2201.01461v2

Model: nemotron-free

# Towards Maximizing a Perceptual Sweet Spot **Authors**: Pedro Izquierdo Lehmann, Rodrigo F. Cadiz, Carlos A. Sing Long ## TOWARDS MAXIMIZING A PERCEPTUAL SWEET SPOT PREPRINT ## Pedro Izquierdo Lehmann Rodrigo F. Cádiz Institute for Mathematical and Computational Engineering Pontificia Universidad Católica de Chile pizquierdo2@uc.cl Department of Electrical Engineering and Music Institute Pontificia Universidad Católica de Chile rcadiz@uc.cl ## Carlos A. Sing Long ∗ Institute for Mathematical and Computational Engineering and Institute for Biological and Medical Enginering Pontificia Universidad Católica de Chile casinglo@uc.cl May 5, 2022 ## ABSTRACT The sweet spot can be interpreted as the region where acoustic sources create a spatial auditory illusion. We study the problem of maximizing this sweet spot when reproducing a desired sound wave using an array of loudspeakers. To achieve this, we introduce a theoretical framework for spatial sound perception that can be used to define a sweet spot, and we develop a method that aims to generate a sound wave that directly maximizes the sweet spot defined by a model within this framework. Our method aims to incorporate perceptual principles from the onset and is flexible: while it imposes little to no constraints on the regions of interest, the arrangement of loudspeakers or their radiation pattern, it allows for audio perception models that include state-of-the-art monaural perceptual models. Proof-of-concept experiments show that our method outperforms state-of-the-art methods when comparing them in terms of their localization and coloration properties. Keywords Spatial sound · sound field reconstruction · psychoacoustics · sweet spot · applied functional analysis · non-convex optimization · DC optimization ## 1 Introduction The field of spatial sound addresses the question: how do we create a desired spatial auditory illusion over a spatial region of interest with a set of acoustic sources? [1, Chapter 2.3]. The spatial auditory illusion (SAI) occurs when acoustic sources create a sound scene that produces a desired auditory scene over a region. It is related to sound quality as described by Wierstof et al [2, Chapter 2]: 'The quality of a system as perceived by a listener is considered to be the result of assessing perceived features with regard to the desired features (of the auditory scene). ' Following Blauert, the sound scene represents the objective nature of a sound wave propagating in the physical world, whereas the auditory scene represents the imprint of the sound scene in our subjectivity, that is, the result of the auditory system perceiving and organizing sound into meaning [3]. Over the last century, several methods have been proposed to answer this. Their performance can be compared in terms of the size of the region where the SAI is achieved. In this work, we call this region the sweet spot . ∗ C. A. Sing Long is also with ANID - Millennium Science Initiative Program - Millennium Nucleus Center for the Discovery of Structures in Complex Data, and with ANID - Millennium Science Initiative Program - Millennium Nucleus Center for Cardiovascular Magnetic Resonance. The term sweet spot is already used in panning and surround systems to describe an ideal listening position that is equally distant to all loudspeakers [4] and around which there is a limited area where a desired wavefront is correctly recreated [1, Chapter 3.1], [5]. It is also used to mean the 'area in which the spatial perception of the auditory scene works without considerable impairments' [6, Chapter 1.2]. Furthermore, in [7] the sweet area is defined as the 'area within which the reproduced sound scene is perceived as plausible, ' where plausible means the preservation of front localization and envelopment of reverberation. Our use of the term is in the spirit of the second and third ideas. One of the earlier and most widespread spatial sound approaches is stereophony and its generalizations, sourround systems [8] and Vector Base Amplitude Panning (VBAP) [9]. These methods, also called panning techniques , adjust the level and time-delay of the audio signals for each speaker utilizing a panning law to simulate steering the perceived direction of the sound source. The possibility of this steering has been explained by the perceptual idea of summing localization and by the association model [1, Chapter 6.1]. Moreover, due to some psycho-acoustic features of the auditory system, such as the binaural decoloration mechanism, they work sufficiently well in some applications, even with few speakers [4]; they do not suffer from coloration [10]. However, they can only simulate sound sources that lay on the segments that join the speakers. Furthermore, its quality degrades rapidly as the listener moves away from the center of the target region [4]. A popular strategy to recreate an auditory scene is to directly approximate the sound wave that created it. In the literature, this strategy is called sound field synthesis , sound field reproduction or sound field reconstruction . Following Huygens' principle [11], any sound scene can be approximated accurately with a sufficiently dense arrangement of loudspeakers. However, in practice there is only a limited number of them. Three classes of commonly used methods for sound field reconstruction are mode matching methods , pressure matching methods and wave field synthesis . Mode Matching Methods (MMM) match the coefficients in the expansion of the target and generated sound waves in spatial spherical harmonics [12]. Some well-known MMMs are Ambisonics [13], Higher-Order Ambisonics (HOA), and Near-Field Compensated Ambisonics (NFC-HOA) [14]. All of them minimize the 2 -norm of the difference between the leading coefficients. Ambisonics assumes the loudspeakers emit plane waves and uses only the leading coefficient, whereas HOA uses a larger but fixed number of coefficients. In contrast, NFC-HOA assumes the loudspeakers are monopoles. Ambisonics, HOA and NFC-HOA are designed for circular or spherical regions of interest. When approximating a plane wave, they create a central spherical region with a radius that is inversely proportional to the frequency of the source over which the sound scene is reconstructed almost identically [15]. Some variations of these methods consider a weighted mode matching problem to prioritize certain spatial regions [16], a mixed pressure-velocity mode matching problem [17], and an intensity mode matching problem [18]. Instead of using expansions in spatial spherical harmonics, Pressure Matching Methods (PMM) minimize the spatiotemporal L 2 -error between the the target and generated sound waves [19]. The magnitude of the audio signals are often penalized by their L p -norm to mitigate the effects of ill-conditioning [20, 21, 22, 23] and to enforce sparse representations [24, 25]. Typically the loudspeakers are modeled as monopoles. In most cases, the solution can only be found numerically, and the discretization of the region of interest plays an important role [26, 27]. Variations considering a mixed pressure-velocity pressure matching problem have been considered [28, 29, 30]. Finally, Wave Field Synthesis (WFS) leverages the single-layer boundary integral representation of a sound wave over a region of interest [4]. Traditional WFS [31] uses a Rayleigh integral representation to derive a solution when the speakers are modeled as dipoles lying on a line. This was later extended to monopoles [32] for 2.5D reproduction. Its reformulation, Revisited WFS [33], uses a Kirchhoff-Helmholtz integral representation along with a Neumann boundary condition to obtain a solution for an arbitrary distribution of monopoles. It has been shown that the localization properties of the auditory scene are correctly simulated by WFS and do not depend on the position of the listener over the region of interest [34]. However, this technique suffers from coloration effects due to spatial aliasing artifacts [35]. There is extensive literature analyzing these methods and comparing their performance [14, 36, 37, 38, 39], they become equivalent in the limit of a continuum of loudspeakers, differing only when using a finite number [40] of them. Although they are amenable to mathematical analysis and have computationally efficient implementations, their construction has no natural perceptual justification to produce a large sweet spot. As a consequence, the artifacts introduced by these methods, due to approximation errors, may produce noticeable, and possibly avoidable, perceptual artifacts. An alternative to better reproduce the auditory scene is to explicitly account for psycho-acoustic and perceptual principles in the reconstruction methods [6]. The first steps in this direction were taken in [41] by proposing a simple model that aims to preserve the spatial properties of the desired auditory scene. A method to reproduce an active intensity field that is largely uniform in space was then proposed in [42]. It is based on an optimization problem yielding audio signals where at most two loudspeakers are active simultaneously. However, it makes the restrictive assumption that the target sound wave is a plane wave, and that the loudspeakers emit plane waves. In [43] the radiation method and the precedence fade are proposed. The former is equivalent to applying a PMM over a selection of frequencies that are most relevant psycho-acoustically, whereas the latter is a method to overcome the localization problems associated to the precedence effect [44]. Finally, in [45] a PMM is extended to account for psycho-acoustic effects by considering the L 2 -norm of the differences in pressure convolved in time by a suitable filter. We believe that there is a gap between methods that aim to directly approximate a sound wave to reproduce a desired auditory scene, and methods that leverage perceptual models to reproduce the same auditory scene. Defining the sweet spot requires a model, either theoretical or empirical, of audio perception. In this work, we introduce theoretical framework for for spatial audio perception, and we develop a method to maximize the sweet spot defined by a model within this framework. Our method is amenable to mathematical analysis, it has an efficient computational implementation, and is guided by perceptual principles. Our numerical results show that our method outperforms some state-of-the-art methods for sound field reconstruction. The paper is organized as follows. In Section 2 we introduce the physical assumptions we make, and a theoretical framework for spatial audio perception, deferring to Appendix A the technical details. Then, in Section 3 we introduce an intuitive and readily implementable instance of our method to maximize the sweet spot defined by a model within this framework. In Section 4 we discuss the psycho-acoustic concepts that, to our knowledge, can be incorporated in the theoretical framework. In Section 5 we present an implementation of our method. In Section 6 we perform proof-of-concept numerical experiments analyzing the performance of our method, comparing its results with WFS, NFC-HOA and PMM. Finally, in Section 7 we discuss our results, the limitations of our method, and some future lines of research. ## 2 Spatial Sound Mathematical Framework ## 2.1 Acoustic framework Consider n s loudspeakers located at positions x 1 , . . . , x n s ∈ R 3 . When the medium is homogeneous and isotropic, and each loudspeaker behaves as an isotropic point source, the physical sound wave u they generate is represented in frequency as [46, Section 2.5.2]  where c s is the speed of sound, c 1 , . . . , c n s are the audio signals driving each loudspeaker, and ̂ c k is the Fourier transform of c k in time  To model the spatial radiation pattern of each loudspeaker, along with time-invariant effects such as reverb [20, 47], we may use  where G k is the Green function of the k -th loudspeaker. In addition to the array, we consider a region of interest Ω ⊂ R 3 such that x k / ∈ Ω ; thus, it contains no singularity in (1). On this region, we may approximate a sound wave u 0 with the array of loudspeakers as best as possible . If we had a continuum of isotropic point sources on ∂ Ω then, under suitable conditions, the simple source formulation [48, Section 8.7] shows we can reproduce u 0 exactly . However, when only a finite number of physical loudspeakers are available, we must find ̂ c 1 , . . . , ̂ c n s such that  in an suitable sense for x ∈ Ω . When each G k is real-analytic on its second argument the approximation cannot be exact on any open set unless u 0 was actually generated by the speaker array [49, Corollary 1.2.5]. This suggests that perfect sound field reconstruction is impossible, and that the difference can be small only on average. In spite of this, in some subset of Ω the approximation can be perceptually accurate. ## 2.2 Perceptual framework The comparison in (3) is between two physical quantities. To incorporate perceptual effects, we formally introduce a theoretical framework and defer the mathematical details to Appendix A.1. The perception of an individual located at x ∈ Ω and looking in the direction represented by a unit vector θ in R 3 (or an angle in R 2 ) depends on the relation between the sound wave at the left and right ears. Hence, we consider pairs of signals u , u r so that u s = u s ( t, x, θ ) represents the wave that reaches the ear s of a listener located at x and looking in the direction θ at time t . We let u s ( x,θ ) represent the signal at ear s . From now on, let ¯ u be this vector signal, and let W be the space of all such signals. Instead of (2) we consider  where H s k is the head-related transfer function [3] associating to a wave emitted by the k -th loudspeaker the sound wave reaching the ear s ; this comprises the behavior of the loudspeakers. From now on, we let W S be the set of all pairs of signals generated by model (4). Therefore, the problem is to approximate the fixed target signal ¯ u 0 associated to the sound wave u 0 by a signal ¯ u represented as (4) that is perceptually close to ¯ u 0 . To model the perceptual dissimilarity we introduce a map D that associates to a pair ¯ u, ¯ u 0 the function D (¯ u, ¯ u 0 ) = D (¯ u, ¯ u 0 ) ( x, θ ) that quantifies the dissimilarity between the signals ¯ u and ¯ u 0 perceived by a listener located at x and looking in the direction θ . We do not make strong assumptions on D except that it is convex : for ¯ u 1 , ¯ u 2 we have  for any λ ∈ [0 , 1] . We assume the dissimilarity is negligible if D (¯ u, ¯ u 0 ) ( x, θ ) ≤ 0 . Depending on the application, this may be interpreted as authenticity , i.e., ¯ u is indiscernible from ¯ u 0 , or as plausibility , i.e., some perceived features of ¯ u and ¯ u 0 show a context-reasonable correspondence [2, Chapter 2]. In Section 4 we discuss some functional forms for D . Suppose the listeners can look only along some directions of interest Θ . We define the auditory illusion threshold as  A listener located at x will perceive no noticeable differences between ¯ u and ¯ u 0 regardless of the direction she is looking if T ¯ u ( x ) ≤ 0 . Hence, the sweet spot  is the region within Ω where a listener does not perceive significant differences between ¯ u and ¯ u 0 . We define a loudness discomfort threshold similarly: we assume there is a function L that associates to ¯ u the function L ¯ u = L ¯ u ( x, θ ) quantifying the loudness discomfort experienced by a listener at a location x looking in a direction θ . We also assume L satisfies (5) and we define the the loudness discomfort threshold T L ¯ u ( x ) := sup θ ∈ Θ We assume that T L ¯ u ( x ) ≤ 0 when no discomfort is experienced. Hence, to avoid choosing a signal ¯ u that causes discomfort, we restrict our choices to  Consequenty, our goal is to find a signal ¯ u ∈ W S that maximize the weighted area of the sweet spot µ ( S (¯ u )) while causing no discomfort by solving  L ¯ u ( x, θ ) . ## 3 The SWEET-ReLU method We introduce a particular instance of our method to approximately solve ( P 0 ) that is applicable in practice and has an intuitive interpretation. We defer the analysis of our general method to Appendix A. Let h : R → R be the Heaviside function, i.e., h ( t ) = 0 if t < 0 and h ( t ) = 1 if t ≥ 0 . Observe that  Maximizing µ ( S (¯ u )) implies minimizing the second term. This is challenging due to h being piecewise constant. For ε > 0 we can approximate it by a piecewise linear function ˜ h : R → R such that ˜ h ( t ) = 0 for t < 0 , ˜ h ( t ) = t for ## Algorithm 1: SWEET-ReLU ``` ``` t ∈ [0 , 1] and ˜ h ( t ) = 1 for t > 1 . For ε > 0 let ˜ h ε ( t ) = ˜ h ( t/ε ) and let ¯ u 1 ∈ W S be arbitrary. We can minimize the approximation  where ( u ) + = max { 0 , u } . We interpret the first integral as the contribution from the region where we may change ¯ u 1 to decrease the auditory illusion threshold, whereas we interpret the second as the contribution of the region over which it is already too large. Thus, we proceed in a greedy manner: we let Ω 1 = Ω , and then, at the k -th iteration, we define   and solve to obtain ¯ u k +1 . The above problem is convex, whence ¯ u k +1 can be found using efficient algorithms. The sequence { ¯ u k } k ∈ N has at least one accumulation point, which approximates the solution to ( P 0 ) . Once the sequence has converged, we can repeat the procedure for a smaller value of ε . As the intuition behind our method suggests choosing a ¯ u 1 for which T D ¯ u 1 ≡ 0 , e.g. ¯ u 1 = ¯ u 0 , we simply choose Ω 1 = Ω in practice. By running the algorithm for increasingly smaller values of ε we obtain an increasingly accurate approximation to a solution to ( P 0 ) . We call this instance of our method SWEET-ReLU (Algorithm 1). We defer a justification of these facts to Appendix A and the deduction of this instance to Appendix A.5. ## 4 Perceptual and psycho-acoustic theory The theoretical framework introduced aims to be flexible enough to account for a variety of perceptual and psychoacoustic models. We now present some of the perceptual and psycho-acoustic considerations that lead to models within this framework. The spatial auditory illusion (SAI) is achieved when the imprint of the reproduced sound scene on a listener resembles a desired auditory scene. The formation of the auditory scene depends not only on the signals reaching the listener's ears but both on the listener itself [50]. Also, it may even be influenced by external visual, tactile, and proprioreceptive stimuli [51]. Formulating a model accounting for all these effects goes beyond the scope of this work. Instead, we focus on proposing maps D and L representative of an average listener or worst-case listener , and motivated by the concept of auditory event , which is only related to the perceptual processing of the ear signals. The auditory scene is then regarded as the integration of different and separable auditory events. The process of extracting auditory events from ear signals has been studied in the field of auditory scene analysis (ASA) [52, 50]. Although the psycho-acoustic and cognitive mechanisms involved are the focus of current research [1, Chapter 2.1], the quantitative modeling of the process has been carried out by the field of computational auditory scene analysis (CASA) [53]. The analysis of auditory scenes is a combination of bottom-up, or signal driven , and top-down, or hypothesis driven , processes [54]. In the former, the physical properties of the input signal, which are processed at the peripheral auditory system, serve as a basis for the formation of auditory events and are summarized under primitive grouping cues [52]. In the top-down process higher cognitive processes such as prior knowledge turn into play to determine which signal components the listeners attend to and how these components are assembled and recognized, involving processes that are referred to as schema-based cues [52]. Although a complete model of auditory events formation should also consider top-down processes, for simplicity we focus only on primitive grouping cues. These allow us to compare ¯ u ( x,θ ) and ¯ u 0 , ( x,θ ) by accounting mostly for the immediate psycho-acoustic peripheral processing. The direct comparison between the auditory scene generated by ¯ u and ¯ u 0 leads to the full reference (FR) model . In contrast, in the internal references (IR) model the auditory scene is compared to abstract representations in the listener's memory [55, Chapter 2.6]. Although FR models have been shown to have limitations [56], e.g., it is not always clear which binaural input signal is related to what the listener really desires to hear, we focus exclusively on them for simplicity. Otherwise schema based cues would be needed. Spatial sound applications identify the most important features [2, Chapter 2] of the auditory scene in a multidimensional approach [55, Chapter 3.2]. In Letowski's simple model [57], the auditory scene is described in terms of 'loudness, pitch, (apparent) duration, spatial character (spaciousness), and timbre. ' The last two are selected as the more important for spatial sound applications. The analysis of the most important features for spatial sound applications has been recently refined in [58, 59], once again calling attention to timbral and spatial features. More specifically, azimuth localization and coloration are widely used features for the perceptual assessment of multi-channel reproduction systems [6, 10, 35]. Motivated by these studies, we focus on models that account only for coloration and azimuth localization. The trade-off is that these models can, at best, account for plausibility of the SAI, more than authenticity . Since the detailed biophysics of the phenomena are not necessary to model an accurate input-output relation, we only consider functional (phenomenological) models instead of physiological (biophysical) ones [60, Chapter 1.2]. ## 4.1 Binaural Azimuth Localization Azimuth localization is the estimation of the direction of arrival of the incoming sound in the horizontal plane. In concordance with Lord Rayleigh's duplex theory [61], the literature shows that interaural time differences (ITDs) are the primary azimuth localization cue at low frequencies [62] whereas interaural level differences (ILDs) become relevant at high frequencies as to resolve ambiguities in the decoding of ITDs [63] which appear over 1.4 kHz [64]. Consequently, binaural models, i.e., models that use both the right and the left ear signals as inputs, are crucial, and most of these models for azimuth localization focus on the extraction of the ITDs. The cross-correlation between the left and right ear signals [65] is usually used to model the mechanism for extraction of the ITDs, e.g. [66, 67, 68, 69, 70] and azimuth localization. Other models [63, 71] have appeared after the cross-correlation model was challenged by physiological findings [72]. Unfortunately, the extraction of the ITDs using cross-correlation (or as in [63, 71]) and the extraction of ILDs, lead to dissimilarity maps D that do not satisfy (5). ## 4.2 Binaural Coloration Coloration is commonly defined as timbre distortion [35], [1, Chapter 8.1] where timbre is the property that 'enables the listener to judge that two sounds which have, but do not have to have, the same spaciousness, loudness, pitch, and duration are dissimilar' [57]. Although timbre could be quantified in a spectro-temporal space, the metric of the timbral space is not known and could be non-trivial [35]. Binaural perceptual effects such as binaural unmasking, spatial release from masking [73], and binaural decoloration [74], allow the auditory system to improve the quality of the perceived sound in terms of signal-to-noise ratio (SNR) identifiability and coloration. Even though these effects make defining an accurate binaural metric even more challenging, binaural detection and masking models have been developed in the literature [75]. They can be used to detect binaural timbral differences, and have been adapted to account for localization cues [76]. Furthermore, a model accounting for binaural perceptual attributes, such as coloration and localization, is proposed in [77]. More recently, a model for binaural coloration using multi-band loudness model weights to analyse the perceptual relevance of frequency components has been developed [78]. Unfortunately, these binaural methods once again lead to dissimilarity maps that do not satisfy (5). ## 4.3 Monoaural models To our knowledge, the binaural models in the literature do not lead to dissimilarities satisfying (5). In contrast, under suitable assumptions, monoaural models, i.e., models that need just one ear signal as input, do. Furthermore, they can be applied independently over each ear, to then use a worst-case scenario methodology [79] to extend them to binaural signals. We follow this approach and focus on monoaural models as surrogates to capture coloration effects. Monaural spectral localization models have been developed for localization across the sagittal plane, and also for localization across the azimuthal plane [80], but, to our knowledge, they do not satisfy (5). Models to detect monaural distortion aim to determine when two audio signals s 0 = s 0 ( t ) and s = s ( t ) are perceived as different, and how this perception degrades as a function of the dissimilarities between s 0 and s . To achieve this, two main ideas are used for the estimation of audible distortions: the masked threshold and the comparison of internal representations [79]. The masked threshold compares the error signal ε = s -s 0 against s 0 using a perceptual distortion function D ( ε, s 0 ) . The error is assumed to be inaudible if this value is less than a fixed masking threshold [81, 82]. The comparison of internal representations leverages a model for an internal representation s ↦→ I R ( s ) resulting from the signal transformations performed in the ear. The internal representations are compared using an internal detector ( I R ( s ) , I R ( s 0 )) ↦→ D ( I R ( s ) , I R ( s 0 )) and the difference between the signals is assumed to be perceptible if this value exceeds a given threshold [83, 79]. These studies do not provide analytical expressions that satisfy (5) for the representation nor for the internal detector. An approximation yielding such expressions is given in [84]; another simplified model is developed in [85]. The models developed in [81, 84, 85] yield monoaural dissimilarity maps D that satisfy (5). These methods can be represented as  where B 1 , . . . B n b are filters of the form  for a suitable function K B k representing a time-variant or time-invariant filter that may depend on s 0 itself. In [81, 85] the filters B k represent the auditory distortion over the k -th auditory filter of the cochlea, whereas in [84] the sum reduces to only one locally time invariant filter that accounts for the whole auditory distortion. Although monoaural, these models can be used for binaural signals ¯ s by taking the worst distortion between ear signals [79]  ## 4.4 Discomfort To model the loudness discomfort L we consider empirical evaluations of discomfort. This is a simplification motivated by computational simplicity and also by a small number of comprehensive studies on the subject. Empirical thresholds for loud discomfort levels for sinusoidal signals over a finite set of frequencies have been defined in the literature, e.g. in [86, 87]. Naturally, for a sinusoidal signal of frequency f k these can be expressed with the monaural expression  where ρ k ( f ) ≡ ρ k ∈ R + is the multiplicative inverse of the threshold at f k . Finally, for binaural signals, these models can be applied taking the worst discomfort between ears as in (12). ## 5 Implementation We provide a proof-of-concept implementation of SWEET-ReLU for approximating a sound wave generated by a (pseudo) sinusoidal, i.e., where the spectrum is concentrated around a single frequency, monopole emitting at a single frequency f . ## 5.1 Implementation of the acoustic framework The original sound wave u 0 is assumed to be emitted by an isotropic point source at x 0 ∈ R 3 . Each loudspeaker is assumed to be an isotropic point source. As we consider (pseudo) sinusoidal audio signals, the sound wave u generated by the array is given by (1) with  for coefficients a k ∈ C and a fixed spectral localization parameter σ 1 . ## 5.2 Implementation of the perceptual framework Monaural distortion detectability methods cannot represent the necessary features to correctly define an auditory illusion map as described in Section 4. Hence, they may not be optimal when modelling binaural perception. For instance, they cannot represent explicitly any type of azimuth localization, nor binaural coloration effects. However, they can represent monaural coloration effects, and some yield dissimilarity maps satisfying (5). For this reason, we use a monoaural model as a proof-of-concept. We use van de Par's spectral psycho-acoustic model [81]. Although it is suboptimal when modeling temporal masking effects, the signals we consider are stationary, whence temporal masking is almost non-existent. This monoaural model can be applied to binaural signals by using the worst-case as in (12). For x ∈ Ω and θ ∈ Θ we apply this model to the left and right ear signals ¯ u ( x, θ ) and ¯ u 0 ( x, θ ) . As van de Par's model can be represented by time-invariant filters in (11), for s ∈ { , r } we have that   The constant C A > 0 limits the perception of very weak signals in silence. The weight w B j is defined as w B j := | ηγ f j | 2 where  models the outer and middle ear as proposed by Terhardt [88] with C η, 0 = 4 . 69 , C η, 1 = 18 . 2 × 10 1 . 4 , C η, 2 = 32 . 5 × 10 -7 and C η, 3 = 5 × 10 -16 , and  models the filtering property of the basilar membrane in the inner ear at the center frequency f j , where the Equivalent Rectangular Bandwidth (ERB) of the auditory filter centered at f j is ERB ( f j ) = 24 . 7(1 + 4 . 37 × 10 -3 f j ) -1 as suggested by Glasberg and Moore [89]. The center frequencies f j are uniformly spaced on the ERB-rate scale ERBS ( f ) = 21 . 4 log(1 + 4 . 37 × 10 -3 f ) . In van de Par's model, the distortion is noticeable when its metric is greater or equal to 1. Hence, the monaural dissimilarity map becomes  where C ′ Ψ = 2 1 / 4 π 1 / 2 σC Ψ and we used the approximation for (pseudo) sinusoidal signals  when σ 1 . The constants C ′ Ψ and C A are defined as suggested in [81]. This accounts for the absolute threshold of hearing and the just-noticeable difference in level for sinusoidal signals, which gives, C ′ Ψ ≈ 1 . 555 and C A ≈ 4 . 481 when considering n b = 100 as the number of center frequencies, and f 1 = 20 , f n b = 10 3 as the first and last center frequency. The worst-case extension of this perceptual dissimilarity to binaural signals is given by  To model the loudness discomfort we use the experimental results in [86] about the discomfort caused by sinusoidal signals. We interpolate the data in this study with cubic splines with natural boundary [90, Section 8.6] to obtain a function η P > 0 . Therefore, we consider  where ρ B j depends on u 0 as where ρ f ( f, x, θ ) ≡ γ f ( f ) /η P ( f ) . Naturally, C ′ Π = 1 , as the empirical thresholds in [86] are attained when L m u s ( x ) ≤ 0 . Then, the worst-case extension to binaural signals is  Although this implementation is intended to study single-frequency signals, it can be generalized to multifrequency signals. The generalization of D m is direct and it comprises additional terms in the sum. The generalization of L m to a multifrequency signal could sum the discomfort associated to each frequency, similarly to the way the auditory filter errors are summed in D m , or it could use an integrating function as indicated in Section 4.4. These are simple heuristics for a proof-of-concept study, and their effectiveness should be validated experimentally. ## 5.3 Discretization In a typical experiment, listeners are seated in a room, and their locations and orientations within the room are determined in advance. In this case, a simplification consists in defining the sweet spot in terms of the number listeners for which the SAI is achieved. If the listeners can be located at finite number of points z 1 , . . . , z n l ∈ Ω then we can model the weighted area of the sweet spot as  which is equivalent to assuming µ is an atomic measure. In this case, every component of the proof-of-concept implementation can be evaluated either in closed-form, as is the case of the weighted area or the Green function of the loudspeakers, or can be approximated to very high-accuracy, as is the case of the head-related transfer functions (see Section 6 for details). The approximation (14) can be used when there is a discrete number of locations for listeners in a room. In other applications where it is necessary to control a continuum, e.g., when listeners may move across the room, quadrature rules must be used. In this case, the approach to solve ( P 0 ) follows an approximate-then-discretize approach, and numerical errors may have an effect on the sweet spot computed in practice. ## 6 Experiments For the experiments we compare the performance of our method with the state-of-the-art methods WFS, NFC-HOA and L 2 -PMM in terms of its azimuth localization and coloration performance, as they are the main features of the auditory scene for spatial sound. We use Dietz's model to measure binaural azimuth localization [63] and McKenzie's model for binaural coloration [78]. The setup for the numerical experiments consists of an equispaced arrangement of 20 loudspeakers lying on a circle of radius 2.5 m and at π/ 4 ≈ 0 . 785 m from each other. The region of interest Ω is a concentric circle of radius 2.4975 m (Fig. 1). The speed of sound is c s = 343 m/s. Two instances of this setup were evaluated: the near-field instance , where the source outside the arrangement at 5 m of its center with ̂ c 0 ( f ) = 68 dB, and the focus-source instance , where the source is inside the arrangement at 0.82 m of its center (Fig. 1b) with ̂ c 0 ( f ) = 60 dB. In both cases, f = 343 Hz. To construct the perceptual maps D and L we assume that the listeners are looking at the virtual sound source, which implies that Θ = Θ( x ) = { ang ( x 0 -x ) } . The SWEET-ReLU algorithm and the L 2 -PMM method were implemented in Python 3.8 using the CVXPY package, version 1.1.15 [91, 92] and MOSEK, version 9.3.6 [93]. The simulations of 2.5D NFC-HOA and 2.5D WFS were done with the Sound Field Synthesis Toolbox (SFST), version 3.2 [94], unless the focus-source 2.5D NFC-HOA simulations, which were done following the angular weighting approach [95]. The HRTFs used to simulate ¯ u and ¯ u 0 were constructed as the circulant Fourier transform of the elements of the TU-Berlin HRIR free data base [96]. Dietz's and McKenzie's models were implemented using Matlab 2022a with the Auditory Modelling Toolbox (AMT), version 1.1 [97]. For the implementation of the HRTFs, the 3 meters radial distance HRIRs of the data set were radially extrapolated using delay and attenuation, according to the map  where d is the desired radial distance. It should be noticed that for short distances, e.g. less than 1 m, ILDs vary significantly with distance [96]. Hence, the experiments might be enhanced by using a complete HRTF data set. For the Figure 1: Rows: Experimental setup. Target ̂ u 0 ( f ) (real part). Columns: Near-field instance. Focus-source instance. <details> <summary>Image 1 Details</summary> ![13834ff6](/v1/image/13834ff6cccdb4fc5e44aa75b8347628b4f3ded7273969624cc736f0d8ede6db) ### Visual Description ## Diagram: Wave Propagation and Interference Patterns ### Overview The image consists of four subplots (a-d) depicting wave propagation scenarios. Subplots (a) and (b) show geometric arrangements of sources, speakers, and Omega points, while (c) and (d) display heatmaps of wave intensity distributions. All subplots share a circular coordinate system with axes ranging from 0 to 5. ### Components/Axes - **Axes**: - X-axis: 0–5 (labeled "x") - Y-axis: 0–5 (labeled "y") - **Legends** (top-right of each subplot): - **Source**: Black dot (•) - **Speakers**: Black triangle (▲) - **Omega**: Green dot (•) - **Color Scales** (right of heatmaps): - (c): -0.010 (dark blue) to 0.010 (dark red) - (d): -0.020 (dark blue) to 0.020 (dark red) ### Detailed Analysis #### Subplot (a) - **Source**: Positioned at (0, 5) (top-left of the circle). - **Speakers**: 12 gray triangular elements arranged uniformly around the perimeter of the circle. - **Omega Points**: 12 green dots distributed along the circular boundary, aligned with speaker positions. - **Pattern**: No wavefronts shown; static arrangement of components. #### Subplot (b) - **Source**: Positioned at (2.5, 2.5) (center of the circle). - **Speakers**: Same 12 gray triangular elements as in (a), unchanged in position. - **Omega Point**: Single green dot at (2.5, 2.5), coinciding with the source. - **Pattern**: No wavefronts shown; static arrangement with centralized source. #### Subplot (c) - **Wave Intensity**: - Horizontal sinusoidal pattern with alternating red (positive) and blue (negative) stripes. - Amplitude range: -0.010 to 0.010. - No central focus; uniform horizontal variation. #### Subplot (d) - **Wave Intensity**: - Concentric circular pattern with alternating red (positive) and blue (negative) rings. - Central dark red core (peak intensity: ~0.020). - Amplitude range: -0.020 to 0.020. - Radial symmetry around the center. ### Key Observations 1. **Source Positioning**: - (a): Source at the edge of the circle. - (b): Source at the center of the circle. 2. **Omega Points**: - (a): Omega points on the perimeter, aligned with speakers. - (b): Omega point at the center, overlapping the source. 3. **Wave Patterns**: - (c): Horizontal interference pattern (no radial focus). - (d): Radial interference pattern (centralized source effect). 4. **Amplitude**: - (d) exhibits twice the maximum amplitude of (c), suggesting a stronger source or different boundary conditions. ### Interpretation The diagrams illustrate two wave propagation scenarios: 1. **Edge Source (a)**: - Source at the perimeter may simulate boundary-driven waves (e.g., acoustic reflections). - Omega points on the perimeter could represent measurement nodes or boundary conditions. 2. **Central Source (b)**: - Source at the center mimics omnidirectional wave generation. - Single Omega point at the center suggests a focus on central intensity measurement. 3. **Heatmap Comparison**: - (c) shows uniform horizontal variation, possibly from a line source or boundary effect. - (d) demonstrates radial interference from a central source, with higher amplitude due to constructive/destructive wave interactions. 4. **Anomalies**: - In (b), the Omega point coinciding with the source may indicate a measurement at the origin, which could be physically unrealistic for certain wave types (e.g., pressure waves at a point source). ### Technical Implications - The transition from (a) to (b) highlights how source position alters wavefront geometry. - Heatmaps (c) and (d) quantify interference patterns, with (d) showing a 2× amplitude increase, suggesting a direct relationship between source centrality and wave intensity. - The use of Omega points as boundary/measurement nodes in (a) versus a central node in (b) implies different modeling approaches for wave propagation studies. </details> implementation of Dietz's model, since we treated (pseudo) sinusoidal signals, the interaural phase differences (IPDs) and ILDs of the reproduced signals were extracted manually following the convention of [63] as    Then, the unwrapped ITDs were obtained from the ILDs and IPDs using the dietz2011\_unwrapitd.mat function. The estimated azimuth localization is obtained by plugging the ITDs into the itd2angle.mat function, which uses the itd2angle\_lookuptable.mat table. The latter table is constructed with the same HRTFs that we consider for the simulation of ¯ u and ¯ u 0 . For the implementation of McKenzie's model, the binaural signals were transformed to time-domain using a sampling frequency of 44100 Hz and a number of samples of 256. As proposed in [98, Chapter 5.6.2], the implementation of the angular weighting for NFC-HOA in focus-source instances was defined, for the n -th mode, as  where d is the distance from the source to the center of the room, and ω = 2 πf . For the implementation of the SWEET method, we have chosen ε i adaptively with percentile p = 99 . For SWEET and L 2 -PMM a uniform discretization of 2348 points was used for Ω at a distance of at most 0.09 m, achieving more than 30 points per wavelength. To compare the performance of the methods, we measure the size of the localization sweet spot (LSS) and coloration sweet spot (CSS). We former is the region where the perceived azimuth localization measured by Dietz's model deviates no more than 5 degrees from the desired one, whereas the latter is the region where the coloration measured by McKenzie's model is lower or equal than 13 sones. As discussed in [78], a coloration lower than 13 sones is strongly correlated with empirical MUSHRA tests with more than 80 out of 100 points. It should be noted that, since we analyse (pseudo) sinusoidal signals of frequency 343 Hz, in these experiments the CSS and LSS are constituted by the points where the interaural amplitude or phase (respectively) of the binaural signal are correctly reconstructed. Figure 2: Near-field instance. Rows: Near-field ̂ u ( f ) (real part). Dietz's near-field azimuth localization, where the direction of the arrows represent the perceived localization whereas the color represents the deviation in degrees of the perceived localization from the desired one. McKenzie's near-field coloration (sones). Columns: SWEET-ReLU, NFC-HOA, WFS, and L 2 -PMM. <details> <summary>Image 2 Details</summary> ![51e938cd](/v1/image/51e938cdc2183d924c1831f97936255f70c449a9d5aa1503046ebfb716bae7d6) ### Visual Description ## Circular Flow Field Analysis: 12-Regime Comparison ### Overview The image presents a 3x4 grid of circular flow field visualizations (labeled a-l) depicting fluid dynamics around a central object (likely a turbine or fan). Each plot combines color-coded scalar fields with vector arrows, showing variations in flow patterns, pressure distributions, and turbulence intensities across different operational regimes. ### Components/Axes - **Domain**: All plots share a circular coordinate system (0-5 units radius) with a central object at (0,0). - **Color Scales**: - Plots a-d: ±0.010 (likely pressure/velocity fluctuations) - Plots e-h: 0-90 (magnitude scale, possibly velocity) - Plots i-l: 0-100 (intensity scale, possibly turbulence) - **Legends**: Right-aligned color bars with numerical ranges; blue=low values, red=high values. - **Vectors**: Arrows in e-h and l indicate flow direction/magnitude (blue=low, red=high). ### Detailed Analysis #### Row 1 (a-d): Laminar Flow Regimes - **(a)**: Horizontal sinusoidal stripes (red/blue) with uniform amplitude (±0.010). Suggests steady oscillatory flow. - **(b)**: Similar stripes but with increased vertical perturbation (turbulence onset). Amplitude peaks at ±0.008. - **(c)**: Wavy patterns with localized high-pressure regions (red peaks at ±0.012). Indicates flow separation. - **(d)**: Smoother gradient with minimal vector activity. Represents transitional flow state. #### Row 2 (e-h): Vector Field Dynamics - **(e)**: Uniform flow vectors (blue) radiating outward. Indicates free-stream conditions. - **(f)**: Chaotic vector distribution with 30% red vectors. Shows turbulent mixing. - **(g)**: Converging vectors near center (red core, blue periphery). Represents suction flow. - **(h)**: Diverging vectors with 45° angular spread. Indicates flow expansion. #### Row 3 (i-l): High-Intensity Turbulence - **(i)**: Deep blue vortex core (magnitude 80) surrounded by red turbulence (60-100). Classic stalled flow pattern. - **(j)**: Dual vortex structure with opposing rotation directions. Amplitude asymmetry (left=75, right=65). - **(k)**: Radial shear layer with gradient from 20 (blue) to 90 (red). Indicates boundary layer transition. - **(l)**: Turbulent wake with 60% red vectors. Shows high-energy dissipation. ### Key Observations 1. **Flow Regime Transition**: a-d → e-h → i-l shows progression from laminar to turbulent flow. 2. **Central Object Influence**: All plots exhibit radial symmetry disruption, confirming object-induced flow modification. 3. **Vector Correlation**: Red vectors consistently align with high-magnitude regions across all plots. 4. **Turbulence Intensity**: Plots i-l show 300% increase in scalar field magnitude vs. a-d. ### Interpretation This visualization demonstrates the Reynolds number effects on flow around a rotating object. The color gradients represent pressure/velocity fields, while vectors quantify directional changes. The transition from ordered stripes (a-d) to chaotic vectors (e-h) and high-intensity turbulence (i-l) suggests increasing flow velocity or object rotation speed. The dual-vortex structure in (j) and wake turbulence in (l) indicate complex flow separation mechanisms. These patterns align with computational fluid dynamics (CFD) simulations of rotating machinery, where turbulence intensity correlates with mechanical efficiency losses. </details> The CSS and LSS generated by each method for the near-field and focus-source instances are shown in Fig. 2 and 3 respectively, and their size is shown in Table 1. The blue zones of Figs 2e-l, Figs 3e-l represent the sweet spots of each case. The estimated localization in Figs 2e-h, Figs 3e-h is shown for deviations of 0 to 90 degrees from the desired one. Greater deviations are represented by a dot with no direction. | | SWEET | NFC-HOA | WFS | L 2 -PMM | |-------------|---------|-----------|-------|------------| | NF CSS | 70.8% | 51% | 55.6% | 3.3% | | NF LSS | 68.4% | 42.9% | 47.9% | 52.3% | | FS CSS | 58.7% | 27.8% | 0.1% | 5.2% | | FS LSS | 54% | 42.9% | 16.2% | 40.1% | | FS LSS (DH) | 50.8% | 37.8% | 12.5% | 28.9% | Table 1: CSS and LSS over Ω fractions in Near-field (NF) and Focus-Source (FS)] instances. [(DH) disregards the convergent halfspace]. Figure 3: Focus-source instance. Rows: Near-field ̂ u ( f ) (real part). Dietz's near-field azimuth localization, where the direction of the arrows represent the perceived localization whereas the color represents the deviation in degrees of the perceived localization from the desired one. McKenzie's near-field coloration (sones). Columns: SWEET-ReLU, NFC-HOA, WFS, and L 2 -PMM. <details> <summary>Image 3 Details</summary> ![a01c9858](/v1/image/a01c98589c5b810c2a28ed3741f1592a711bee2ec839c217779b7c21776114a0) ### Visual Description ## Heatmaps and Vector Field Visualizations: Flow Patterns Around a Circular Domain ### Overview The image contains 12 subplots (a)-(l) depicting fluid dynamics simulations of flow patterns and pressure distributions around a circular domain with boundary conditions. Each subplot uses color gradients and vector fields to represent scalar quantities (e.g., pressure) and vector quantities (e.g., velocity direction/magnitude). The circular domain is bounded by gray square markers representing fixed boundary conditions. --- ### Components/Axes - **Axes**: - X-axis: 0–5 (linear scale) - Y-axis: 0–5 (linear scale) - Circular domain centered at (2.5, 2.5) with radius ~2.5 units. - **Legends**: - Color scales vary per subplot: - Subplots (a)-(d): -0.020 to 0.020 (pressure/velocity magnitude). - Subplots (e)-(h): 0 to 90 (velocity magnitude). - Subplots (i)-(l): 0 to 100 (pressure/velocity magnitude). - Arrows in vector fields (e)-(h) indicate direction and magnitude. - **Boundary Conditions**: Gray squares along the circular perimeter (fixed walls or no-slip boundaries). --- ### Detailed Analysis #### Subplots (a)-(d): Scalar Fields (Pressure/Velocity Magnitude) - **(a)**: Central vortex with concentric pressure gradients. Red (high pressure) at the center transitions to blue (low pressure) at the edges. - **(b)**: Spiral flow pattern with alternating high/low pressure regions. - **(c)**: Alternating banded structure with sharp transitions between red and blue. - **(d)**: Central vortex with radial streaks, suggesting turbulent flow. #### Subplots (e)-(h): Vector Fields (Velocity Direction/Magnitude) - **(e)**: Radial outward flow with uniform arrow density. - **(f)**: Flow separation at the top boundary, creating recirculation zones. - **(g)**: Symmetric flow with minimal deviation from the centerline. - **(h)**: Complex flow with vortices and directional streaks. #### Subplots (i)-(l): High-Magnitude Scalar Fields - **(i)**: Sharp pressure gradient with a central low-pressure zone (blue) and high-pressure regions (red). - **(j)**: Symmetric flow with a central vortex and radial pressure waves. - **(k)**: High-pressure regions (red) dominate, with a central low-pressure zone. - **(l)**: Concentric pressure waves resembling shock waves or acoustic patterns. --- ### Key Observations 1. **Flow Separation**: Subplots (f) and (h) show boundary-layer separation, indicated by reversed flow directions near the top boundary. 2. **Vortices**: Central vortices appear in (a), (d), (j), and (l), with varying intensity and structure. 3. **Pressure Gradients**: Subplots (i) and (k) exhibit extreme pressure contrasts, suggesting high-speed flow or shock interactions. 4. **Symmetry**: Subplots (e), (g), and (l) display axisymmetric flow, while (b) and (c) show asymmetric patterns. --- ### Interpretation These visualizations likely represent computational fluid dynamics (CFD) simulations of flow around a circular object (e.g., a cylinder or sphere). The variations in flow patterns suggest differences in: - **Reynolds Number**: Higher Reynolds numbers (turbulent flow) may explain the complex vortices in (d), (h), and (l). - **Boundary Conditions**: Fixed walls (gray squares) influence flow separation and recirculation (e.g., (f)). - **Flow Regimes**: Subplots (a)-(d) may represent laminar flow, while (e)-(h) and (i)-(l) show transitional/turbulent regimes. The pressure distributions (red/blue gradients) correlate with velocity magnitudes (arrow lengths in vector fields), indicating regions of acceleration/deceleration. For example, the central low-pressure zones in (a), (j), and (k) align with high-velocity regions, consistent with Bernoulli’s principle. The simulations could inform aerodynamic design, turbulence modeling, or boundary-layer control strategies. Outliers like the sharp pressure waves in (l) may represent unsteady flow phenomena or numerical artifacts requiring further validation. </details> For the near-field instance, both the LSS and CSS generated by our method are more than 20 and 10 points (respectively) larger than that generated by any other method. The LSS and CSS generated by NFC-HOA (Figs. 2j, 2f) are centered, whereas that generated by WFS (Figs. 2k, 2g) are localized farther away from the source. This is correlated with their degradation of the sound field, which is consistent with the analysis in [14]. Moreover, their LSS are consistent with the empirical results exposed in [34]: the perceived localization for NFC-HOA degrades away from the center, whereas for WFS the perceived localization is fairly good over almost all the listening region. However, we believe that the perceived localization for WFS and NFC-HOA behaves slightly worse here than in [34] because we analyze sinusoidal signals instead of Gaussian white noise, which has uniform spectral content. In contrast, the LSS and CSS generated by our method (Figs. 2i, 2e) behave like those generated by WFS, but almost encompasses those generated by NFC-HOA. The LSS of L 2 -PMM (Fig. 2h) is larger than that of WFS and NFC-HOA, but its CSS (Fig. 2l) is almost negligible. This is consistent with the sound wave u produced with L 2 -PMM (Fig. 2d) as the spatial phase of the signals is fairly well reconstructed, whereas its amplitude is too small. In the focus-source instance, due to reasons of causality, theoretically any method can achieve the correct reproduction of the direction of propagation of u 0 in one half-space defined by { x i } n s i =0 , where the sound field diverges from the focus-source position [99]. In the other half-space the reproduced wave field converges towards the location of the virtual source. As shown in Figs. 3e-h, the LSS of all the methods comprise a portion of the converging part of the sound field. This is possible because the interaural phase of the binaural sinusoidal signals is correctly recreated at those points. However, we believe that in more complex scenarios, involving multi-frequency signals and allowing the listener to turn her head, e.g., considering a larger Θ , it would not be possible to recreate correctly and consistently the localization illusion. As shown in [98, Chapter 5.6] 'for listeners located in the converging part of the sound field, the perception is unpredictable since the interaural cues are either contradictory or change in a contradictory way when the listener moves the head. ' Table 1 contains the fraction of the LSS over Ω for the focus-source instance considering all the points of the converging half-space as incorrectly reconstructed, denoted by the label (DH). For the focus-source instance, the LSS and CSS generated by our method (Fig. 3e, 3i) is approximately 10 and 30 (respectively) points larger than those generated by other methods. The LSS and CSS generated by NFC-HOA (Fig. 3f, 3j) is concentrated in a limited region at the diverging part and around a vertical line that passes through x 0 . The LSS generated by WFS (Fig. 3g) is almost contained in the same vertical line, although the error in the localization reconstruction is below 15 degrees in a larger area. The CSS generated by WFS (Fig. 3k) is almost empty as the resulting u has a large amplitude. This suggest that a focus-source formulation for WFS needs a factor for amplitude normalization. The LSS of L 2 -PMM (Fig. 3h) has almost the same size as that of NFC-HOA, but its CSS (Fig. 2l) is almost negligible. This is consistent with the sound wave u produced with L 2 -PMM (Fig. 3d) as the spatial phase of the signals is fairly well reconstructed, whereas its amplitude is too small. The LSS and CSS generated by our method (Fig. 3e, 3i) comprises almost all the divergent part. This highlights one of the advantages of the greedy approach of SWEET-ReLU: it is capable to detect the direction of u 0 over Ω in its first iterations, to then prioritize the part of Ω where a good fit to ¯ u 0 can be obtained. This is a possible explanation for the amplitude mismatch of L 2 -PMM both in the near-field (Fig. 2d) and the focus-source (Fig. 3d) instances: just minimizing the square of the spatial errors strongly penalizes the spatial points where the amplitude is very large and difficult to reconstruct, i.e., near the loudspeakers. Then, L 2 -PMM finds a solution where the amplitude error at those points is not too large, leading to a small overall amplitude. ## 7 Discussion Our results show the SWEET-ReLU method yields state-of-the-art results in standard numerical experiments with our proof-of-concept implementation. We believe the performance in these experiments is representative of what we would observe when using more complex pyscho-acoustic models for the perceptual dissimilarity and the loudness discomfort. A key component of our method is the perceptual dissimilarity D . Although its form in our proof-of-concept implementation is quite flexible, it does not account for spatialization and other binaural effects. Finding a model to account for these effects such that D satisfies (5) is the subject of future research. It should be noted that, as it is shown in [100], the overall quality of a spatial sound system can be explained to 70% by coloration or timbral fidelity, which can be partially characterized by monoaural effects, and 30% by spatial fidelity, which needs to be characterized by binaural effects. Furthermore, our proof-of-concept experiments show that even though the perceptual model we use is an extension of a monoaural model using a worst-case approach, it still is able to perform better than state-of-the-art methods in terms of localization and coloration. This suggests our implementation with this model is able to capture correctly some of the spatial properties of the auditory scene, even though these properties are not explicitly in the model. This might be explained because the coloration and localization is strongly dependant of the amplitude and phase of the binaural signals, which are controlled by our implementation of a binaural extension of an amplitude and phase-sensitive monaural model. Although our implementation assumes the loudspeakers and the sources are monopoles, we believe our method can be readily implemented in real settings with non-trivial sound sources. For instance, reverberation, different radiation patterns for the loudspeakers, and other time-invariant effects can be incorporated by modifying the Green function G k in (2) and the transfer functions in (4) accordingly. Finally, although we have not fully developed a theory for the convergence of SWEET-ReLU, our numerical experiments show that the method converges to reasonable results in practice. Furthermore, our proof-of-concept implementation avoids any potential issues arising from the discretization of the models, either due to numerical computation of the Green function or transfer functions, or to the discretization of the integral that defines the weighted area. Further analysis about this point will be the subject of future work. ## 8 Conclusion In this work, we introduced a theoretical framework for spatial audio perception that allows the definition of a perceptual sweet spot, that is, the region where the spatial auditory illusion is achieved when approximating one sound wave by another. Furthermore, we developed a method that finds an approximating sound wave that maximizes this sweet spot while guaranteeing no loudness discomfort over a spatial region of interest. We provided a theoretical analysis of the method, and an efficient algorithm, the SWEET-ReLU algorithm, for its numerical implementation. In a proofof-concept implementation using monopoles emitting (pseudo) sinusoidal signals, our method successfully captures some of the spatial properties of the auditory scene, such as localization and coloration, even though these properties are not explicitly in the model. We believe our method is a first step towards a novel approach for spatial sound with loudspeakers, bridging a gap between methods based on perceptual principles, and sound field synthesis methods. ## Acknowledgment C. A. SL. was partially funded by ANID - FONDECYT - 1211643, ANID - Millennium Science Initiative Program -NCN17\_059 and ANID - Millennium Science Initiative Program - NCN17\_129. ## References - [1] Rozenn Nicol. Creating auditory illusions with spatial-audio technologies. In The Technology of Binaural Understanding , pages 581-622. Springer, 2020. - [2] Hagen Wierstorf, Alexander Raake, and Sascha Spors. Binaural assessment of multichannel reproduction. 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We define F : W → W as F ¯ u ( x,θ ) = ( ̂ u ( x,θ ) , ̂ u r ( x,θ ) ) . It can be verified F is an isometry in W . Let I S ⊂ R and let γ max > 0 . The set of admissible audio signals driving each loudspeaker is  where | denotes restriction; they are bandlimited to I S and have norm bounded by γ max. The sound waves in (4) belong to  To quantify the area of the sweet spot in (7) we use a finite Borel measure µ on Ω [101, Section 1.2] and we suppose that the resulting measure space is complete [101, Section 1.5]; we usually suppose µ is absolutely continuous with respect to the Lebesgue measure or atomic. If ¯ u is the pair of signals generated by the array, then µ ( S (¯ u )) is the weighted area of the sweet spot S (¯ u ) . We consider the space L ∞ µ (Ω) of (equivalence classes of) real-valued Borel measurable functions that are bounded µ -a.e. [101, Section 3.3]. Frequently used operations, such as the sum, supremum or infimum of functions, the integral, and inequalities, are well-defined for such equivalence classes of measurable functions. Assumption 1. (i) Ω and Θ are compact. (ii) I S is compact. (iii) The functions H k , H r k are continuous and bounded on I S × Ω × Θ . (iv) The dissimilarity map D : W × W → C 0 (Ω × Θ) is continuous and convex on its first argument. (v) The discomfort map L : W → C 0 (Ω × Θ) is continuous and convex. (vi) ¯ u 0 ∈ W . The model proposed in Section 2.2 is well-defined. Proposition 1. Under Assumption 1 the following assertions are true: (i) The set W S is convex and compact in W . (ii) The map T D : W S → L ∞ µ (Ω) is continuous, and for every ¯ u ∈ W S the map ¯ u → T D ¯ u ( x ) in (6) is convex for µ -a.e. x . (iii) The map µ ◦ S : W → R is well-defined, that is, its values do not depend on the choice of representative of T D ¯ u . (iv) The set P in (8) is convex and closed in W . We defer the proof to Appendix A.8. Although the feasible set for ( P 0 ) is compact, the objective depends on the properties of the set-valued function u ⇒ S ( u ) . As studying these properties and minimizing µ ◦ S is potentially challenging, we propose an approximation to ( P 0 ) that can be analyzed and solved with standard methods. ## A.2 The layer-cake representation We approximate the area of S ( u ) using the layer-cake representation . Assumption 2. ϕ : R → R is absolutely continuous, bounded, non-negative and such that ϕ ( t ) = 0 for t < 0 and ‖ ϕ ‖ L 1 = 1 . For ε > 0 let ϕ ε denote ϕ ε ( t ) = ϕ ( t/ε ) /ε and define  Since Φ ε is continuous, the composition Φ ε ◦ v is well-defined as an element in L ∞ µ (Ω) for any v ∈ L ∞ µ (Ω) . Similarly,  is well-defined for any v ∈ L ∞ µ (Ω) . By Assumption 2 Φ ε is non-decreasing, whence v 1 ≤ v 2 implies A ε ( v 1 ) ≤ A ε ( v 2 ) , i.e., A ε is non-decreasing. Proposition 2. Under Assumption 2, for every v ∈ L ∞ µ (Ω) and any representative v ′ of v we have  Proof of Proposition 2. Let t ≥ 0 and let { ε n } n ∈ N be non-negative and monotone decreasing to zero. Define V t,n := { x ∈ Ω : v ′ ( x ) ≥ ε n t } and note that V t,n ⊆ V t,n +1 . Define V := ⋃ n> 0 V t,n = { x ∈ Ω : v ′ ( x ) > 0 } and h n ( t ) = ϕ ( t ) µ ( V t,n ) . Note h n is measurable for every n as t ↦→ µ ( V t,n ) is monotone. Then h n ( t ) ↑ ϕ ( t ) µ ( V ) as n → ∞ by continuity from below [101, Proposition 1.2.5]. Since Ω is bounded, v ∈ L 1 µ (Ω) and v ′ is absolutely integrable. By Fubini's theorem,  where we used the change of variables s = t/ε n and the monotone convergence theorem [101, Theorem 2.4.1]. As { ε n } n ∈ N is arbitrary, the claim follows. For ¯ u ∈ W S and ε > 0 sufficiently small we have by Propositions 1 and 2 that  where T D ¯ u ′ is any representative of T D ¯ u . Consequently, µ ( S (¯ u )) ≈ µ (Ω) -A ε ( T D ¯ u ) and for every fixed ¯ u ∈ W S we can approximate µ ( S (¯ u )) by A ε ( T D ¯ u ) . ## A.3 The variational problem We propose to solve the surrogate problem  Proposition 3. Suppose Assumption 2 holds. The function A ε : L ∞ µ (Ω) → R is continuous, and ( P ε ) has at least one minimizer. Proof of Proposition 3. Let δ > 0 , let v 0 , v ∈ L ∞ µ (Ω) be such that ‖ v -v 0 ‖ L ∞ µ < δ/ 2 , and let v ′ and v ′ 0 be representatives. There exists Ω ∗ ⊂ Ω with µ (Ω \ Ω ∗ ) = 0 such that | v ′ ( x ) -v ′ 0 ( x ) | < δ/ 2 for x ∈ Ω ∗ . Since ϕ ε is non-negative and bounded on the interval [ -‖ v 0 ‖ L ∞ µ -δ/ 2 , ‖ v 0 ‖ L ∞ µ + δ/ 2] , for any x ∈ Ω ∗ we have that  where c ϕ ε > 0 depends only on ϕ ε . As the bound is independent of the choice of v ′ , v ′ 0 , | A ε ( v ) -A ε ( v 0 ) | ≤ c ϕ ε µ (Ω) δ whence A ε is continuous. The existence of solutions follows from the compactness of W S ∩ P . ## A.4 DC Formulation To solve ( P ε ) we first rewrite it equivalently as  We interpret the auxiliary variable v as an overestimate of the auditory illusion map over Ω . Proposition 4. Under Assumptions 1 and 2, if ¯ u is an optimal solution to ( P ε ) then (¯ u , T D ¯ u ) is an optimal solution to ( ˜ P ε ) . In particular, ( ˜ P ε ) has a solution. Proof of Proposition 4. Let p ε , ˜ p ε be the optimal values for ( P ε ) and ( ˜ P ε ) respectively, where ˜ p ε is finite as ( ˜ P ε ) is feasible and A ε ≥ 0 . On one hand, if ¯ u ε is an optimal solution to ( P ε ) , which exists by Proposition 3, then (¯ u ε , T D ¯ u ε ) is feasible for ( ˜ P ε ) . Hence, ˜ p ε ≤ p ε . On the other, if (¯ u, v ) feasible for ( ˜ P ε ) then ¯ u is feasible for ( P ε ) . Since A ε is monotone, p ε ≤ A ε (¯ u ) ≤ A ε ( v ) whence p ε ≤ ˜ p ε . We conclude ˜ p ε = p ε and (¯ u ε , T D ¯ u ε ) is an optimal solution to ( ˜ P ε ) . Under suitable assumptions, the objective function in ( ˜ P ε ) is the difference of convex functions . Assumption 3. In addition to Assumptions 1 and 2, there exists ϕ + : R → R absolutely continuous, non-decreasing and such that ϕ + ( t ) = 0 for t < 0 and that ϕ + -ϕ is a non-decreasing function. We let ϕ + ε ( x ) = ϕ + ( x/ε ) /ε and we define  Similarly, let ϕ -ε = ϕ -ϕ + ε and Φ -ε ( t ) = Φ + ε ( t ) -Φ ε ( t ) . By construction, Φ ε = Φ + ε -Φ -ε . Proposition 5. Under Assumption 3, Φ + ε and Φ -ε are convex. Proof of Proposition 5. By construction, both Φ + ε and Φ -ε have derivatives ϕ + ε and ϕ -ε respectively, which are both non-decreasing, hence monotone [102, Proposition 17.10]. Since Φ + ε , Φ -ε are convex, they are continuous. We decompose A ε as A ε = A + ε -A -ε where  and A -ε is defined similarly. It is apparent that A + ε , A -ε : L ∞ µ (Ω) → R are convex and also continuous. We conclude ( ˜ P ε ) is a Difference-of-Convex (DC) program [103, 104]. The Convex-Concave Procedure (CCCP) [105] is an efficient method to attempt to find a solution to this class of optimization problems. The CCCP is an iterative method that uses an affine majorant for the concave part, e.g., using subgradients, to majorize the objective function in (16) by a convex function. Let v 0 ∈ L ∞ µ (Ω) and let L ∞ µ (Ω) ∗ be the topological dual of L ∞ µ (Ω) . We say g ∈ L ∞ µ (Ω) ∗ is a subgradient of A -ε at v 0 if  The subdifferential ∂A -ε ( v 0 ) is the collection of all subgradients at v 0 . Since A -ε : L ∞ µ (Ω) → R is continuous and convex, it has a subdifferential at every v 0 [106, Proposition 2.36]. We can use the convex majorizer  where g v 0 ∈ L ∞ µ (Ω) ∗ and solve  Proposition 6. Under Assumption 3, for ε > 0 and v 0 ∈ L ∞ µ (Ω) ( ˜ P ε,v 0 ) has at least one optimal solution. We defer the proof to Appendix A.9. In our method we make an explicit choice of a subgradient. Proposition 7. Under Assumption 3, for v 0 ∈ L ∞ µ (Ω) the linear application  is well-defined for v ∈ L ∞ µ (Ω) , continuous and is a subgradient for A -ε at v 0 . Proof of Proposition 7. Since v 0 ∈ L ∞ µ (Ω) and ϕ -ε is non-decreasing, ϕ -ε ◦ v 0 ∈ L ∞ µ (Ω) . Hence, g v 0 is well-defined and g v 0 ∈ L ∞ µ (Ω) ∗ . By the definition of Φ -ε and Assumption 2, Φ -ε ( t ) ≥ Φ -ε ( t 0 ) + ϕ -ε ( t 0 )( t -t 0 ) for all t, t 0 ∈ R . This implies  Given (¯ u 0 , v 0 ) the CCCP constructs a sequence { (¯ u k , v k ) } k ∈ N where (¯ u k +1 , v k +1 ) is the optimal solution to ( ˜ P ε,v k ) . To our knowledge, the best theoretical guarantees for finite-dimensional problems show that this sequence converges to a stationary point of ( ˜ P ε ) [103, Theorem 3], whereas we are not aware of similar guarantees for infinite-dimensional problems. However, { ¯ u k } k ∈ N is a sequence in W S and we can extract a subsequence { ¯ u k ( ) } ∈ N with limit ¯ u . If { ˜ p k } k ∈ is the sequence of optimal values to each ( ˜ P ε,v k ) then  by the continuity of T D , A ε and the fact that A ε is non-decreasing. The optimal values are a conservative estimate of A ε ( T D ¯ u ) . Our numerical results show the solutions found this way performs well in practice. ## A.5 SWEET-ReLU When ϕ is the indicator function of [0 , 1] the function Φ becomes the difference of two Rectified Linear Units (ReLUs). In this case, ϕ ε = ε -1 χ [0 ,ε ] . The decomposition Φ ε = Φ + ε -Φ -ε becomes   Let Ω ε,v 0 := { x ∈ Ω : v 0 ( x ) ≤ ε } . Since both A -ε ( v 0 ) and g v 0 ( v 0 ) in ( ˜ P ε,v 0 ) are constant, it suffices to compute  where we used the fact that t + -t = ( -t ) + . The second term is non-negative, and becomes positive only when v takes negative values. As Tu ≤ v in ( ˜ P ε,v 0 ) we can choose v arbitrarily large on Ω c ε,v 0 to decrease the objective value and to neglect the second integral. Then, only the first term contributes to the objective in ( ˜ P ε,v 0 ) and we obtain  As the positive-part function is monotone, we can eliminate v to obtain  which is precisely the problem ( P SReLU 1 ) when v 0 ≡ 0 . It depends on v 0 only through Ω ε,v 0 . To construct an optimal solution (¯ u k , v k ) from the optimal solution ¯ u k we proceed as follows: by choosing v k | Ω ε,v k -1 = T D ¯ u k | Ω ε,v k -1 and v k | Ω c ε,v k -1 = max { ε, T D ¯ u k | Ω c ε,v k -1 } we obtain Ω ε,v k = { x ∈ Ω : v ′ k ( x ) ≤ ε } = { x ∈ Ω ε,v k -1 : T D ¯ u ′ k ( x ) ≤ ε } = Ω ε,v k -1 ∩ { x ∈ Ω : T D ¯ u ′ k ( x ) ≤ ε } , yielding the method as presented in Section 3. and the subgradient (17) becomes ## A.6 A class of monoaural dissimilarity maps We introduce a class of dissimilarity metrics based on time-variant filters satisfying Assumption 1. Lemma 1. Let K : Ω × Θ → L 2 ( R 2 ) be continuous with  finite. Define for ( x, θ ) ∈ Ω × Θ , w ∈ L 2 ( R )  Then A K ( x,θ ) is linear, A K ( x,θ ) w ∈ L 2 ( R ) and ( x, θ, w ) ↦→ A K ( x,θ ) w is continuous. Proof. The linearity follows from the integral representation. From Young's inequality for integral operators [107, Theorem 0.3.1]  whence ( x, θ ) ↦→ A ( x,θ ) w is bounded. By the Cauchy-Schwarz inequality  where continuity follows from hypothesis. Proposition 8. Let ¯ u 0 ∈ W and let { B k } n b k =1 be as in (11) where { K B k } n b k =1 satisfy the hypotheses of Lemma 1. Let Ψ : R n b + → R be convex and monotone increasing on each one of its arguments. For s ∈ { , r }  is a dissimilarity satisfying Assumption 1. In particular, so is  Proof. For simplicity, we prove the result for ¯ u 0 = 0 . It can be verified that B k u s ( x,θ ) = ‖ A K B k ( x,θ ) u s ( x,θ ) ‖ 2 L 2 . By Lemma 1, a function of the form  is continuous on Ω × Θ . Since A K B k ( x,θ ) is linear on u s ( x,θ ) and the norm is convex, the convexity of D s follows from the assumptions on Ψ . ## A.7 Discussion Although Proposition 2 implies A ε converges pointwise to µ ◦ S , this is not sufficient to ensure a global minimizer for ( P ε ) converges to a global minimizer for ( P 0 ) . A future line of work consists on leveraging Γ -convergence to answer this question. Related to it is the choice of ϕ . Although we have not studied extensively the effect of this choice, we believe it affects the quality of the approximation to the area of the sweet spot. This is another interesting future line of work. In addition, we would like to point out that the advantage of solving a sequence of approximate problems for decreasing values of ε over solving a single approximate problem for ε 1 lies in the fact that each approximate problem is non-convex. Then, to find an approximate solution to it, the DCCC algorithm needs an initial point. This, coupled with the observation that for a sufficiently large ε the problem becomes equivalent to a convex problem, solving a sequence of approximate problems is a systematic way to find an initial point for the approximate problems defined for ε 1 . Finally, the method allows for several choices of µ . Therefore, the results presented apply both for the continuous case, e.g., when µ is the Lebesgue measure, and the discrete case, e.g., when µ is discrete. ## A.8 Proof of Proposition 1 Proof of (i). It is apparent that W S is convex. Since Ω × Θ is a separable metric space, if W S is bounded and equicontinuous, by Arzelà-Ascoli's theorem [108, Theorem 11.28] it follows it is compact. By Assumption 1,  and ( x, θ ) ↦→ u ( x,θ ) is uniformly bounded. Thus, W S is bounded. Let ε > 0 . Since ̂ H s k is continuous on the compact set I S × Ω × Θ , there is δ > 0 such that for any | x -y | , | θ -φ | < δ and f ∈ I S we have that | ̂ H s k ( f, x, θ ) -̂ H s k ( f, y, φ ) | < ε/ 2 n 2 s γ 2 max . Then,  whence ( x, θ ) ↦→ ¯ u ( x,θ ) is continuous. Since δ is independent of ¯ u , we conclude W S is equicontinuous. Proof of (ii). Let ¯ u, ¯ u 0 ∈ W . The function D (¯ u, ¯ u 0 ) is continuous on the compact set Ω × Θ and thus bounded. Hence, T D ¯ u is bounded and we can associate to it its equivalence class in L ∞ µ (Ω) . Let ε > 0 . There exists δ > 0 such that ‖ v -u ‖ L 2 , ‖ v r -u r ‖ L 2 < δ implies | D (¯ v, ¯ u 0 ) ( x, θ ) -D (¯ u, ¯ u 0 ) ( x, θ ) | < ε/ 2 . This implies | T D ¯ v ( x ) -T D ¯ u ( x ) | < ε whence T D is continuous. By Assumption 1, the map D is convex on its first argument. The conclusion follows from  Proof of (iii). For T D u ∈ L ∞ µ (Ω) we can choose representatives T D u ′ , T D u ′′ of T D u . Hence, the set { x ∈ Ω : T D u ′ ( x ) = T D u ′′ ( x ) } has µ -measure zero, from where the conclusion follows. Proof of (iv). From the same arguments used for (ii) the map T L : W → L ∞ µ (Ω) is continuous. As { v ∈ L ∞ µ (Ω) : v ( x ) > 0 µ -a.e. } is open, then P c = { ¯ u ∈ W : T L ¯ u ( x ) > 0 µ -a.e. } is open, whence P is closed. ## A.9 Proof of Proposition 6 Let v ′ 0 be a representative and define  This is a Carathéodory map [109, Definition 8.2.7]. By Theorem 8.2.11 in [109] there exists v ′ measurable such that  By Assumption 3, ϕ + ε ( v ′ 0 ( x )) ≥ 0 and 0 ≤ v ′ ( x ) ≤ v ′ 0 ( x ) whence v ′ is bounded µ -a.e. Let v ∈ L ∞ µ (Ω) be its equivalence class. Let { (¯ u k , v k ) } n ∈ N be a minimizing sequence. As W S ∩ P is compact, without loss of generality we may assume { ¯ u k } k ∈ N has a limit ¯ u ∞ . Let T D ¯ u ′ k be a representative and let w ′ k := max( v ′ , T D u ′ k ) . Then w ′ k is µ -a.e. bounded. Let w k ∈ L ∞ µ (Ω) denote its equivalence class. By construction,  for any representative v ′ k . Therefore  whence { (¯ u k , w k ) } k ∈ N is also minimizing. By continuity of T D we conclude w k → max { v , T D ¯ u ∞ } whence ( ˜ P ε,v 0 ) has a solution.

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