Selfcalibration method without joint iteration for distributed small satellite SAR systems
 Qing Xu^{1}Email author,
 Guisheng Liao^{1},
 Aifei Liu^{1} and
 Juan Zhang^{1}
https://doi.org/10.1186/16876180201331
© Xu et al.; licensee Springer. 2013
Received: 19 June 2012
Accepted: 7 December 2012
Published: 22 February 2013
Abstract
The performance of distributed small satellite synthetic aperture radar systems degrades significantly due to the unavoidable array errors, including gain, phase, and position errors, in real operating scenarios. In the conventional method proposed in (IEEE T Aero. Elec. Sys. 42:436–451, 2006), the spectrum components within one Doppler bin are considered as calibration sources. However, it is found in this article that the gain error estimation and the position error estimation in the conventional method can interact with each other. The conventional method may converge to suboptimal solutions in large position errors since it requires the joint iteration between gainphase error estimation and position error estimation. In addition, it is also found that phase errors can be estimated well regardless of position errors when the zero Doppler bin is chosen. In this article, we propose a method obtained by modifying the conventional one, based on these two observations. In this modified method, gain errors are firstly estimated and compensated, which eliminates the interaction between gain error estimation and position error estimation. Then, by using the zero Doppler bin data, the phase error estimation can be performed well independent of position errors. Finally, position errors are estimated based on the Taylorseries expansion. Meanwhile, the joint iteration between gainphase error estimation and position error estimation is not required. Therefore, the problem of suboptimal convergence, which occurs in the conventional method, can be avoided with low computational method. The modified method has merits of faster convergence and lower estimation error compared to the conventional one. Theoretical analysis and computer simulation results verified the effectiveness of the modified method.
Keywords
1. Introduction
With the development of spaceborne synthetic aperture radar (SAR) systems, the functions, such as SAR image, ground moving target indication (GMTI), and SAR interferometry (InSAR), have been well performed [1–4]. In the conventional spaceborne SAR systems, large antennas are required due to the minimum antenna area constraint [5]. However, it leads to the failure for the systems to obtain an image of wide area since the illumination area is inversely related to the aperture size of the antennas [6]. Distributed small satellite synthetic aperture radar (DSSSAR) systems [6–12] were developed to deal with the problem and have received considerable attention in recent years. In DSSSAR systems, several small satellites move in a special orbital configuration and function as a single “virtual satellite”. A small antenna covering wide area is placed on each satellite with the total antenna area constituted by all the small antennas satisfying the minimum antenna area requirement. Due to the flying formation of DSSSAR systems, alongtrack baselines and acrosstrack baselines may exist synchronously. And the acrosstrack baseline is needed for terrain height estimation [7] while the alongtrack baseline is suitable for the function of SAR and GMTI [8]. In [9], the SAR train configuration is analyzed and many scholars focus their attention on SAR imaging or GMTI based on this configuration [10, 11]. However, for the echo received by each small satellite, range or azimuth (Doppler) ambiguities will occur due to the use of small antennas. In order to image a wide swath unambiguously, the echoes of small antennas should be combined coherently in the DSSSAR system. In [10, 11], the low pulse repetition frequency (PRF) is chosen to avoid range ambiguity which results in Doppler ambiguity, and the approaches are also given to suppress Doppler ambiguity. However, their excellent performance is critically dependent on the knowledge of the array manifold (parameterized by many parameters, such as angle of arrivals, and antennas’ position information). The array manifold is used in coherent combination of small antennas’ echoes to suppress Doppler ambiguity [10]. In practice, there always exist various perturbations in the array manifold which are always called as array errors, such as gain, phase, and position errors. Since the array manifold cannot be exactly obtained because of the existence of array errors, the performance of Doppler ambiguity suppression [11, 12] can significantly be degraded. Therefore, it is necessary to estimate and calibrate array errors prior to carry out Doppler ambiguity suppression. In [12], the array error calibration method has also been discussed.In array error estimation of DSSSAR systems, the existing array calibration methods [13–18] can be applied to the systems only when proper calibration sources are chosen. In [12], spectrum components within one Doppler bin are used as calibration sources with known directions which are called “virtual calibration sources.” Since the number of spectrum components is more than one due to Doppler ambiguity, it is possible to apply array calibration methods with more than one calibration source [15–18] to DSSSAR systems. In [12], a twostep iterative autocalibration method is presented to estimate gainphase and position errors. In the first step, assuming that position errors are known, gainphase errors are estimated by using the method in [16]. In the second step, based on the gainphase error estimated in the former step, position errors can be obtained by the least squared method [17]. These two steps should be iterated alternatively to obtain final solutions. For convenience, the array error estimation method in [12] is named as the conventional method (the comparison in this article is limited in terms of array error estimation method).
In the conventional method, two kinds of errors, the gainphase error and the position error, are respectively estimated under the assumption that other kinds of errors are known. The inherent relationship among gain, phase, and position errors is not considered and analyzed in the conventional method. In this article, by studying of the conventional method, the following two aspects are observed. First, gain error estimation and position error estimation can affect each other, which will influence the convergence rate. And the conventional method may even suffer from suboptimal convergence in large position errors. Second, if spectrum components within the zero Doppler bin are used as calibration sources to estimate the errors, phase error estimation can be performed independent of position errors. Based on the above two aspects, a modified array error estimation method is proposed in this article. First, in order to eliminate the interaction between the gain and position error estimations, gain errors are first estimated and compensated. Then, phase errors are estimated by using the spectrum components within the zero Doppler bin as calibration sources. Finally, position errors are estimated based on Taylorseries expansion. However, since Taylorseries expansion causes approximation errors, position error estimation should be iterated in order to obtain higher estimation accuracy. In comparison with the conventional method, the modified method can avoid the iteration between gainphase error estimation and position error estimation, which guarantees that it can converge to optimal solutions with lower computational load and fast convergence speed. Simulation results verify that the modified method performs better than the conventional one.
The remainder of the article is arranged as follows. In Section 2, the modified method for DSSSAR systems is described in detail. The performance of the modified method is verified by using Monte Carlo simulations in Section 3. The article ends with some conclusions given in Section 4.
2. Modified method for DSSSAR systems
2.1. Signal model
Since Δy _{ m }cosθ(τ, f _{ d })sinϕ(τ) and Δz _{ m }cosϕ(τ) can be neglected in r _{ m }(x, y, z, f _{ d }), it can be obtained that r _{1}(x, y, z, f _{ d }) ≈ ⋯ ≈ r _{ M }(x, y, z, f _{ d }) ≜ r(x, y, z, f _{ d }). So, as H _{1}(τ, f _{ d }) ≈ ⋯ ≈ H _{ M }(τ, f _{ d }) ≜ H(τ, f _{ d }).
where S = [S _{1},…, S _{ M }]^{ T }, $\mathbf{\Gamma}=\mathrm{diag}\left\{1,\dots ,{g}_{M}{e}^{j{{\xi}^{\prime}}_{M}}\right\}$, A = [a ^{−I },…,a ^{ I }], ${\mathbf{a}}^{i}={\left[1,\dots ,{e}^{j\frac{4\pi}{\lambda}{{d}^{\prime}}_{M}^{i}}\right]}^{T},$ H = [H ^{−I },…,H ^{ I }]^{ T }, ( • )^{ T } denotes the transpose operation.
The covariance matrix of S is denoted as R _{ SS }. Denote eigenvalues and corresponding eigenvectors of the covariance matrix R _{ SS } with ƛ _{ m } (listed in descending order) and u _{ m } (m = 1,…, M). Each column of ΓA is orthogonal to the matrix U = [u _{2I+2},…,u _{ M }]. And the orthogonality can be used to estimate the gainphase and position errors.
2.2. The conventional method
where real (•) takes the real part of the matrix. The phase error introduced by Taylorseries expansion above is within 4° at Xband under the assumption that Δx _{ m } ≤ 20 cm. And higher accuracy can be achieved after several iterations. However, from computer simulations, it is found that if Δx _{ m } > 30 cm, the estimate difference of position errors will be larger than 0.008 m. The conventional method can be summarized as joint iteration between the following two steps.

Step 1 Choose some Doppler bin to obtain gainphase errors based on (10).

Step 2 Estimate position errors based on (20) and compensate x _{ mo } by Δx _{ m }.
2.3. Formulation of the modified method
Lets consider the gain error estimation of the conventional method.
where g = [1, g _{2},…,g _{ M }]^{ T }, abs (•) denotes the complex modulus of the elements of a matrix. The gain error estimate, ĝ, will be inaccurate because of the existence of the position error ΔX (derived by Q). Moreover, the estimation differences of gain errors will be larger with the increase of position errors.
where ρ = [ρ _{1}, …, ρ _{ M }]^{ T } and η = [η _{1}, …, η _{ M }]^{ T } denote the amplitude and phase of ${\tilde{a}}^{i}$, respectively.
where $\widehat{{g}_{k}}$ and Δg _{ k } denote estimated values and differences of gain errors, $\widehat{{{\xi}^{\prime}}_{k}}$ and Δξ ^{′} _{ k } represent estimated values and differences of phase errors, respectively. Then $\widehat{{\rho}_{k}}={\rho}_{k}\left(\widehat{{g}_{k}},+,\Delta ,{g}_{k}\right)/\widehat{{g}_{k}}$ and $\widehat{{\eta}_{k}}={\eta}_{k}+\Delta {{\xi}^{\prime}}_{k}$ instead of ρ _{ k } and η _{ k } will be obtained if (29) is used to estimate position errors. Thus, Δg _{ k } will affect the position error estimation accuracy. Considering the fact that position errors have an effect on the gain error estimation during the first step while gain errors affect position error estimation during the second step, estimating differences of gain and position errors using (27) and (20) iteratively in the conventional method could converge to suboptimal solutions in large position errors.
where P is the number of Doppler bins, σ _{ n } ^{2} can be obtained by averaging ƛ _{2I+2} to ƛ _{ M }.
After estimating gain errors, phase and position error estimations will be considered in the following. The conventional method requires joint iteration between phase and position error estimations. Through the following study, the joint iteration is avoided in the modified method.
where $\widehat{{\xi}^{\prime}}={\left[{{\xi}^{\prime}}_{1},{{\xi}^{\prime}}_{2},\dots ,{{\xi}^{\prime}}_{M}\right]}^{T}$, angle(·) returns the phase angles of a matrix. This result is consistent with the phenomenon mentioned in [12] that when f _{ d } = 0 is chosen, the estimation accuracy of phase errors can be satisfactory with position errors assumed to be zero. Since Δξ ^{′} _{ k } is induced without the effect of position errors, we do not discuss the influence of Δξ ^{′} _{ k } on the estimation of the position error, ΔX, described by (30).
Based on the analysis above, the modified method can be summarized as follows.

Step 1 Estimate gain errors based on (31) and compensate the received data using estimated gain errors.

Step 2 Choose the zero Doppler bin to obtain phase error estimate $\widehat{{\xi}^{\prime}}$ based on (35).

Step 3 Use $\widehat{{\xi}^{\prime}}$ to reconstruct $\tilde{\Gamma}=\mathrm{diag}\left\{{e}^{j\widehat{{\xi}^{\prime}}}\right\}$ and estimate position errors based on (20).
Through the analysis above, phase error estimation method can perform robustly with the existence of position errors. Since the Taylorseries expansion is used in estimating position errors, Step 3 should be applied repeatedly in order to obtain higher estimation accuracy with x _{ mo } compensated by Δx _{ m } (which is estimated in the former iteration) in each iteration.
In the modified method, gain errors are compensated first, hence the relationship between gain and position error estimations is eliminated, which guarantees the estimation accuracy.
The change on the iterative fashion makes it possible for the modified method to work with less computational load. Let L denote the iteration number for the conventional method, the computational load is 3LM ^{3} which mainly arises from the matrix eigendecomposition (equals M ^{3}) and the matrix inversion (equals M ^{3}). However, the computational load of the modified method is 2 M ^{3} + L ^{′} M ^{3} in which L ^{′} denotes the iteration number of Step 3. From the computer simulations, we find that the estimates of the gain, phase, and position errors through the conventional method do not converge to the final solutions even when L equals to be 10 and the zero Doppler bin is chosen. And for the modified method, L ^{′} should be more than two to satisfy the estimation accuracy. For example, based on the assumptions that L = 10 and L ^{′} = 3, the computational load of the modified algorithm is 5 M ^{3}, which is lower than that of the conventional method (30 M ^{3}).
3. Simulation experiment
Simulation parameters of DSSSAR systems
Orbit altitude  750 km 
Incidence angle  45° 
Band  Xband 
Antenna size  2 m × 1 m 
Bandwidth  100 MHz 
PRF  1496 Hz 
Velocity  7481.5 m/s 
3.1. Effect of SNR
3.2. Effect of gain errors
3.3. Effect of position errors
3.4. Effect of iterations
For the modified method, only the position error estimate ARMSE versus the number of iterations is shown in Figure 5c since only the position error estimation is iterated in the modified method. It is noticed from Figure 5c that the position error estimation converges to the optimal solution with less than three iterations. To sum up, the computational load of the modified method is less than that of the conventional method. Meanwhile better performance can be obtained by the modified method.
4. Conclusions
In this study, we focus on gain, phase, and position error estimations of DSSSAR systems. Based on the conventional method, a modified array error estimation method is proposed here. In the conventional method, the estimation of gain and position errors may converge to suboptimal solutions especially when position errors are large and the joint iteration between the gainphase and position error estimations are needed. That is because of the interaction between the estimations of gain and position errors. In the modified method, gain errors are first estimated and compensated before the other errors’ estimation, which guarantees the position error estimation accuracy to be higher than that in the conventional method. Meanwhile, by using the zero Doppler bin data, the phase error estimation can behave independently of position errors. Then the joint iteration strategy between the gainphase and position error estimations in the conventional method can be avoided, which makes the modified method perform stably with low computational load. Theoretical analysis and simulation results demonstrate the effectiveness of the modified method.
Declarations
Acknowledgment
The authors would like to thank the anonymous reviewers for their constructive comments, which led to significant improvements in this study. Special thanks to Dr. Yinghua Wang and Xuefeng Zheng for improving the English usage and also for their valuable suggestions. This study was sponsored in part by the National Basic Research Program of China (973 Program) under Grant no. 2011CB707001, in part by the Natural Science Foundation of China under Grant no. 61101242, in part by the Fundamental Research Funds for the Central Universities under Grant no. K50511020009, and in part by the Program for Changjiang Scholars and Innovative Research Team in University under Grant no. IRT0954.
Authors’ Affiliations
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