Abstract
The estimation of the direction of electromagnetic (EM) waves from a radio source using electrically short antennas is one of the challenging problems in the field of radio astronomy. In this paper we have developed an algorithm which performs better in direction and polarization estimations than the existing algorithms. Our proposed algorithm Snapshot Averaged Matrix Pencil Method (SAM) is a modification to the existing Matrix Pencil Method (MPM) based Direction of Arrival (DoA) algorithm. In general, MPM estimates DoA of the incoherent EM waves in the spectra using unitary transformations and least square method (LSM). Our proposed SAM modification is made in context to the proposed Space Electric and Magnetic Sensor (SEAMS) mission to study the radio universe below 16 MHz. SAM introduces a snapshot averaging method to improve the incoherent frequency estimation thereby improving the accuracy of DoA estimation. It can also detect polarization to differentiate between Right Hand Circular Polarlization (RHCP), Right Hand Elliptical Polarlization (RHEP), Left Hand Circular Polarlization (LHCP), Left Hand Elliptical Polarlization (LHEP) and Linear Polarlization (LP). This paper discusses the formalism of SAM and shows the initial results of a scaled version of a DoA experiment at a resonant frequency of \(\sim \)72 MHz.
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Notes
\(35.3^\circ \) is the angle between the each monopole and the ground plane. This is derived by equating all the direction cosines of the monopoles.
Here the coordinate setting is such that each orthogonal monopoles subtends an angle of \(35.3^\circ \) with the ground plane (x-y plane) and one can consider the new locations of the monopoles as the new local coordinates; then the relationship between the local and the reference coordinate is given by Eq. (8).
The SVR factor is the summation of the ratio between the consecutive values of the eigen values obtained from Singular value decomposition (SVD). This is a good measure to test the performance of the algorithm because the order of eigen values in the SVD are arranged from the most prominent feature in the signal to least prominent feature. If there are a few incoherent waves incident then the change observed in the consecutive eigen values will be abrupt or steep. If the ratio between the consecutive eigenvalues is high, it means that the signal can be detected easily.
The url - “https://drive.google.com/file/d/1lldWOl5q1jK_3br4wBW0qT0y9olMdE8q/view?usp=sharing" contains a video showing the phase shift in the received signal if the source is mobile.
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Acknowledgements
H.A.T. acknowledges the valuable discussions with Mr. Atharva Kulkarni (SPPU) regarding the SEAMS payload design and electronics and with Mr. Krishna Makhija (NRAO) regarding the CST simulations. Authors are thankful to Department of Electronic Science, SPPU (specially Prof D. Gharpure) for its support right from the beginning of this project (2017). Authors are thankful to the entire team of the SEAMS project. H.A.T. is thankful to Mr. Archisman Guha (IIT Indore) and Mr. Abhijeet Dutta (IIT Indore) for their support in DoA experiment. H.A.T. is thankful to research scholars Ms. Aishrila Majumder (IIT Indore), Ms. Deepthi Ayyagari (IIT Indore) and Mr. Sarvesh Mangla (IIT Indore) for their technical suggestions while drafting this manuscript. Authors also thank Dr. C. Bhatacharya for his critical comments.
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The corresponding author thanks Indian Institute of Technology Indore for providing Teaching Assistant-ship grant to pursue the research in the field of Low frequency Astronomy.
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In the initial stages of the work all authors contributed towards conceptualizing and formulation of the methodology and practical tests. The author Harsha Avinash Tanti contributed towards algorithm development, simulations, testing, and was a major contributor in writing the manuscript. Authors Abhirup Datta and S. Ananthakrishnan reviewed and revised the manuscript.
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Harsha Avinash Tanti, Abhirup Datta and S. Ananthakrishnan have contributed equally to this work.
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Appendices
Appendix A: Phase contamination by electronic components
In circuit theory any receiving antenna can be viewed as a independent voltage source with a source impedance called antenna impedance or radiation resistance [4]. Figure 15 is the circuit equivalent diagram of an receiving antenna with a load resistance of 50 \(\Omega \).
Since, the voltage received (\(V_{RX}\)) by the antenna is due to electric field of EM wave then, \(V_{RX}\,=\,h_{eff}\textbf{E}\) where \(h_{eff}\) is the effective height of the antenna and \(\textbf{E}\) is the electric field present in the EM wave. Using the plane wave consideration the electric field component can be written as \(\textbf{E}\,=\,E_0 e^{j(\textbf{k}\cdot \textbf{r} - \omega t)}\) here, \(\omega \,=\,2\pi f\). Thus, the voltage received can be written as following:
Using Eq. (A1) and circuit in Fig. 15 the received signal \(V_{out}\) can be written as
As impedance comprises of resistive (R) and reactive component thus antenna impedance can be written as \(Z_{ANT}\,=\,R_{ANT}+jX_{ANT}\). Considering the antenna impedance and Eq. (A2) on can observe analytically how phase is being modified due to the impedance in Eq. (A3).
In case of addition of several circuit components either in series or in parallel, the antenna impedance \(Z_{ANT}\) in Eq. (A3) has to be replaced by the effective impedance of the circuit also known as the Thevenin’s equivalent.
Appendix B: Matrix pencil method
The Matrix Pencil method is used to obtain the best estimates since it interacts directly with the data instead of generating a co-variance matrix, reducing computer complexity [48]. Eq. (6) is used to generate a Hankel matrix in order to estimate N and \(\omega ^n\).
where, L is selected between (M/3, M/2] for optimum performance and is known as the pencil parameter [37]; M is the total sample length. The real matrix(\(\Lambda _R\)) is computed using a Unitary matrix transformation [37] ( \(\Lambda _R = U^\dagger [\Lambda \mid \Pi _{M-L} \Lambda ^* \Pi _{L+1}]U\); where, \(^\dagger \) represents hermitian conjugate and U is the unitary matrix [23]) and the complex number matrix \(\Lambda \). Later, an estimate of the singular values of \(\Lambda _R\) is generated using SVD formulation. Matrix \(A_s\) consisting of N largest singular vectors of \(\Lambda _R\) is estimated by performing a thresholding operation on the normalized Eigen value i.e., \(\sigma _i/\sigma _{\max }\). N generalized singular values are then calculated using an unitary transformation (\(-[Re(U^\dagger J_1 U)A_s]^{-1}\cdot Im(U^\dagger J_1 U)A_s\)) which are, \(\psi _1, \psi _2,\cdots ,\psi _N\). Also, N incoherent frequencies are calculated by \(\omega ^n = 2arctan(\psi _n)/\delta \) for \(n = 1,2,\cdots ,N\) [21, 23, 40].
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Tanti, H.A., Datta, A. & Ananthakrishnan, S. Snapshot averaged Matrix Pencil Method (SAM) for direction of arrival estimation. Exp Astron 56, 267–292 (2023). https://doi.org/10.1007/s10686-023-09897-6
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DOI: https://doi.org/10.1007/s10686-023-09897-6