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Constant rank factorisations of smooth maps, with applications to sonar

Published online by Cambridge University Press:  01 December 2022

Michael Robinson*
Affiliation:
Mathematics and Statistics, American University, Washington, DC 20016, USA
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Abstract

Sonar systems are frequently used to classify objects at a distance by using the structure of the echoes of acoustic waves as a proxy for the object’s shape and composition. Traditional synthetic aperture processing is highly effective in solving classification problems when the conditions are favourable but relies on accurate knowledge of the sensor’s trajectory relative to the object being measured. This article provides several new theoretical tools that decouple object classification performance from trajectory estimation in synthetic aperture sonar processing. The key insight is that decoupling the trajectory from classification-relevant information involves factoring a function into the composition of two functions. The article presents several new general topological invariants for smooth functions based on their factorisations over function composition. These invariants specialise to the case when a sonar platform trajectory is deformed by a non-small perturbation. The mathematical results exhibited in this article apply well beyond sonar classification problems. This article is written in a way that supports full mathematical generality.

Information

Type
Papers
Creative Commons
Creative Common License - CCCreative Common License - BY
This is an Open Access article, distributed under the terms of the Creative Commons Attribution licence (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted re-use, distribution and reproduction, provided the original article is properly cited.
Copyright
© The Author(s), 2022. Published by Cambridge University Press
Figure 0

Figure 1. General CSAS collection geometry wherein the sensor platform orbits a target, where one scatterer’s position has been highlighted.

Figure 1

Figure 2. Two simple composite scatterers (a) one with 2-fold symmetry and (b) one with 3-fold symmetry.

Figure 2

Figure 3. Signatures of the composite scatterers shown in Figure 2 (a) has 2-fold symmetry and (b) has 3-fold symmetry.

Figure 3

Figure 4. Signatures of the composite scatterers with trajectory distortions over a single orbit of the target; after removing distortions (a) has 3-fold symmetry and (b) has 5-fold symmetry.

Figure 4

Figure 5. Combined scatterer with $P=2$, $Q=3$, and relative angle $\beta = 28^\circ$ shown.

Figure 5

Figure 6. A typical signature of the sum of the two scatters shown in Figure 5, where $P=2$, $Q=3$, and the relative angle is $\beta=28^\circ$.

Figure 6

Figure 7. Response as a function of scatterer angles at (a) 300 Hz and (b) 600 Hz.

Figure 7

Figure 8. Extracted single-frequency response with a constant relative angle ($28^\circ$) between scatterers at 300 Hz.

Figure 8

Figure 9. Single-frequency response with a constant relative angle ($28^\circ$) as a torus knot at (a) 300 Hz, (b) 600 Hz.

Figure 9

Figure 10. (a) Signature of the sum of a 4-fold symmetric scatterer and a 6-fold scatterer, (b) Response as a function of scatterer angles at 300 Hz.

Figure 10

Figure 11. Principal components analysis plots of the signature of (a) a 3-fold symmetric scatterer (Figure 3(b)) and (b) a distorted 3-fold symmetric scatterer (Figure 4(a)).

Figure 11

Figure 12. Different responses at 300 Hz for (a) the (2, 3) torus knot signature with relative angle $28^\circ$, (b) the (2, 3) torus knot signature with relative angle $100^\circ$, and (c) the (2, 5) torus knot signature with relative angle $28^\circ$.