \alpha \left({f}_{\tau}+{f}_{0}+f\right){r}_{c}/c$, $-4\pi \left({f}_{\tau}+{f}_{0}+f\right){r}_{c}/c$, and $-4\pi \alpha \left({f}_{\tau}+{f}_{0}+f\right){r}_{c}/c$ are the last terms of the three spectrums, respectively. They are almost the same except for the second one which does not contain a Doppler factor $\alpha $. All of them are introduced by the dechirp-on-receive approach and refer to the constant range and azimuth shifts.

- 5)
The Doppler factor $\alpha $ is generated by the relative motion between the platform and targets, which is always larger than 1. $\alpha $ will significantly be large when the platform velocity and wave propagation speed are comparable, like SAA imaging circumstance.

We will validate the significance of the accurate FMCW SAR PTRS in “Simulation experiment” section and quest for if the other two spectrum formulations (6) and (7) can work under FMCW SAIS systems, i.e., SAA imaging system and FMCW radar system.

### Validating method

where ${p}_{r}\left(t\right)$ and ${p}_{a}\left(\tau \right)$ are the sinc-like compressed pulse envelope in the range and azimuth, respectively.

From (11), we can see that for the only target we consider at $P\left({\tau}_{0},{r}_{0}\right)$, the signal is perfectly focused when we define the reference slant range as the closest range from the target to the antenna. That is to say, if the spectrum represents the characteristic of FMCW SAIS well, the target at the reference range will be well focused, otherwise, it will be de-focused.

In the next section, we will highlight the significance of the range–azimuth coupling term and range walk term introduced by the variation of the slant range during the long pulse duration, by showing the different simulation results based on the different PTRS models.

### Simulation experiment

Airborne simulations will be carried out in this section to validate the performance of FMCW SAIS spectrum model in both SAA imaging configuration and FMCW radar systems, respectively. We will also show the significance of the additional range–azimuth coupling term and range walk term, by calculating the phase error of the signal model in (4) and (5), and show the different simulation results based on the different spectrum models.

### SAA imaging system

**SAA imaging system parameters**

Parameters and requirements | Values |
---|---|

Carrier frequency | 10 kHz |

Acoustic signal velocity | 340 m/s |

Altitude | 100 m |

Platform velocity | 30 m/s |

PRF | 1200 Hz |

Range bandwidth | 1 kHz |

Azimuth antenna length | 0.4 m |

Squint angle | 0 |

Slant range | 140 m |

- (1)
The first filtering function is based on the FMCW SAIS PTRS (6), i.e., $H\left({f}_{\tau},f,{r}_{\mathit{ref}}\right)$, which is formulated based on the analytical development without any approximation. This is the most accurate formulation for FMCW SAIS. The processing result based on the FMCW SAIS PTRS is shown in Figure 3a. To show the focusing performance in more details, the contour of the target amplitude is shown in Figure 3b. The measured parameters of the focused target listed in Table 2 agree well with the theoretical values, which means that the proposed SAIS PTRS model gets the target well focused.

- (2)The second simulation experiment is based on the traditional SAR signal PTRS model, which is developed under stop-and-go approximation. According to (4), the matched filter based on conventional SAR model is formulated as${F}_{\mathit{SAR}}\left({f}_{\tau},f,{r}_{0}\right)=exp\left\{j\left[\frac{4\pi {r}_{0}}{c}\sqrt{{\left({f}_{0}+f\right)}^{2}-{\left(\frac{c{f}_{\tau}}{2v}\right)}^{2}}-\frac{2\pi {f}^{2}}{{K}_{r}}-4\pi \frac{{r}_{c}}{c}\left({f}_{\tau}+{f}_{0}+f\right)\right]\right\}$(14)The focused result using the conventional SAR matched filter ${F}_{\mathit{SAR}}\left({f}_{\tau},f,{r}_{0}\right)$ (12) is shown in Figure 3c. The contour of the focused result is shown in Figure 3d for more details. Parameters of the focused target are listed in Table 2, which greatly deviate from the theoretical values. Obviously applying ${F}_{\mathit{SAR}}\left({f}_{\tau},f,{r}_{0}\right)$ does not achieve satisfactory focusing result. This could be explained by the phase error term of SAR spectrum model ${\Phi}_{\mathit{ESAR}}\left({f}_{\tau},f,{r}_{0}\right)$, i.e.,${\Phi}_{\mathit{ESAR}}\left({f}_{\tau},f,{r}_{0}\right)=-\frac{4\pi {r}_{0}}{c}\left(\alpha \sqrt{{\left({f}_{0}+f\right)}^{2}-{\left[\frac{v}{c}\left({f}_{0}+f\right)+\frac{c{f}_{\tau}}{2\alpha v}\right]}^{2}}-\sqrt{{\left({f}_{0}+f\right)}^{2}-{\left(\frac{c{f}_{\tau}}{2v}\right)}^{2}}\right)$(15)Based on the system parameters shown in Table 1, the phase error term (13) is shown in Figure 4a. The phase error is unacceptable as it is much greater than the acceptable level $\pi /4$. It is obvious that the conventional SAR signal model is not suitable for SAA imaging configuration. The stop-and-go assumption is no long valid in SAIS configuration with acoustic source.
- (3)The third simulation experiment considers about the SAA signal model (5), where it is assumed that the time from the transmitter to the reflector equals to half of the round-trip delay, thus the matched filter is formulated as${F}_{\mathit{SAA}}\left({f}_{\tau},f,{r}_{0}\right)=exp\left\{j\left[\frac{4\pi {r}_{0}}{c}\sqrt{\alpha {\left({f}_{0}+f\right)}^{2}-\frac{1}{\alpha}{\left[\frac{v}{c}\left({f}_{0}+f\right)-\frac{c{f}_{\tau}}{2\alpha v}\right]}^{2}}-2\pi {f}_{\tau}\frac{f}{{K}_{r}}-4\pi \frac{{r}_{c}}{c}\left({f}_{\tau}+{f}_{0}+f\right)\right]\right\}$(16)

**Parameters of focused target under acoustic imaging system using different filters**

SAIS | SAR | SAA | ||||
---|---|---|---|---|---|---|

Azimuth | Range | Azimuth | Range | Azimuth | Range | |

IRW | 0.2 m | 0.17 m | 0.65 m | 0.44 m | 0.25 m | 0.21 m |

PSLR | −13.27 dB | −13.26 dB | −16.07 dB | −22 dB | −14.62 dB | −14.06 dB |

ISLR | −9.76 dB | −9.76 dB | −15.97 dB | −12.96 dB | −10.66 dB | −10.22 dB |

The focused result using the SAA matched filter (14) is shown in Figure 3e. The contour of the focused result is shown in Figure 3f for more detail. Parameters of the focused target are listed in Table 2, which also deviate from the theoretical values.

Figure 4b presents the phase error (15), which is not only much smaller than that of the conventional SAR model, but also greater than the acceptable level of $\pi /4$, proving that the SAA system signal model also do not express the signal of SAA imaging system well enough.

The simulation experiments proved the accuracy of the analytical FMCW SAIS in SAA imaging configuration, where the assumptions in traditional pulse SAR signal model seriously degrade the focusing performance, and the assumption in developing SAA model is not accurate enough.

### FMCW radar imaging

**Parameters of FMCW radar (broadside/high-squint)**

Parameters and requirements | Values |
---|---|

Azimuth Antenna length | 0.6 m |

Carrier frequency | 10 GHz |

Signal velocity | 3 × 0 |

Altitude | 800 m |

Platform velocity | 50 m/s |

PRF | 1000 Hz |

Range bandwidth | 500 MHz |

Squint angle | 0/60° |

Shortest slant range | 1100 m |

#### Case 1: broadside configuration

We design a broadside FMCW radar system following the parameters in Table 3, where the target is orthogonal to the flight direction. The theoretical resolutions are all 0.3 m in both range and azimuth directions. We also perform the three formulations of matched filtering function in the 2D frequency domain, i.e., $F\left({f}_{\tau},f,{r}_{0}\right)$, ${F}_{\mathit{SAR}}\left({f}_{\tau},f,{r}_{0}\right)$, and ${F}_{\mathit{SAA}}\left({f}_{\tau},f,{r}_{0}\right)$.

**Parameters of focused targets under broadside FMCW radar system using different filters**

SAIS | SAR | SAA | ||||
---|---|---|---|---|---|---|

Azimuth | Range | Azimuth | Range | Azimuth | Range | |

IRW | 0.29 m | 0.3 m | 0.31 m | 0.45 m | 0.3 m | 0.3 m |

PSLR | −13.26 dB | −13.26 dB | −13.01 dB | −18.06 dB | −13.26 dB | −13.27 dB |

ISLR | −9.76 dB | −9.75 dB | −10.28 dB | −14.66 dB | −9.75 dB | −9.76 dB |

Figure 5c shows the simulation result using the matched filter based on traditional SAR signal model, and Figure 5d shows its contour response. Table 4 shows its 2D measured parameters, which are far from the theoretical values.

Then, we apply the match filtering operation based on ${F}_{\mathit{SAA}}\left({f}_{\tau},f,{r}_{0}\right)$ in broadside FMCW configuration, and exhibit the simulation results in Figure 5e,f. The 2D measured parameters are listed in Table 4. The focusing performance does not show obvious difference from the result achieved by FMCW SAIS filtering, and the calculated parameters agree with the theoretical ones. The phase error expressed in (15) is presented in Figure 6, which is too small to affect the focusing performance.

From the simulation experiments above we note that the assumptions in traditional pulse SAR signal model causes great errors, but the assumption in developing SAA signal model is acceptable in broadside FMCW radar configuration.

#### Case 2: high-squint configuration

**Parameters of focused target under FMCW radar system with a 60° squint angle using different filters**

Filter | SAIS | SAR | SAA | |||
---|---|---|---|---|---|---|

Azimuth | Range | Azimuth | Range | Azimuth | Range | |

IRW | 0.6 m | 0.29 m | 0.96 m | 0.52 m | 0.72 | 0.35 |

PSLR | −13.29 dB | −13.27 dB | −19.51 dB | −19.66 dB | −14.38 dB | −14.35 dB |

ISLR | −9.77 dB | −9.76 dB | −16.02 dB | −15.84 dB | −10.93 dB | −10.82 dB |

Then, we verify the performance of conventional PTRS in high-squint FMCW radar system, and show the focused target in Figure 8c and its contour in Figure 8d, respectively. Figure 8d,e shows the focusing performance by applying the SAA-matched filtering function in FMCW radar system with a 60° squint angle. Measured parameters of the focused targets are shown in Table 5 for reference.

The focusing results show the failure of both conventional pulse SAR PTRS model and SAA signal PTRS model in characterizing high-squint FMCW radar signal spectrum, which could be forecasted by the value of phase error.

The simulation experiments show that the additional range–azimuth coupling components play an important role in high-squint FMCW radar cases. Neglecting the variation of the slant range during the long pulse duration will result in a significant degradation in the focusing performance.

## Conclusion

In this article, we validated the significance of the additional range–azimuth coupling term and range walk term in FMCW SAIS PTRS introduced by the variation of slant range during the long pulse durations, and proved the failure of the other two spectrum models in pulsed SAR and SAA imaging system under acoustic imaging system in FMCW configuration and high-squint angle FMCW radar imaging system. Simulation experiments are carried out concerning the acoustic source FMCW SAIS, the broadside FMCW radar, and high-squint FMCW radar cases. It needs to emphasize that the previous algorithms in [8–10] perform well in the broadside FMCW radar case but fail in acoustic imaging and high-squint FMCW radar cases.

Simulation experiments are carried out to validate the performances of different signal models and to analyze the accuracy of them. The analytical signal model works well under all of the aforementioned conditions, proving its capability as a general expression for FMCW SAIS systems with both acoustic source and electromagnetic wave. Simulation results show that the additional range–azimuth coupling components and range walk term play an important role under acoustic imaging and high-squint FMCW radar cases. Neglecting the range–azimuth coupling phase terms will result in a significant degradation in focusing performance.

## Declarations

### Acknowledgment

This work reported herein was jointly supported by the Hundred Talents Program of The Chinese Academy of Sciences and the General Program of National Natural Science Foundation of China under Grant 61172122.

## Authors’ Affiliations

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## Copyright

This article is published under license to BioMed Central Ltd. This is an Open Access article distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/2.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.