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<front>
<journal-meta>
<journal-id journal-id-type="publisher-id">Front. Earth Sci.</journal-id>
<journal-title>Frontiers in Earth Science</journal-title>
<abbrev-journal-title abbrev-type="pubmed">Front. Earth Sci.</abbrev-journal-title>
<issn pub-type="epub">2296-6463</issn>
<publisher>
<publisher-name>Frontiers Media S.A.</publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="doi">10.3389/feart.2019.00065</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Earth Science</subject>
<subj-group>
<subject>Methods</subject>
</subj-group>
</subj-group>
</article-categories>
<title-group>
<article-title>The PiSpec: A Low-Cost, 3D-Printed Spectrometer for Measuring Volcanic SO<sub>2</sub> Emission Rates</article-title>
</title-group>
<contrib-group>
<contrib contrib-type="author" corresp="yes">
<name><surname>Wilkes</surname> <given-names>Thomas Charles</given-names></name>
<xref ref-type="aff" rid="aff1"><sup>1</sup></xref>
<xref ref-type="corresp" rid="c001"><sup>&#x002A;</sup></xref>
<uri xlink:href="http://loop.frontiersin.org/people/507822/overview"/>
</contrib>
<contrib contrib-type="author">
<name><surname>Pering</surname> <given-names>Tom David</given-names></name>
<xref ref-type="aff" rid="aff1"><sup>1</sup></xref>
<uri xlink:href="http://loop.frontiersin.org/people/461462/overview"/>
</contrib>
<contrib contrib-type="author">
<name><surname>McGonigle</surname> <given-names>Andrew John Samuel</given-names></name>
<xref ref-type="aff" rid="aff1"><sup>1</sup></xref>
<xref ref-type="aff" rid="aff2"><sup>2</sup></xref>
<uri xlink:href="http://loop.frontiersin.org/people/438779/overview"/>
</contrib>
<contrib contrib-type="author">
<name><surname>Willmott</surname> <given-names>Jon Raffe</given-names></name>
<xref ref-type="aff" rid="aff3"><sup>3</sup></xref>
</contrib>
<contrib contrib-type="author">
<name><surname>Bryant</surname> <given-names>Robert</given-names></name>
<xref ref-type="aff" rid="aff1"><sup>1</sup></xref>
<uri xlink:href="http://loop.frontiersin.org/people/243373/overview"/>
</contrib>
<contrib contrib-type="author">
<name><surname>Smalley</surname> <given-names>Alan Lomas</given-names></name>
<xref ref-type="aff" rid="aff1"><sup>1</sup></xref>
<uri xlink:href="http://loop.frontiersin.org/people/614858/overview"/>
</contrib>
<contrib contrib-type="author">
<name><surname>Mims</surname> <given-names>Forrest Marion</given-names> <suffix>III</suffix></name>
<xref ref-type="aff" rid="aff4"><sup>4</sup></xref>
<uri xlink:href="http://loop.frontiersin.org/people/711356/overview"/>
</contrib>
<contrib contrib-type="author">
<name><surname>Parisi</surname> <given-names>Alfio V.</given-names></name>
<xref ref-type="aff" rid="aff5"><sup>5</sup></xref>
<uri xlink:href="http://loop.frontiersin.org/people/463491/overview"/>
</contrib>
<contrib contrib-type="author">
<name><surname>England</surname> <given-names>Rebecca Anne</given-names></name>
<xref ref-type="aff" rid="aff1"><sup>1</sup></xref>
</contrib>
</contrib-group>
<aff id="aff1"><sup>1</sup><institution>Department of Geography, The University of Sheffield</institution>, <addr-line>Sheffield</addr-line>, <country>United Kingdom</country></aff>
<aff id="aff2"><sup>2</sup><institution>School of Geosciences, The University of Sydney</institution>, <addr-line>Sydney, NSW</addr-line>, <country>Australia</country></aff>
<aff id="aff3"><sup>3</sup><institution>Department of Electronic and Electrical Engineering, The University of Sheffield</institution>, <addr-line>Sheffield</addr-line>, <country>United Kingdom</country></aff>
<aff id="aff4"><sup>4</sup><institution>Geronimo Creek Observatory</institution>, <addr-line>Seguin, TX</addr-line>, <country>United States</country></aff>
<aff id="aff5"><sup>5</sup><institution>Faculty of Health, Engineering and Sciences, University of Southern Queensland</institution>, <addr-line>Toowoomba, QLD</addr-line>, <country>Australia</country></aff>
<author-notes>
<fn fn-type="edited-by"><p>Edited by: John Stix, McGill University, Canada</p></fn>
<fn fn-type="edited-by"><p>Reviewed by: Ryunosuke Kazahaya, Geological Survey of Japan (AIST), Japan; J. Maarten De Moor, OVSICORI-UNA, Costa Rica</p></fn>
<corresp id="c001">&#x002A;Correspondence: Thomas Charles Wilkes, <email>tcwilkes1@sheffield.ac.uk</email></corresp>
<fn fn-type="other" id="fn002"><p>This article was submitted to Volcanology, a section of the journal Frontiers in Earth Science</p></fn>
</author-notes>
<pub-date pub-type="epub">
<day>16</day>
<month>04</month>
<year>2019</year>
</pub-date>
<pub-date pub-type="collection">
<year>2019</year>
</pub-date>
<volume>7</volume>
<elocation-id>65</elocation-id>
<history>
<date date-type="received">
<day>14</day>
<month>09</month>
<year>2018</year>
</date>
<date date-type="accepted">
<day>14</day>
<month>03</month>
<year>2019</year>
</date>
</history>
<permissions>
<copyright-statement>Copyright &#x00A9; 2019 Wilkes, Pering, McGonigle, Willmott, Bryant, Smalley, Mims, Parisi and England.</copyright-statement>
<copyright-year>2019</copyright-year>
<copyright-holder>Wilkes, Pering, McGonigle, Willmott, Bryant, Smalley, Mims, Parisi and England</copyright-holder>
<license xlink:href="http://creativecommons.org/licenses/by/4.0/"><p>This is an open-access article distributed under the terms of the Creative Commons Attribution License (CC BY). The use, distribution or reproduction in other forums is permitted, provided the original author(s) and the copyright owner(s) are credited and that the original publication in this journal is cited, in accordance with accepted academic practice. No use, distribution or reproduction is permitted which does not comply with these terms.</p></license>
</permissions>
<abstract>
<p>Spectroscopy has been used to quantify volcanic gas emission rates, most commonly SO<sub>2</sub>, for a number of decades. Typically, commercial spectrometers costing 1000s USD are employed for this purpose. The PiSpec is a new, custom-designed, 3D-printed spectrometer based on smartphone sensor technology. This unit has &#x2248;1 nm spectral resolution and a spectral range in the ultraviolet of &#x2248;280&#x2013;340 nm, and is specifically configured for the remote sensing of SO<sub>2</sub> using Differential Optical Absorption Spectroscopy (DOAS). Here we report on the first field deployment of the PiSpec on a volcano, to demonstrate the proof of concept of the device&#x2019;s functionality in this application area. The study was performed on Masaya Volcano, Nicaragua, which is one of the largest emitters of SO<sub>2</sub> on the planet, during a period of elevated activity where a lava lake was present in the crater. Both scans and traverses were performed, with resulting emission rates ranging from 3.2 to 45.6 kg s<sup>&#x2212;1</sup> across two measurement days; these values are commensurate with those reported elsewhere in the literature during this activity phase (<xref ref-type="bibr" rid="B1">Aiuppa et al., 2018</xref>; <xref ref-type="bibr" rid="B36">Stix et al., 2018</xref>). Furthermore, we tested the PiSpec&#x2019;s thermal stability, finding a wavelength shift of 0.046 nm/&#x00B0;C between 2.5 and 45&#x00B0;C, which is very similar to that of some commercial spectrometers. Given the low build cost of these units (&#x2248;500 USD for a one-off build, with prospects for further price reduction with volume manufacture), we suggest these units hold considerable potential for volcano monitoring operations in resource limited environments.</p>
</abstract>
<kwd-group>
<kwd>UV spectroscopy</kwd>
<kwd>DOAS</kwd>
<kwd>sulfur dioxide</kwd>
<kwd>volcanic emissions</kwd>
<kwd>Masaya volcano</kwd>
<kwd>smartphone sensor</kwd>
<kwd>Raspberry Pi</kwd>
<kwd>3D printing</kwd>
</kwd-group>
<contract-num rid="cn001">EP/M009106/1</contract-num>
<contract-num rid="cn002">Department of Geography Scholarship</contract-num>
<contract-num rid="cn002">GLOSS studentship</contract-num>
<contract-sponsor id="cn001">Engineering and Physical Sciences Research Council<named-content content-type="fundref-id">10.13039/501100000266</named-content></contract-sponsor>
<contract-sponsor id="cn002">University of Sheffield<named-content content-type="fundref-id">10.13039/501100000858</named-content></contract-sponsor>
<counts>
<fig-count count="7"/>
<table-count count="2"/>
<equation-count count="2"/>
<ref-count count="51"/>
<page-count count="12"/>
<word-count count="0"/>
</counts>
</article-meta>
</front>
<body>
<sec><title>Introduction</title>
<p>Ground-based remote sensing of sulfur dioxide (SO<sub>2</sub>) emissions from volcanoes has been performed for a number of decades, aiding in both monitoring efforts and volcanic research (e.g., <xref ref-type="bibr" rid="B51">Young et al., 1998</xref>; <xref ref-type="bibr" rid="B34">Shinohara et al., 2008</xref>; <xref ref-type="bibr" rid="B2">Arellano et al., 2017</xref>). Differential Optical Absorption Spectroscopy (DOAS) is the most commonly applied retrieval approach, utilizing the distinct absorption features of SO<sub>2</sub>, most commonly in the &#x2248;300&#x2013;325 nm wavelength range (<xref ref-type="bibr" rid="B31">Platt and Stutz, 2008</xref>). A variety of instrument designs and deployment modes have been proposed and employed within this scientific community: Multi AXis DOAS (MAX-DOAS; e.g., <xref ref-type="bibr" rid="B16">H&#x00F6;nninger et al., 2004</xref>; <xref ref-type="bibr" rid="B4">Bobrowski et al., 2007</xref>; <xref ref-type="bibr" rid="B10">Galle et al., 2010</xref>), walking traverses (e.g., <xref ref-type="bibr" rid="B25">McGonigle et al., 2002</xref>), road traverses (<xref ref-type="bibr" rid="B25">McGonigle et al., 2002</xref>; <xref ref-type="bibr" rid="B11">Galle et al., 2003</xref>; <xref ref-type="bibr" rid="B33">Salerno et al., 2009</xref>), airborne traverses (<xref ref-type="bibr" rid="B11">Galle et al., 2003</xref>; <xref ref-type="bibr" rid="B26">McGonigle et al., 2004</xref>; <xref ref-type="bibr" rid="B14">Grutter et al., 2008</xref>), high time-resolution fixed field of view deployments (e.g., <xref ref-type="bibr" rid="B23">McGonigle et al., 2009</xref>; <xref ref-type="bibr" rid="B38">Tamburello et al., 2011</xref>) and satellite remote sensing (e.g., <xref ref-type="bibr" rid="B19">Khokhar et al., 2005</xref>; <xref ref-type="bibr" rid="B32">Rix et al., 2009</xref>; <xref ref-type="bibr" rid="B39">Theys et al., 2015</xref>). Airborne DOAS instruments have also been proposed as a means of improving aviation safety related to volcanic hazard, by providing early detection of volcanic plumes (<xref ref-type="bibr" rid="B43">Vogel et al., 2011</xref>). Most prominently in volcanology, the Network for Observation of Volcanic and Atmospheric Change (NOVAC) project has led to the deployment of a large number of scanning spectrometers at volcanoes across the globe, monitoring SO<sub>2</sub> emissions along with other gas species (<xref ref-type="bibr" rid="B10">Galle et al., 2010</xref>).</p>
<p>Recently, we have developed the PiSpec, a 3D-printed UV spectrometer based on a detector primarily designed for the smartphone market (<xref ref-type="bibr" rid="B49">Wilkes et al., 2017</xref>). The sensor, here packaged as part of a Raspberry Pi camera module, is modified by removal of its Bayer filter, as described in <xref ref-type="bibr" rid="B48">Wilkes et al. (2016)</xref>, to deliver significant enhancement in UV sensitivity. This instrument provides a relatively low-cost alternative to off-the-shelf commercially available UV spectrometers (&#x2248;500 USD vs. &#x003E;1000 USD), with the potential to drive costs down further with mass production. Furthermore, the presented methodology allows researchers to quite easily design and build new spectrometers with spectral ranges and resolutions specifically tailored for their desired applications. The initial article (<xref ref-type="bibr" rid="B49">Wilkes et al., 2017</xref>) highlighted that this specific PiSpec design has the performance to facilitate DOAS retrievals of SO<sub>2</sub>, with comparable functionality to a commercial USB2000 (Ocean Optics, Inc.) instrument. However, those relatively rudimentary tests, using SO<sub>2</sub> filled quartz cells, did not rigorously assess the spectrometer&#x2019;s performance under representative field deployment conditions, which can often be more challenging than isolated laboratory experiments, for example, involving road traverses on bumpy roads or large changes in ambient temperatures. Here, we therefore present the first deployment of the PiSpec on a volcano, in this case at Masaya volcano (11&#x00B0;59&#x2032;3.65&#x2033; N, 86&#x00B0;10&#x2032;5.28&#x2033; W), Nicaragua, to demonstrate its performance under &#x201C;real world&#x201D; field conditions. Both scanning and road traverse retrievals are presented from this campaign, which took place during a period of heightened activity, whilst a lava lake was present in the crater. Furthermore, since spectrometers can be subjected to a wide range of ambient conditions during field deployments, we also characterize the thermal stability of the spectrometer via laboratory tests.</p>
</sec>
<sec id="s1" sec-type="materials|methods">
<title>Materials and Methods</title>
<sec><title>Measurement and Retrieval Technique</title>
<p>The PiSpec instrument design is described in detail in <xref ref-type="bibr" rid="B49">Wilkes et al. (2017)</xref>. It is based on a Czerny-Turner optical bench layout, with off-the-shelf optical components mounted in a 3D-printed housing. Light enters through a slit aperture and is collimated using a mirror, before falling incident onto a diffraction grating; the dispersed light is then focused onto a detector, to provide a system spectral resolution and range of &#x2248;1 nm and &#x2248;280&#x2013;340 nm, respectively. The detector is an Omnivision OV5647 sensor, primarily designed for the smartphone market, but here packaged as part of the Raspberry Pi v1.3 camera module (Raspberry Pi Foundation). This camera board has the advantage of greater user control, such as raw 10-bit data access and better gain control, relative to sensors incorporated into smartphone units themselves. Furthermore, this board-based configuration makes the sensor more readily accessible, such that we are able to chemically remove the Bayer filter, as described by <xref ref-type="bibr" rid="B48">Wilkes et al. (2016)</xref>; this produces a uniformly responding sensor with enhanced UV sensitivity, both of which are crucial features for this application area. The detector acquisition is controlled by a Raspberry Pi computer, which in turn is controlled by a custom Python 3 graphical user interface run on a Windows laptop. As in <xref ref-type="bibr" rid="B49">Wilkes et al. (2017)</xref>, all spectra captured herein have been generated by co-adding 11 rows across the PiSpec sensor, to increase the signal-to-noise ratio (SNR).</p>
<p>We have previously demonstrated that the instrument has &#x2248;1 nm spectral resolution and a spectral range of &#x2248;280&#x2013;340 nm, with a 30 &#x03BC;m slit in place. This implementation makes it well tailored for DOAS retrievals of SO<sub>2</sub>, following approaches which are extensively documented elsewhere (<xref ref-type="bibr" rid="B11">Galle et al., 2003</xref>; <xref ref-type="bibr" rid="B31">Platt and Stutz, 2008</xref>). In brief, the method involves collection of a clear-sky Fraunhofer spectrum, <italic>I</italic><sub>0</sub>(&#x03BB;), with which subsequent in-plume spectra, <italic>I</italic>(&#x03BB;), can be used to calculate the plume optical density, <italic>D</italic>(&#x03BB;):</p>
<disp-formula id="E1"><label>(1)</label><mml:math id="M1"><mml:mrow><mml:mi>D</mml:mi><mml:mo stretchy='false'>(</mml:mo><mml:mtext>&#x03BB;</mml:mtext><mml:mo stretchy='false'>)</mml:mo><mml:mo>=</mml:mo><mml:mi>ln</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mfrac><mml:mrow><mml:msub><mml:mi>I</mml:mi><mml:mn>0</mml:mn></mml:msub><mml:mo stretchy='false'>(</mml:mo><mml:mtext>&#x03BB;</mml:mtext><mml:mo stretchy='false'>)</mml:mo></mml:mrow><mml:mrow><mml:mi>I</mml:mi><mml:mo stretchy='false'>(</mml:mo><mml:mtext>&#x03BB;</mml:mtext><mml:mo stretchy='false'>)</mml:mo></mml:mrow></mml:mfrac></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:math></disp-formula>
<p>The differential optical density, <italic>D</italic>&#x2032;(&#x03BB;), can then be isolated through applying a high-pass filter to <italic>D</italic>(&#x03BB;); here, we use a Butterworth high-pass filter implemented in MATLAB<sup>&#x00AE;</sup>. A reference spectrum of the SO<sub>2</sub> absorption cross-section, such as that provided by <xref ref-type="bibr" rid="B41">Vandaele et al. (2009)</xref>, is then convolved with the instrument&#x2019;s line shape and high-pass filtered also. This spectrum is then fitted to <italic>D</italic>&#x2032;(&#x03BB;), using a least-squares method, such that the scaling factor of the fit provides the column density of SO<sub>2</sub> for that spectral acquisition. An O<sub>3</sub> absorption spectrum (taken from the HITRAN database; <xref ref-type="bibr" rid="B12">Gordon et al., 2017</xref>) is similarly fitted, to remove effects from this species, which also has distinct absorption features within the spectral fitting window; SO<sub>2</sub> column densities retrieved with and without this O<sub>3</sub> correction differed by &#x003C;2%. In this work, the fitting window was manually determined for each spectrum, by assessing the degree of saturation present at shorter wavelengths when large column densities of SO<sub>2</sub> were present; we then ensured that a sufficiently long start wavelength for the fitting window was chosen in order to avoid this saturation. Typically, for larger column densities a fit window of &#x2248;314&#x2013;324 nm was used, which we later show is linear up to &#x2248;4000 ppm &#x22C5; m. Whilst fitting window determination could be automated for the PiSpec, as with any other DOAS instrument (<xref ref-type="bibr" rid="B44">Vogel et al., 2013</xref>), this was not the purpose of this study.</p>
<p>In practice, spectra <italic>I</italic><sub>0</sub>(&#x03BB;) and <italic>I</italic>(&#x03BB;) first must be corrected for dark current and stray light. Firstly, for the former a dark spectrum was acquired with the entrance optics blocked, in this case with a lens cap covering the lens. On Masaya, the dark acquisitions were made immediately prior to or after a full scan/traverse sequence. The dark spectrum is then subtracted from all spectra. Stray light was subsequently corrected for by subtracting the average digital number (DN) between &#x2248;285&#x2013;295 nm from the entire spectrum. At these wavelengths, the irradiance at the Earth&#x2019;s surface is negligible, due to strong absorption by Ozone, therefore, the signal at the detector should be &#x2248;0. In reality this is not the case, due to stray light within the spectrometer, which is assumed to be uniform across the detector.</p>
<p>For the PiSpec&#x2019;s entrance slit we predominantly used the 30 &#x03BC;m slit aperture; however, for some field traverses we tested a 50 &#x03BC;m slit to explore the outcomes of increased light throughput, with associated reduction in required exposure times. This modification does, however, result in decreased spectral resolution, which can be detrimental to the DOAS retrievals.</p>
</sec>
<sec><title>Thermal Stability</title>
<p>Volcanoes can be located in a range of extreme environments, often found at low temperatures due to their altitude, or in hot conditions from direct sun exposure at lower latitudes. Since spectrometers can be sensitive to changes in thermal conditions, shifting and warping the line function (e.g., <xref ref-type="bibr" rid="B31">Platt and Stutz, 2008</xref>), it is important to address this issue as part of evaluating the PiSpec&#x2019;s utility in volcanic surveillance operations.</p>
<p>These tests were performed by acquiring spectra from a Hg-Ar lamp (Ocean Optics, Inc.) coupled to the PiSpec by an optical fiber. This setup was placed in an incubator (Panasonic MIR-254-PE), set on Low Humidity Mode, to expose it to temperatures between &#x2248;0 and 50&#x00B0;C. The PiSpec was further placed inside a plastic pouch containing silica gel, to reduce humidity and prevent condensation; within this pouch the lowest temperature actually achieved was 2.5&#x00B0;C. Temperature was logged every minute using a LogTag<sup>&#x00AE;</sup> HAXO-8 recorder. At each temperature setting a repose period of &#x2248;1 h was applied before acquisition, to allow the pouch to equilibrate with the incubator temperature. The tests spanned 2 days, 19&#x2013;20 June 2018.</p>
</sec>
<sec><title>Field Deployment</title>
<p>The PiSpec was tested on Masaya volcano, Nicaragua, on the 14th (19:20 to 21:30 UTC) and 16th of June 2017 (16:40 to 18:20 UTC). At this time, a vigorously overturning lava lake was emplaced in Masaya&#x2019;s Santiago crater. The lake, which has been visible since late 2015 (<xref ref-type="bibr" rid="B42">Venzke, 2017</xref>), has been the subject of only a few published articles to date (<xref ref-type="bibr" rid="B1">Aiuppa et al., 2018</xref>; <xref ref-type="bibr" rid="B35">Stephens and Wauthier, 2018</xref>; <xref ref-type="bibr" rid="B50">Wilkes et al., 2018</xref>; <xref ref-type="bibr" rid="B30">Pering et al., 2019</xref>). SO<sub>2</sub> emission rates from the crater, measured with a NOVAC scanning-DOAS system, have been highly variable since the lake appeared, with measured fluxes ranging between 0 and 50 kg s<sup>&#x2212;1</sup> (<xref ref-type="bibr" rid="B1">Aiuppa et al., 2018</xref>). Between 2005 and 2015, <xref ref-type="bibr" rid="B5">Carn et al. (2017)</xref> listed Masaya as the 18th largest passive volcanic emitter of SO<sub>2</sub> on earth. Furthermore, due to the low elevation of Masaya&#x2019;s crater, and hence its plume, emissions can have a considerable impact on surrounding vegetation and communities (<xref ref-type="bibr" rid="B7">Delmelle et al., 2002</xref>).</p>
<p>We deployed the PiSpec to acquire under two distinct observation modes: scanning-DOAS (14th June) and road traverses (16th June). For the former set up, tests were performed close to the vent, manually scanning horizontally through the plume whilst it was still rising buoyantly from the crater. Contemporaneous visible video was acquired with a DSLR camera, allowing plume transport speed determinations by tracking the condensed plume. This was based on integrating the pixel brightness over two cross sections through the rising plume, then generating time series for each of these feeds, which were cross correlated in order to determine the temporal lag between them. This follows the commonly applied approach in both spectral and image based determinations of plume speed in volcanic SO<sub>2</sub> emission rate estimations (<xref ref-type="bibr" rid="B24">McGonigle et al., 2005</xref>; <xref ref-type="bibr" rid="B28">Mori and Burton, 2006</xref>). Indeed, in settings where a volcanic plume is persistently condensed, this also demonstrates that visible imagery can provide an effective low-cost method of retrieving plume speeds for a DOAS instrument.</p>
<p>Uncertainties associated with the cross-correlation technique are dominated by knowledge of the distance from observer to camera, and the angle of plume motion relative to the normal of the camera viewing direction, i.e., plume speed has a 1/cos&#x03B1; dependency on relative angle of plume motion, where &#x03B1; is the angular offset from a plume motion that is perpendicular to the camera viewing direction (<xref ref-type="bibr" rid="B20">Klein et al., 2017</xref>). For the scans in particular, since they were located close to the source, the relative uncertainty associated with distance to the plume dominates the total uncertainty; it was estimated to be &#x2248;&#x00B1; 0.2 (20%). Conversely, even with a relatively large absolute uncertainty for the angle of plume motion (estimated to be &#x2248;&#x00B1; 10&#x00B0;), the associated relative uncertainty is small (&#x2248;&#x00B1; 0.02).</p>
<p>Road traverses were performed by supporting the PiSpec out of a car window and continuously acquiring GPS receiver (Adafruit Ultimate GPS breakout) geo-referenced spectra whilst driving under the plume on La Carretera a Masaya, located to the north east of the Santiago crater (see <xref ref-type="fig" rid="F1">Figure 1</xref>). These measurements were made under rather rare conditions, with the plume blowing approximately north-north-east, making La Carretera a Masaya the optimal route for traverses; the prevailing wind direction is approximately from the east, as evidenced by the SO<sub>2</sub> impacts on plant growth on the western side of the volcano. At times, overhanging trees may have interfered with the traverse spectra; however, we were careful to pause acquisitions when large regions of obstruction were encountered. In general, the quality of fitted SO<sub>2</sub> spectra suggests that significant issues from trees were avoided. Plume speed, again, was estimated using visible video acquired shortly before we began the traverses, and using cross correlation. Traverse emission rates were then computed from the wind, GPS and spectral concentration data following the methodology outlined by <xref ref-type="bibr" rid="B22">McGonigle (2007)</xref>.</p>
<fig id="F1" position="float">
<label>FIGURE 1</label>
<caption><p>Traverse SO<sub>2</sub> column densities (ppm &#x22C5; m) plotted in bars for two traverses started at 17:46:01 UTC (red) and 17:55:10 UTC (blue); emission rates were 16.3 and 27.2 kg s<sup>&#x2212;1</sup>, respectively. Traverses were performed along La Carretera a Masaya. Base map topographic data retrieved from <xref ref-type="bibr" rid="B40">USGS (2018)</xref>. Data for this figure, and all other figures in this manuscript, are available in <xref ref-type="supplementary-material" rid="SM1">Supplementary Data Sheet S1</xref>.</p></caption>
<graphic xlink:href="feart-07-00065-g001.tif"/>
</fig>
</sec>
</sec>
<sec><title>Results and Discussion</title>
<sec><title>Comparison of the PiSpec With the USB2000</title>
<p>A number of commercial spectrometers are currently used for DOAS applications in volcanology. Although it has now been discontinued, the USB2000 (Ocean Optics) was once perhaps the most commonly used spectrometer (e.g., <xref ref-type="bibr" rid="B11">Galle et al., 2003</xref>; <xref ref-type="bibr" rid="B29">Mori et al., 2006</xref>; <xref ref-type="bibr" rid="B17">Kantzas et al., 2009</xref>; <xref ref-type="bibr" rid="B3">Bobrowski et al., 2010</xref>), and therefore provides a good benchmark to compare the PiSpec against. This instrument is also very similar to the USB2000+ and Flame-S spectrometers, the next generation versions of the USB2000, which are currently market available and frequently used today. <xref ref-type="table" rid="T1">Table 1</xref> provides some useful features of these PiSpec, USB2000 and USB2000+ spectrometers, for comparison; the Flame-S specifications are very similar to that of the USB2000+, but the former instrument is manufactured with new techniques to improve thermal stability and reduce unit-to-unit variability. As may be expected, the Ocean Optics instruments have some advantages, such as a higher bit-depth (12-/16-bit for the USB2000/2000+ vs. 10-bit for the PiSpec) and, in this configuration, a greater spectral resolution (0.65 nm for the USB2000/2000+ vs. 1 nm for the PiSpec).</p>
<table-wrap position="float" id="T1">
<label>Table 1</label>
<caption><p>A comparison of the PiSpec with the USB2000 and USB2000+ (Ocean Optics).</p></caption>
<table cellspacing="5" cellpadding="5" frame="hsides" rules="groups">
<thead>
<tr>
<th valign="top" align="left"></th>
<th valign="top" align="center">PiSpec</th>
<th valign="top" align="center">USB2000</th>
<th valign="top" align="center">USB2000+</th>
</tr>
</thead>
<tbody>
<tr>
<td valign="top" align="left">Dimensions [mm]</td>
<td valign="top" align="center">80 &#x00D7; 75 &#x00D7; 57</td>
<td valign="top" align="center">89 &#x00D7; 63 &#x00D7; 34</td>
<td valign="top" align="center">89 &#x00D7; 63 &#x00D7; 34</td>
</tr>
<tr>
<td valign="top" align="left">Interface</td>
<td valign="top" align="center">CSI port</td>
<td valign="top" align="center">USB 2.0</td>
<td valign="top" align="center">USB 2.0</td>
</tr>
<tr>
<td valign="top" align="left"></td>
<td valign="top" align="center">(e.g., Raspberry Pi)</td>
<td valign="top" align="center">RS-232</td>
<td valign="top" align="center">RS-232</td>
</tr>
<tr>
<td valign="top" align="left">Sensor</td>
<td valign="top" align="center">Omnivision OV5647</td>
<td valign="top" align="center">Sony ILX511A</td>
<td valign="top" align="center">Sony ILX511A</td>
</tr>
<tr>
<td valign="top" align="left">Sensor Architecture</td>
<td valign="top" align="center">CMOS</td>
<td valign="top" align="center">CCD</td>
<td valign="top" align="center">CCD</td>
</tr>
<tr>
<td valign="top" align="left">Senor dimensions [pixels]</td>
<td valign="top" align="center">2592 &#x00D7; 1944</td>
<td valign="top" align="center">2048 &#x00D7; 1</td>
<td valign="top" align="center">2048 &#x00D7; 1</td>
</tr>
<tr>
<td valign="top" align="left">Bit depth</td>
<td valign="top" align="center">10</td>
<td valign="top" align="center">12</td>
<td valign="top" align="center">16</td>
</tr>
<tr>
<td valign="top" align="left">Spectral Resolution [nm]<sup>1</sup></td>
<td valign="top" align="center">&#x2248;1.0</td>
<td valign="top" align="center">0.65</td>
<td valign="top" align="center">0.65</td>
</tr>
<tr>
<td valign="top" align="left">Spectral Range [nm]<sup>1</sup></td>
<td valign="top" align="center">&#x2248;280&#x2013;340</td>
<td valign="top" align="center">&#x2248;250&#x2013;400</td>
<td valign="top" align="center">&#x2248;250&#x2013;400</td>
</tr>
<tr>
<td valign="top" align="left">Stray light/320 nm signal</td>
<td valign="top" align="center">0.034&#x2013;0.13</td>
<td valign="top" align="center">0.031&#x2013;0.12</td>
<td valign="top" align="center">0.050&#x2013;0.069</td>
</tr>
</tbody>
</table>
<table-wrap-foot>
<attrib><italic>Note the Ocean Optics spectrometers can be configured in a number of ways. This comparison presents a configuration which may be optimal for DOAS retrievals of SO<sub>2</sub>.</italic></attrib>
</table-wrap-foot>
</table-wrap>
<p>Contemporaneously acquired clear-sky spectra from both the PiSpec and USB2000 are displayed in <xref ref-type="fig" rid="F2">Figure 2</xref>. Both spectra have been corrected for dark current by subtracting a dark spectrum, and the signals have been normalized to the peak at &#x2248;330 nm to facilitate comparison. Prior to normalization, the 330 nm signals were 2147 and 487 for the USB2000 and PiSpec, respectively; for the 12- and 10-bit A/D converters, this corresponds to saturation of 52 and 48%, respectively. Shutter speeds of approximately 1.5 and 6 s were used in this case, for the USB2000 and PiSpec respectively, highlighting the greater sensitivity of the USB2000 device, as would be expected.</p>
<fig id="F2" position="float">
<label>FIGURE 2</label>
<caption><p>Clear sky spectra gathered by the PiSpec and USB2000. Both spectra have been dar-subtracted and then normalized to the peak at &#x2248;330 nm. This peak was at 48 and 52% saturation for the PiSpec and USB2000, respectively.</p></caption>
<graphic xlink:href="feart-07-00065-g002.tif"/>
</fig>
<p>In general, the spectra show similar features, although the peaks and troughs of the USB2000 spectrum are more pronounced than the PiSpec&#x2019;s. This is in accordance with the smaller instrument line shape (ILS) of the USB2000, which will more precisely preserve the high frequency oscillations in sky intensity. Below 330 nm, the signal in the PiSpec drops off somewhat faster than the USB2000. It is likely that this is due to the detector in the USB2000 being coated with a UV fluorescent coating, to enhance its UV sensitivity by absorbing UV radiation and emitting visible light which is sensed at the detector.</p>
<p>From these spectra, the stray light was quantified following the method of <xref ref-type="bibr" rid="B17">Kantzas et al. (2009)</xref>, by taking the ratio of stray light signal at approximately 290 nm to signal at 320 nm. Here, the stray light was quantified as 0.033 and 0.034 for the USB2000 and the PiSpec, respectively. These remarkably similar values are also toward the lower end of the range of values found by <xref ref-type="bibr" rid="B17">Kantzas et al. (2009)</xref>, who investigated three USB2000s, two USB2000+s, one USB4000 and one Avantes B.V. Avaspec-2048-USB2. Values ranged between 0.012 (Avaspec) and 0.12 (one USB2000). On a separate occasion, the PiSpec stray light was quantified as 0.13 (<xref ref-type="bibr" rid="B49">Wilkes et al., 2017</xref>), which remains comparable to the upper end of the aforementioned commercial spectrometers.</p>
<p>Of particular pertinence to this work, some comparison of the PiSpec and USB2000 was made by <xref ref-type="bibr" rid="B49">Wilkes et al. (2017)</xref>, where DOAS retrievals of quartz-filled SO<sub>2</sub> cells were performed with both instruments. The analysis of sets of 10 spectra acquired by each instrument showed that both resulted in similar column density retrievals when measuring &#x2248;300 and &#x2248;1200 ppm &#x22C5; m gas cells: 304 &#x00B1; 31 (&#x00B1;1 SD) and 1257 &#x00B1; 58 ppm &#x22C5; m for the PiSpec; 296 &#x00B1; 12 and 1184 &#x00B1; 30 ppm &#x22C5; m for the USB2000. Shutter speeds of 6 and 1.5 s were used for the PiSpec and USB2000, respectively. Whilst the performance of the USB2000 was somewhat more consistent for each cell (smaller standard deviation), the PiSpec&#x2019;s performance was still quite reasonable considering its lower price. From these tests, the maximum cell uncertainty for the PiSpec was &#x2248;10%, for the cell with the lower of the two SO<sub>2</sub> column densities. This value will be combined with the plume speed uncertainty to give a rough estimate of overall uncertainty in emission rate measurements presented in Section &#x201C;Traverse and Scanning DOAS.&#x201D;</p>
</sec>
<sec><title>Thermal Stability</title>
<p>Here, we discuss thermally induced changes in ILS and spectral calibration using the 313.150 nm emission line from the Hg-Ar lamp, in order to investigate the system robustness to variations in ambient conditions during field operations. This peak is located within typical fit windows for SO<sub>2</sub> DOAS retrievals, which are generally somewhere in the 300&#x2013;325 nm range. Our results suggest that the spectrometer calibration has a generally linear dependence on temperature across the considered range (<xref ref-type="fig" rid="F3">Figure 3</xref>); however, a few notable deviations from this trend are also apparent. Firstly, there appears to be no change in peak location between 20 and 25&#x00B0;C. This may partly be a result of the pixel discretization of a continuous spectrum. There is, however, some change in line shape, in keeping with the general trend (see <xref ref-type="fig" rid="F4">Figure 4</xref>). The second effect is apparent at the highest temperature measurements, &#x2248;50&#x00B0;C. Here, there is a large shift in the peak, which jumps &#x2248;1 nm from the 45&#x00B0;C spectrum. This notable displacement may be caused by a significant mechanical movement in one of the PiSpec&#x2019;s components, for example, the detector, via some release mechanism activated above a particular threshold. The similarity in line shape between the 45 and 50&#x00B0;C would corroborate this argument (<xref ref-type="fig" rid="F4">Figure 4</xref>). The detector and associated Pi Camera board is currently mounted to the spectrometer with nuts and bolts which may allow movement, especially under changing thermal conditions. Securing this part more stringently, with glue for instance, may prevent such issues, and it ought to be emphasized that the current hardware is very much a first version of this instrument. As we believe this issue to be independent of the general thermal stability characteristics of the spectrometer, we omit these data points from the regression analysis; we then also propose that above 45&#x00B0;C the PiSpec alignment may become unstable.</p>
<fig id="F3" position="float">
<label>FIGURE 3</label>
<caption><p>Thermal stability of the spectrometer displayed as wavelength change of the 313.155 nm mercury emission line with temperature. Shifts are shown relative to the peak location at 25&#x00B0;C. A linear regression model indicates a wavelength shift dependence of 0.046 nm/&#x00B0;C, with a good model fit of <italic>r</italic><sup>2</sup> = 0.97. The two high-temperature points, boxed in red, do not follow the linear trend, and may be caused by a larger scale shift in one of the optical components in the PiSpec. These data are not included in the regression analysis, since they are clearly associated with a different mechanism. Nevertheless, they should not be ignored, and suggest that at high temperatures &#x003E; 45&#x00B0;C the PiSpec may begin to become unstable. In general, such high temperatures should be easily avoidable by keeping the instrument out of direct sunlight.</p></caption>
<graphic xlink:href="feart-07-00065-g003.tif"/>
</fig>
<fig id="F4" position="float">
<label>FIGURE 4</label>
<caption><p>Normalized instrument line shapes for a number of temperatures displayed in <xref ref-type="fig" rid="F3">Figure 3</xref>. At low temperatures the line shape becomes quite broad, possibly preventing DOAS retrievals from being performed. Toward higher temperatures a double peak begins to form.</p></caption>
<graphic xlink:href="feart-07-00065-g004.tif"/>
</fig>
<p>The linear dependence, omitting the high temperature data as discussed above, indicates that the PiSpec displays wavelength shifts of &#x2248;0.046 nm/&#x00B0;C (&#x2248;0.5 pixel/&#x00B0;C) between &#x2248;2.5&#x2013;45&#x00B0;C; the coefficient of determination, <italic>r</italic><sup>2</sup> = 0.97, indicates that this linear model fits the wavelength shifts well across this temperature range. This thermal stability is in extremely good agreement with shifts quoted by <xref ref-type="bibr" rid="B31">Platt and Stutz (2008)</xref> of 0.05 nm/&#x00B0;C for commercial spectrometers, indicating that in this sense there is no trade off in using this lower cost unit for these spectral measurements. In terms of pixel shifts, <xref ref-type="bibr" rid="B31">Platt and Stutz (2008)</xref> quote a typical value of 0.1 pixel/&#x00B0;C, which is lower than the 0.5 pixel/&#x00B0;C for the PiSpec. This should not impact the PiSpec&#x2019;s performance, since the shift can be corrected for using software.</p>
<p>Thermal instabilities of spectrometers can also lead to a stretch or squeeze of spectra which goes beyond a simple linear shift of all wavelengths across the sensor (<xref ref-type="bibr" rid="B22">McGonigle, 2007</xref>; <xref ref-type="bibr" rid="B31">Platt and Stutz, 2008</xref>). To investigate this effect, widely separated emission lines (296.728 and 334.148 nm) were tracked through the spectra captured across the studied temperature range, and their separation in numbers of pixels were recorded. For all temperatures below 40&#x00B0;C these two peaks were separated by exactly 393 pixels, indicating that the peaks shifted simultaneously in the same direction. For the three spectra above 40&#x00B0;C the pixel separation moved to 392 pixels. Since each pixel in the PiSpec represents a 0.095 nm band, this squeeze in spectra remains relatively insignificant even at the quite extreme temperatures.</p>
<p>There is, however, a change in the ILS of the unit across this temperature range (see <xref ref-type="fig" rid="F4">Figure 4</xref>). In particular, at cooler temperatures the PiSpec&#x2019;s ILS is notably wider, with the spectral resolution, defined as the full-width-at-half-maximum of an emission line, increasing markedly. At 2.5&#x00B0;C this increases to 2.9 nm, which would likely be too broad to enable conventional SO<sub>2</sub> DOAS measurements. At 25&#x00B0;C the spectral resolution measured here is &#x2248;1.1 nm. An instrument with a broader ILS (lower spectral resolution) can have a lower sensitivity to SO<sub>2</sub>, especially when the ILS approaches the line width of the SO<sub>2</sub> absorption structures, where response can also become non-linear (<xref ref-type="bibr" rid="B9">Frankenberg et al., 2005</xref>; <xref ref-type="bibr" rid="B31">Platt and Stutz, 2008</xref>). This is likely to be the case beyond a spectral resolution of &#x2248;1 nm, therefore, a changing line shape induced by thermal instability could affect the PiSpec&#x2019;s retrievals of SO<sub>2</sub>. Linearity/non-linearity is discussed in more detail in Section &#x201C;Detection Limit and Linearity.&#x201D;</p>
<p><xref ref-type="bibr" rid="B17">Kantzas et al. (2009)</xref> show that the spectral resolution of commercial units (USB2000, Ocean Optics) is also impacted by changing ambient temperatures; however, the temperature range considered therein was not as extreme as that presented here. Another point made by <xref ref-type="bibr" rid="B17">Kantzas et al. (2009)</xref>, is that the line widths and thermal responses vary between spectrometers, even for the same model, and we note that the same should be expected of the PiSpec; to date, only one PiSpec instrument has been built and tested.</p>
<p>As discussed by <xref ref-type="bibr" rid="B31">Platt and Stutz (2008)</xref>, thermostating a spectrometer is the best means of preventing thermal instabilities from affecting DOAS retrievals. As with commercial spectrometers, here we highlight that the PiSpec would similarly benefit from such measures. Nevertheless, DOAS measurements with commercial instruments are frequently made without such controls in place, and our tests described later (see Traverse and Scanning DOAS) show that the PiSpec does appear to work adequately, at least within the range of conditions encountered in this study, without thermal stabilization. To some extent post processing of spectra, by wavelength shifting and squeezing/stretching the differential optical density array such that it better fits the SO<sub>2</sub> reference spectrum, can account for calibration error caused by thermal instability, as can measurements of gas cells containing known column amounts of SO<sub>2</sub>, and/or regular calibration with mercury lamps under the conditions encountered in the field. However, the change in ILS is more difficult to correct for, unless the change is well characterized. Inspecting the changes in ILS in <xref ref-type="fig" rid="F4">Figure 4</xref>, we may, therefore, suggest that the PiSpec could function acceptably within &#x2248;&#x00B1; 5&#x00B0;C of its calibration temperature; although this will still result in some error in retrieved column densities, as discussed earlier. <xref ref-type="bibr" rid="B27">Meroni et al. (2010)</xref> present a method for calibrating spectrometers using Fraunhofer lines and atmospheric absorption features, therefore providing a possible means of recalibration without the need for a calibration lamp in the field. In general, whilst short term deployments, such as the scans and traverses presented herein, are unlikely to be significantly affected by changing temperatures, permanent DOAS installations for automated monitoring can be subject to considerable changes in temperatures both on daily and seasonal timescales. As such, permanent installations with the PiSpec, as with commercial spectrometers, should consider measures to prevent or compensate for thermal instabilities in the instrumentation.</p>
</sec>
<sec><title>Traverse and Scanning DOAS</title>
<p>Seven spectrometer scans (<xref ref-type="table" rid="T2">Table 2</xref>) were performed on the Santiago crater rim. A typical scan and example DOAS retrieval are displayed in <xref ref-type="fig" rid="F5">Figure 5</xref>. The estimated plume rise speed of 3.9 &#x00B1; 0.8 m s<sup>&#x2212;1</sup>, obtained through cross-correlation, resulted in emission rates of between 3.2 &#x00B1; 0.7 and 7.3 &#x00B1; 1.7 kg s<sup>&#x2212;1</sup>, with a mean of 5.1 kg s<sup>&#x2212;1</sup>. Within these scans, column densities of up to &#x2248;2000 ppm &#x22C5; m SO<sub>2</sub> were measured. SO<sub>2</sub> emission rates from six road traverses ranged between 11.3 &#x00B1; 1.9 and 45.6 &#x00B1; 7.6 kg s<sup>&#x2212;1</sup> (<xref ref-type="fig" rid="F1">Figure 1</xref> shows two typical traverses); the mean traverse rate was 23.1 kg s<sup>&#x2212;1</sup>. In this case, a plume speed of 5.3 &#x00B1; 0.7 m s<sup>&#x2212;1</sup> was estimated, again from video imagery. Considering both the scan and traverse data, our mean recorded emission rate was 13.4 &#x00B1; 12.3 kg s<sup>&#x2212;1</sup> (&#x00B1;1 standard deviation).</p>
<table-wrap position="float" id="T2">
<label>Table 2</label>
<caption><p>A summary of scan and traverse emission rates measured with the PiSpec.</p></caption>
<table cellspacing="5" cellpadding="5" frame="hsides" rules="groups">
<thead>
<tr>
<th valign="top" align="left">Start Time (UTC)</th>
<th valign="top" align="center">End Time</th>
<th valign="top" align="center">Retrieval Mode</th>
<th valign="top" align="center">Plume Speed (m/s)</th>
<th valign="top" align="center">Emission Rate (kg/s)</th>
</tr>
</thead>
<tbody>
<tr>
<td valign="top" align="left">19:22:25</td>
<td valign="top" align="center">19:32:27</td>
<td valign="top" align="center">Scan</td>
<td valign="top" align="center">3.9 &#x00B1; 0.8</td>
<td valign="top" align="center">3.2 &#x00B1; 0.7</td>
</tr>
<tr>
<td valign="top" align="left">19:33:50</td>
<td valign="top" align="center">19:41:05</td>
<td valign="top" align="center">Scan</td>
<td valign="top" align="center">3.9 &#x00B1; 0.8</td>
<td valign="top" align="center">4.0 &#x00B1; 0.9</td>
</tr>
<tr>
<td valign="top" align="left">19:43:08</td>
<td valign="top" align="center">19:51:01</td>
<td valign="top" align="center">Scan</td>
<td valign="top" align="center">3.9 &#x00B1; 0.8</td>
<td valign="top" align="center">4.6 &#x00B1; 1.0</td>
</tr>
<tr>
<td valign="top" align="left">19:51:59</td>
<td valign="top" align="center">20:01:31</td>
<td valign="top" align="center">Scan</td>
<td valign="top" align="center">3.9 &#x00B1; 0.8</td>
<td valign="top" align="center">3.6 &#x00B1; 0.8</td>
</tr>
<tr>
<td valign="top" align="left">20:02:30</td>
<td valign="top" align="center">20:07:37</td>
<td valign="top" align="center">Scan</td>
<td valign="top" align="center">3.9 &#x00B1; 0.8</td>
<td valign="top" align="center">5.6 &#x00B1; 1.3</td>
</tr>
<tr>
<td valign="top" align="left">21:04:22</td>
<td valign="top" align="center">21:15:42</td>
<td valign="top" align="center">Scan</td>
<td valign="top" align="center">3.9 &#x00B1; 0.8</td>
<td valign="top" align="center">7.3 &#x00B1; 1.7</td>
</tr>
<tr>
<td valign="top" align="left">21:16:37</td>
<td valign="top" align="center">21:25:47</td>
<td valign="top" align="center">Scan</td>
<td valign="top" align="center">3.9 &#x00B1; 0.8</td>
<td valign="top" align="center">7.1 &#x00B1; 1.6</td>
</tr>
<tr>
<td valign="top" align="left">16:42:26</td>
<td valign="top" align="center">16:54:37</td>
<td valign="top" align="center">Traverse</td>
<td valign="top" align="center">5.3 &#x00B1; 0.7</td>
<td valign="top" align="center">45.6 &#x00B1; 7.6</td>
</tr>
<tr>
<td valign="top" align="left">17:02:39</td>
<td valign="top" align="center">17:12:18</td>
<td valign="top" align="center">Traverse</td>
<td valign="top" align="center">5.3 &#x00B1; 0.7</td>
<td valign="top" align="center">17.8 &#x00B1; 2.9</td>
</tr>
<tr>
<td valign="top" align="left">17:28:11</td>
<td valign="top" align="center">17:35:27</td>
<td valign="top" align="center">Traverse</td>
<td valign="top" align="center">5.3 &#x00B1; 0.7</td>
<td valign="top" align="center">20.5 &#x00B1; 3.4</td>
</tr>
<tr>
<td valign="top" align="left">17:46:01</td>
<td valign="top" align="center">17:54:33</td>
<td valign="top" align="center">Traverse</td>
<td valign="top" align="center">5.3 &#x00B1; 0.7</td>
<td valign="top" align="center">16.3 &#x00B1; 2.7</td>
</tr>
<tr>
<td valign="top" align="left">17:55:10</td>
<td valign="top" align="center">18:03:27</td>
<td valign="top" align="center">Traverse</td>
<td valign="top" align="center">5.3 &#x00B1; 0.7</td>
<td valign="top" align="center">27.2 &#x00B1; 4.5</td>
</tr>
<tr>
<td valign="top" align="left">18:08:21</td>
<td valign="top" align="center">18:17:39</td>
<td valign="top" align="center">Traverse</td>
<td valign="top" align="center">5.3 &#x00B1; 0.7</td>
<td valign="top" align="center">11.3 &#x00B1; 1.9</td>
</tr>
</tbody>
</table>
</table-wrap>
<fig id="F5" position="float">
<label>FIGURE 5</label>
<caption><p><bold>(A)</bold> Example DOAS retrieval (fit window of 314.5&#x2013;325 nm) from the scan presented in <bold>(B)</bold>. <bold>(B)</bold> A full PiSpec scan taken from the Santiago crater rim between 21:04 UTC and 21:15 UTC, on 14th June 2017. The resulting emission rate computed from the scan was 7.3 kg s<sup>&#x2212;1</sup>.</p></caption>
<graphic xlink:href="feart-07-00065-g005.tif"/>
</fig>
<p>Other available data to compare our emission rates against come from <xref ref-type="bibr" rid="B1">Aiuppa et al. (2018)</xref> and <xref ref-type="bibr" rid="B36">Stix et al. (2018)</xref>. The former data are derived from the NOVAC network scanning spectrometers in the period 19/07/2016&#x2013;01/03/2017, and range widely from &#x2248;0&#x2013;50 kg s<sup>&#x2212;1</sup>; however, most emission rates are below 25 kg s<sup>&#x2212;1</sup>. The mean emission rate is 7.9 &#x00B1; 3.5 kg s<sup>&#x2212;1</sup> (&#x00B1;1 standard deviation), with significant day to day variability in this period and no clear overall trend over this timescale. The work of <xref ref-type="bibr" rid="B36">Stix et al. (2018)</xref> implemented a drone-mounted DOAS system (DROAS) for traversing the Masaya plume between 04/05/2017 and 06/04/2017. Their measured fluxes ranged between 15 and 22 kg s<sup>&#x2212;1</sup>, with a mean of 18 kg s<sup>&#x2212;1</sup>. These measurements, which were made closer to the time of the work presented herein, are significantly higher than those of <xref ref-type="bibr" rid="B1">Aiuppa et al. (2018)</xref> on average, although they are comfortably within the extremes presented by the latter.</p>
<p>In general, our data are commensurate with the above fluxes from other authors, which were captured in the same activity period, in which Masaya&#x2019;s crater contained the lava lake. Notwithstanding the potential for changes in degassing between the three observation periods, the datasets do compare rather favorably, with all bar two of our fluxes falling within the range 0&#x2013;25 kg s<sup>&#x2212;1</sup>, which encompassed the majority of the <xref ref-type="bibr" rid="B1">Aiuppa et al. (2018)</xref> fluxes; all emission rates herein fall below their quoted maximum flux of 50 kg s<sup>&#x2212;1</sup> in this interval. Our traverse values are also in quite good agreement with the traverses of <xref ref-type="bibr" rid="B36">Stix et al. (2018)</xref>, with mean values of 23 and 18 kg s<sup>&#x2212;1</sup>, respectively.</p>
<p>Our scan data correspond to the quoted <xref ref-type="bibr" rid="B1">Aiuppa et al. (2018)</xref> fluxes rather better than the traverse data, with 4 of 7 scans falling within one standard deviation of their quoted mean; the further 3 are comfortably within 2 standard deviations. This might be expected given the comparison of scan to scan data, however, pushing this comparison further is perhaps tenuous in the sense that the scan orientations are rather different, e.g., the NOVAC scans are from a rather different vantage point; there is also the difference in the acquisition period. Our scan emission rates are rather lower than those from the traverse observations, which might be simply a manifestation of considerable and rapid (timescales of hours to days) variation in emission rate from the volcano, which is also apparent in the NOVAC fluxes reported in <xref ref-type="bibr" rid="B1">Aiuppa et al. (2018)</xref>. The traverse data are more commensurate with the traverses of <xref ref-type="bibr" rid="B36">Stix et al. (2018)</xref>, with both datasets containing notably larger average fluxes than the average of scans presented in <xref ref-type="bibr" rid="B1">Aiuppa et al. (2018)</xref>. Recently, <xref ref-type="bibr" rid="B6">de Moor et al. (2017)</xref> also found that a scanning-DOAS system systematically retrieved lower SO<sub>2</sub> fluxes than traverses when studying emissions from Turrialba in Costa Rica. It is not clear whether this is simply coincidental or whether it is caused by fundamental differences in how the scan/traverse retrieval modes are performed and processed. In their Supplementary Information, <xref ref-type="bibr" rid="B6">de Moor et al. (2017)</xref> provide a good discussion of possible causes for discrepancies, such as ash on the optics or sub-optimal scanning position; for a permanent station the latter is of course impossible to always prevent since wind direction is changeable. Some systematic over-/under-estimation in our data may also come from the plume speed scalar, since all scan emission rates are derived from a single plume speed and, likewise, all traverse emission rates are derived from a separate single plume speed. Any error in this calculated speed will therefore be propagated through all emission rates of that retrieval mode.</p>
<p>In concordance with our earlier vindication of the capacity of the PiSpec to accurately constrain cell SO<sub>2</sub> column amounts, via comparison with a USB2000 spectrometer (<xref ref-type="bibr" rid="B49">Wilkes et al., 2017</xref>), we suggest that the comparisons with NOVAC and DROAS data demonstrate the capability of the PiSpec to accurately retrieve volcanic SO<sub>2</sub> emission rates. Following the substantial contribution to volcano monitoring and research made by the NOVAC project in recent years (e.g., <xref ref-type="bibr" rid="B10">Galle et al., 2010</xref>; <xref ref-type="bibr" rid="B21">L&#x00FC;bcke et al., 2014</xref>; <xref ref-type="bibr" rid="B13">Granieri et al., 2015</xref>; <xref ref-type="bibr" rid="B15">Hidalgo et al., 2015</xref>; <xref ref-type="bibr" rid="B8">Dingwell et al., 2016</xref>; <xref ref-type="bibr" rid="B1">Aiuppa et al., 2018</xref>), we suggest that the low-cost self-built PiSpec could augment efforts to assess and mitigate volcanic hazards globally, by enabling further dissemination of DOAS measurement systems on active volcanoes.</p>
<p>Due to the relatively modest UV sensitivity of the low-cost PiSpec sensor, as we highlighted in <xref ref-type="bibr" rid="B49">Wilkes et al. (2017)</xref>, relatively long shutter speeds are required to provide the high SNR required for sensitive DOAS measurements. In the case of these scans and traverses, shutter speeds of up to 6 s were used when the unit was fitted with the 30 &#x03BC;m slit. This, coupled with apparently large overheads in the camera module&#x2019;s image capture, means that acquisition and transfer of each spectrum took &#x2248;30&#x2013;40 s. Whilst there is likely to be a software fix for this issue, at present this means that a scan takes some &#x2248;10 min to complete. This current performance would preclude the PiSpec from being used for high time resolution (&#x2248;1 Hz) applications, such as that presented by <xref ref-type="bibr" rid="B23">McGonigle et al. (2009)</xref> for integration of SO<sub>2</sub> fluxes with other high time resolution geophysical data. Traverse temporal durations are unaffected by this issue, but it will act to reduce the spatial resolution in comparison with what could be achieved with a commercial spectrometer, for a given traverse speed.</p>
<p>One hardware solution to capturing spectra faster is to implement a larger 50 &#x03BC;m slit aperture, which allowed shutter speeds to be reduced from 4.5&#x2013;6.0 s to 2.5&#x2013;4.0 s, with a considerable reduction in acquisition rate (capturing every 15&#x2013;20 s). This configuration was implemented in the final three traverses of the day. Both instrument setups measured similar emission rates, with no trend of over- or under-estimation for the larger aperture; this suggests that, at least in this context, the larger aperture configuration is a suitable solution to this issue. A further approach could be to co-add more rows of the sensor, e.g., essentially co-adding spectra, which could also result in significant increases in SNR, and hence the prospect to obtain higher acquisition rates by reducing shutter speeds (<xref ref-type="bibr" rid="B49">Wilkes et al., 2017</xref>). Such improvements to this system should be investigated further in the future.</p>
</sec>
<sec><title>Detection Limit and Linearity</title>
<p>Many volcanoes emit much smaller quantities of SO<sub>2</sub> than those measured here on Masaya volcano, whilst others can emit far more. It is therefore important that DOAS instruments are able to detect low column densities of SO<sub>2</sub> accurately, with a high SNR, and that the DOAS retrieval remains linear for higher column densities. Here we provide a quantitative assessment of the PiSpec&#x2019;s performance for detection of both low and high column densities of SO<sub>2</sub>.</p>
<p>As with other spectrometers, the PiSpec&#x2019;s ability to resolve SO<sub>2</sub> will depend on the measurement conditions and acquisition settings. This is highlighted by <xref ref-type="fig" rid="F6">Figure 6</xref>, which displays retrievals of relatively low column densities (86 and 112 ppm &#x22C5; m) from a PiSpec traverse (<xref ref-type="fig" rid="F6">Figure 6A</xref>) and scan (<xref ref-type="fig" rid="F6">Figure 6B</xref>) captured during the Masaya campaign. The scan retrieval shows much noisier absorbances, which is a result of lower signal during these measurements. The clear sky spectrum associated with this scan had a DN of just 50 at 311 nm, whilst the DN of the traverse clear spectrum was 326 at 311 nm. The latter will have a considerably larger SNR, which is preserved in the absorbance spectrum. Both spectra were acquired at the upper limit of the PiSpec&#x2019;s shutter speed range, i.e., with 6 s exposures; therefore, the lower signal in the scan could be caused by the time of day (&#x2248;3 pm local for the scan vs. &#x2248;11 am for the traverse), different sky conditions between these acquisition periods, and/or different viewing orientations.</p>
<fig id="F6" position="float">
<label>FIGURE 6</label>
<caption><p>Relatively low column density DOAS fits for <bold>(A)</bold> traverse and <bold>(B)</bold> scan modes on Masaya volcano. Also shown are noise spectra generated using a second clear-sky spectrum as <italic>I</italic>(&#x03BB;), as opposed to an in-plume spectrum (see Equation 1). Differences in noise levels results from different viewing geometries and conditions for the traverse and scan measurements.</p></caption>
<graphic xlink:href="feart-07-00065-g006.tif"/>
</fig>
<p>More exact determination of the instrument&#x2019;s detection limit was performed by analyzing the noise in an absorbance spectrum generated from two clear-sky images. Following <xref ref-type="bibr" rid="B37">Stutz and Platt (1996)</xref>, an estimation of the detection limit can be made with:</p>
<disp-formula id="E2"><label>(2)</label><mml:math id="M2"><mml:mrow><mml:msub><mml:mover accent='true'><mml:mi>D</mml:mi><mml:mo>&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mtext>limit</mml:mtext></mml:mrow></mml:msub><mml:mo>&#x2248;</mml:mo><mml:mtext>&#x03C3;</mml:mtext><mml:mo>&#x00D7;</mml:mo><mml:mfrac><mml:mn>6</mml:mn><mml:mrow><mml:msup><mml:mrow><mml:mo stretchy='false'>(</mml:mo><mml:mi>n</mml:mi><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn><mml:mo stretchy='false'>)</mml:mo></mml:mrow><mml:mrow><mml:mn>1</mml:mn><mml:mo>/</mml:mo><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac></mml:mrow></mml:math></disp-formula>
<p>where &#x03C3; is the standard deviation of an absorbance spectrum generated from two spectra containing no absorbing species and <italic>n</italic> is the number of pixels in the spectrum. <inline-formula><mml:math id="M3"><mml:mrow><mml:msub><mml:mover accent='true'><mml:mi>D</mml:mi><mml:mo>&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mtext>limit</mml:mtext></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> is the detection limit of the average optical density, which itself is defined by Stutz and Platt as three times the standard deviation of the reference spectrum; it provides a measure of the absorption strength of a given spectrum. It should be noted that the detection limit presented here is somewhat simplified; a much more complex procedure is discussed by <xref ref-type="bibr" rid="B37">Stutz and Platt (1996)</xref> and <xref ref-type="bibr" rid="B31">Platt and Stutz (2008)</xref>, however, this simplified algorithm has been shown to provide a relatively accurate estimation (within 10&#x2013;20% of the more complex method).</p>
<p>From clear sky spectra acquired in Masaya on the end of a traverse sequence, the absorbance noise &#x03C3; was 3.10 &#x00D7; 10<sup>&#x2212;3</sup>. In a fitting window of 85 pixels, such as that used in the DOAS fits in <xref ref-type="fig" rid="F6">Figure 6</xref>, this noise corresponds to a detection limit <inline-formula><mml:math id="M4"><mml:mrow><mml:msub><mml:mover accent='true'><mml:mi>D</mml:mi><mml:mo>&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mtext>limit</mml:mtext></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> of 2.03 &#x00D7; 10<sup>&#x2212;3</sup>. In the presence of residual structures, from unknown gas species or the instrument itself, the detection limit must be scaled by a correction factor of 3&#x2013;4 (<xref ref-type="bibr" rid="B31">Platt and Stutz, 2008</xref>). Here, we conservatively use 4, therefore, the average optical density detection limit is 8.11 &#x00D7; 10<sup>&#x2212;3</sup>. The resulting column density detection limit is 26 ppm &#x22C5; m SO<sub>2</sub>. Following the same methodology for the scan associated with <xref ref-type="fig" rid="F6">Figure 6B</xref>, a detection limit of 50 ppm &#x22C5; m was estimated. As can be seen, these values are case-specific and it is not possible to generate a single detection limit for the PiSpec instrument for all scenarios. Indeed, <inline-formula><mml:math id="M5"><mml:mrow><mml:msub><mml:mover accent='true'><mml:mi>D</mml:mi><mml:mo>&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mtext>limit</mml:mtext></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> will depend on field conditions, PiSpec acquisition settings and the DOAS fitting procedure. Nevertheless, the conservative detection limits presented here are quite reasonable.</p>
<p>The detection limits are an order of magnitude larger than the 2.5 ppm &#x22C5; m quoted by <xref ref-type="bibr" rid="B11">Galle et al. (2003)</xref> for a mini-DOAS instrument; however, it is not clear how they have defined the limit in their work. The limits discussed for the PiSpec are quite conservative, since they include a factor of four increase in <inline-formula><mml:math id="M6"><mml:mrow><mml:msub><mml:mover accent='true'><mml:mi>D</mml:mi><mml:mo>&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mtext>limit</mml:mtext></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> associated with the potential presence of residual structures in the spectra, following <xref ref-type="bibr" rid="B31">Platt and Stutz (2008)</xref>. Omitting this factor, the detection limit for the traverse discussed above would be 6.5 ppm &#x22C5; m, which is quite similar to the mini-DOAS. We suggest, however, that the more conservative estimate, 26 ppm &#x22C5; m in this case, is likely to be more realistic. This general picture of the PiSpec providing a somewhat reduced performance in terms of resolving gas column densities is also borne out in the prior work of <xref ref-type="bibr" rid="B49">Wilkes et al. (2017)</xref>, which is discussed in Section 3.1. Therein a series of 10 measurements of gas cells were made, with both a USB2000 and PiSpec unit, and the standard deviations of the retrieved column densities were assessed. In this case, the variability in gas column densities from the USB2000 was typically a factor of two below that of the PiSpec. This was for instrument integration times of 1.5 and 6 s for the USB2000 and PiSpec, respectively, which provided very similar levels of detector saturation at 330 nm (52 and 48%, respectively).</p>
<p>Conversely, at large column densities DOAS retrievals can become non-linear due to the spectral resolution of the spectrometer not perfectly resolving high frequency variations in the SO<sub>2</sub> absorption cross-section, and due to the fact that the natural logarithm and convolution with the ILS are not commutative operations (<xref ref-type="bibr" rid="B9">Frankenberg et al., 2005</xref>; <xref ref-type="bibr" rid="B46">Wenig et al., 2005</xref>; <xref ref-type="bibr" rid="B3">Bobrowski et al., 2010</xref>). Linearity of PiSpec DOAS retrievals was assessed by modeling the instrument response following <xref ref-type="bibr" rid="B45">Wagner et al. (2003)</xref> and <xref ref-type="bibr" rid="B18">Kern et al. (2017)</xref>. First a column density of SO<sub>2</sub> was assumed. This was used to generate an absorption spectrum through the Beer-Lambert law and use of a high resolution absorption cross-section from <xref ref-type="bibr" rid="B41">Vandaele et al. (2009)</xref>. This absorption spectrum was convolved with the PiSpec ILS and the natural logarithm taken; the resultant spectrum was then down-sampled to the pixel resolution of the PiSpec. Finally, a typical DOAS fit procedure was applied to this spectrum, using the ILS-convolved high resolution absorption cross-section spectrum.</p>
<p>The results of this model are displayed in <xref ref-type="fig" rid="F7">Figure 7</xref>, run for column densities of 0&#x2013;10000 ppm &#x22C5; m, in 1000 ppm &#x22C5; m increments, and for a fit window of 314&#x2013;324 nm. Up to 4000 ppm &#x22C5; m the fit is extremely linear, producing a retrieval of 3957 ppm &#x22C5; m for a true SO<sub>2</sub> column density of 4000 ppm &#x22C5; m. This indicates that for the majority of volcanic applications the PiSpec will perform linearly. In particular, all PiSpec measurements made on Masaya were comfortably within this extremely linear response interval. Since non-linearity becomes more pronounced at higher optical densities, shifting to longer wavelengths, where SO<sub>2</sub> is less strongly absorbing, is one method which could account for this saturation effect where necessary (<xref ref-type="bibr" rid="B3">Bobrowski et al., 2010</xref>); alternatively, the modeled response can be used to correct retrievals (<xref ref-type="bibr" rid="B45">Wagner et al., 2003</xref>; <xref ref-type="bibr" rid="B18">Kern et al., 2017</xref>).</p>
<fig id="F7" position="float">
<label>FIGURE 7</label>
<caption><p>Modeled PiSpec response to SO<sub>2</sub> in the fit window 314&#x2013;324 nm. The response shows the saturation effect, whereby larger optical depths become non-linearly related to column densities, becomes significant above &#x2248;4000 ppm &#x22C5; m. This model can be used to correct for retrieved column densities, or the DOAS fit window can be shifted to longer wavelengths to minimize the effect.</p></caption>
<graphic xlink:href="feart-07-00065-g007.tif"/>
</fig>
</sec>
</sec>
<sec><title>Conclusion</title>
<p>We have presented the first deployment of a custom-built spectrometer (PiSpec) for the retrieval of volcanic SO<sub>2</sub> emission rates. Both scanning and driving traverse DOAS modes were performed on Masaya volcano in June 2017, with both sets of results lying within the bounds of rates measured by NOVAC spectrometers in early 2017 (<xref ref-type="bibr" rid="B1">Aiuppa et al., 2018</xref>) and DROAS traverses in May 2017 (<xref ref-type="bibr" rid="B36">Stix et al., 2018</xref>). Furthermore, we show that the thermal stability of the PiSpec is similar to commercial units quoted by <xref ref-type="bibr" rid="B31">Platt and Stutz (2008)</xref>, with a wavelength shift of &#x2248;0.046 nm/&#x00B0;C within the range 2.5&#x2013;45&#x00B0;C. The PiSpec&#x2019;s line shape is seen to change markedly across this temperature range, as would be expected. Whilst detection limits depend on a number of external (e.g., weather) as well as internal instrumental factors, typically the PiSpec&#x2019;s detection limit was found to be less than &#x2248;50 ppm &#x22C5; m during its deployment on Masaya; in some idealistic scenarios, a limit of less than 10 ppm &#x22C5; m may be possible. These results demonstrate the utility of the PiSpec to deliver broadly comparable performance to commercial DOAS systems in terms of volcanic plume observations. This is significant given the low cost of the PiSpec and the potential for further cost reduction, with mass production, in that this unit could be particularly useful in resource-poor settings to provide valuable data for monitoring and fundamental science applications. We therefore suggest that dissemination of these instruments should be a principal forthcoming objective. Future work on this instrument should also focus on assessing its long-term performance in the field, as well as improvements to the mounting of components in the PiSpec, which may improve the instrument&#x2019;s thermal stability.</p>
</sec>
<sec><title>Author Contributions</title>
<p>TW primarily wrote the manuscript and performed the analyses. AM co-wrote the manuscript. TW, TP, and RE performed the field work. TW, AM, and JW designed the PiSpec instrument. RB co-supervised the project. AS assisted in thermal stability tests. AP and FM assisted in preparation of this manuscript.</p>
</sec>
<sec><title>Conflict of Interest Statement</title>
<p>The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.</p>
</sec>
</body>
<back>
<fn-group>
<fn fn-type="financial-disclosure">
<p><bold>Funding.</bold> TW was supported by a scholarship from the Department of Geography, University of Sheffield. TP and RE were supported by a University of Sheffield GLOSS studentship. JW acknowledges the support of an Engineering and Physical Sciences Research Council grant (EP/M009106/1).</p>
</fn>
</fn-group>
<ack>
<p>We would like to thank reviewers RK and MDM, and editor JS, for their detailed comments on the initial manuscript, which we feel have greatly improved the quality of the article. We would like to thank Ulrich Platt for a number of useful discussions pertinent to this work. We would also like to thank the Laboratory Staff in the Department of Geography, University of Sheffield, for their continued support of our research needs. We acknowledge the use of the Generic Mapping Tool (<xref ref-type="bibr" rid="B47">Wessel et al., 2013</xref>) for drawing <xref ref-type="fig" rid="F1">Figure 1</xref>.</p>
</ack>
<sec sec-type="supplementary material">
<title>Supplementary Material</title>
<p>The Supplementary Material for this article can be found online at: <ext-link ext-link-type="uri" xlink:href="https://www.frontiersin.org/articles/10.3389/feart.2019.00065/full#supplementary-material">https://www.frontiersin.org/articles/10.3389/feart.2019.00065/full#supplementary-material</ext-link></p>
<supplementary-material xlink:href="Data_Sheet_1.xlsx" id="SM1" mimetype="application/vnd.openxmlformats-officedocument.spreadsheetml.sheet" xmlns:xlink="http://www.w3.org/1999/xlink">
<label>DATA SHEET S1</label>
<caption><p>Data for the 7 figures included in the manuscript.</p></caption>
</supplementary-material>
</sec>
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