<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">OJAppS</journal-id><journal-title-group><journal-title>Open Journal of Applied Sciences</journal-title></journal-title-group><issn pub-type="epub">2165-3917</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/ojapps.2013.31002</article-id><article-id pub-id-type="publisher-id">OJAppS-29371</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Biomedical&amp;Life Sciences</subject><subject> Chemistry&amp;Materials Science</subject><subject> Computer Science&amp;Communications</subject><subject> Engineering</subject><subject> Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Estimating Circulation Patterns by Combining Velocity and Tracer Observations
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>eonid</surname><given-names>I. Piterbarg</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Leonid</surname><given-names>M. Ivanov</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>Naval Postgraduate School Moneterey, Monterey, USA</addr-line></aff><aff id="aff1"><addr-line>Department of Mathematics, University of Southern California Kaprielian Hall, Los Angeles, USA</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>piter@usc.edu(EIP)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>29</day><month>03</month><year>2013</year></pub-date><volume>03</volume><issue>01</issue><fpage>8</fpage><lpage>14</lpage><history><date date-type="received"><day>August</day>	<month>31,</month>	<year>2012</year></date><date date-type="rev-recd"><day>November</day>	<month>20,</month>	<year>2012</year>	</date><date date-type="accepted"><day>November</day>	<month>29,</month>	<year>2012</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
   A method is suggested for estimating unknown velocities by combining their sparse measurements with observations of a tracer on a fine grid advected by the underlined velocity field. The dependence of the estimation error on a coarseness parameter and parameters of the flow in question is investigated numerically using synthetic velocity fields typical for real oceanic circulation. In an advanced version of the estimation procedure uncertainty in the transport equation forcing is modeled via a fuzzy sets approach. We also compare the method with a traditional interpolation which is in contrast to the developed procedure unable to capture the flow details.
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</p></abstract><kwd-group><kwd>Data Fusion; Inverse Problem; Surface Velocities; Fuzzy Sets</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The problem of retrieving a surface circulation in the ocean from observations of tracers such as sea surface temperature and chlorophyll concentration has been intensively discussed for the decades [1-15] because of its great practical and theoretical importance. In general it is an ill-posed inverse problem since the current component tangent to the tracer lines never can be recovered [<xref ref-type="bibr" rid="scirp.29371-ref2">2</xref>]. For that reason different additional conjectures were used to get a unique solution such as a scale separation [5-8]. In alternative approaches optimizing an appropriate cost function was suggested [3,4,13] or tracer observations were assimilated in numerical models of oceanic circulation [<xref ref-type="bibr" rid="scirp.29371-ref14">14</xref>].</p><p>If there is an independent source of information on the surface velocities such as a circulation model output then the problem can be formulated in a well-posed fashion using multi-objective optimization ideas [16-18]. The present work extends these ideas to a new set up which is of great practical importance: to estimate a surface circulation from high resolution tracer observations and sparse measurements of the surface velocity itself.</p><p>Typically, direct measurements of the surface velocities in the ocean covering a significant area cannot provide a high degree of the space resolution because of technical difficulties and high cost of such measurements. For example the distance between ADCP (Acoustic Doppler Current Profiler) stations in NAVOCEANO shipboard surveys (California Coastal Region) is about 18.5 km. On the other hand the space resolution of satellite observations of the sea surface temperature and chlorophyll concentration is much higher, 2 km or less depending on a type of radiometers. Thus, a task is to optimally combine these two kinds of data to restore the true circulation with highest possible resolution.</p><p>Here we consider a simplified formulation of the problem as follows. Assume that an unknown 2D velocity field <img src="2-2310080\52702b50-0fd9-485e-84d9-d5e294965079.jpg" /> is observed on a coarse space grid <img src="2-2310080\b54dbe17-b4a3-4158-b004-16eded798554.jpg" /> at a fixed time<img src="2-2310080\7b2bfec5-ffd2-4e1d-ab89-725e28e95455.jpg" />. Then assume that two snapshots <img src="2-2310080\b06bbf05-64dc-4f55-b95d-853a3cc0972b.jpg" /> and <img src="2-2310080\28c98d23-0aa7-4fe5-8d15-b30253832a35.jpg" /> of a tracer field are available as well on a fine grid<img src="2-2310080\d0f1be8d-d744-480b-9bcd-c8ab0edf6c63.jpg" />, where the tracer concentration is covered by</p><disp-formula id="scirp.29371-formula55064"><label>(1)</label><graphic position="anchor" xlink:href="2-2310080\6362c273-ee85-44db-a158-31a47898cf85.jpg"  xlink:type="simple"/></disp-formula><p>with a poorly known forcing<img src="2-2310080\d346f528-f6a0-408c-aab7-6d70d24a1213.jpg" />.</p><p>The problem is to estimate the velocity field on the fine grid by optimally combining both sorts of observations.</p><p>We first discuss the problem when the forcing in (1) is completely known (Section 2). This is the case for satellite observations of sea surface temperature since they are usually accompanied with heat fluxes measurements. In Section 3 we extend the approach to a poorly known forcing modeling its uncertainty in terms of fuzzy sets. An aimed area of application is the ocean color (chlorophyll). An estimation algorithm is derived for the corresponding two-objective fuzzy optimization problem. Numerical experiments with few types of synthetic flows typical for real oceanic circulation are presented in Section 4. Brief conclusions are summed up in Section 5.</p></sec><sec id="s2"><title>2. Velocity Estimation under Completely Known Forcing</title><p>Let us fix a space point<img src="2-2310080\0a1effa6-ba0a-4df1-9e56-8975052c9ede.jpg" />, time moment <img src="2-2310080\257ec47c-3230-4c4b-86ea-1c51074d6f99.jpg" /> and assume <img src="2-2310080\5ea844be-38cd-4215-91f7-14806fcbf060.jpg" /> and spacing <img src="2-2310080\de933bfd-7900-45fb-91ee-4d72f5e6026e.jpg" /> of <img src="2-2310080\dfeb4557-e84d-4c8d-90eb-31cc7104c257.jpg" /> to be small enough such that <img src="2-2310080\5891f833-1170-4b40-bc0f-325d9fe382e1.jpg" /> and <img src="2-2310080\a1ff20f1-3356-44da-8a18-fd50c4ce5f02.jpg" /> can be accurately computed.</p><p>Denote by <img src="2-2310080\273b175d-5b20-463b-959c-279c8f31e4ee.jpg" /> the velocities measured at <img src="2-2310080\3e4ab396-5f21-4b9d-861e-0ba92dc613bc.jpg" /> nearest neighbors <img src="2-2310080\6c61ffbf-b467-4b44-9a1c-1915340d9bc9.jpg" /> of x on the coarse grid<img src="2-2310080\52d8bbd8-e147-4969-b378-0e2b61b90ee5.jpg" />. For the present purposes neither the number <img src="2-2310080\9d939464-208b-4df9-86bc-63ae77dace5e.jpg" /> nor the configuration of the neighbors matters. To estimate the velocity <img src="2-2310080\1f2343df-bb7f-4f60-8dec-1289ccc055f5.jpg" /> at <img src="2-2310080\24708b81-73cb-4801-b668-cdfba2fc53ba.jpg" /> we suggest to solve the following conditional optimization problem</p><p><img src="2-2310080\163e6c61-d2c2-4105-a6b7-242527df1abf.jpg" /></p><p>where <img src="2-2310080\d4af468b-413c-41d5-8469-5d0a5a92635d.jpg" /> are prescribed weights (matrices or scalars). A quadratic cost function is traditionally used in statistical estimation problems. In our context its advantage is that unconditional optimization of <img src="2-2310080\444b014e-7a69-413f-b675-6a82ea3770e9.jpg" /> leads to a linear interpolation widely used in oceanographic research.</p><p>The solution obtained by a standard procedure of Lagrangian multiplier is given by</p><disp-formula id="scirp.29371-formula55065"><label>(2)</label><graphic position="anchor" xlink:href="2-2310080\62b36051-cf76-44d4-ac18-7331f83b484f.jpg"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.29371-formula55066"><label>(3)</label><graphic position="anchor" xlink:href="2-2310080\f137f248-ffe5-42ca-a9af-d4edd07bb7ef.jpg"  xlink:type="simple"/></disp-formula><p>is the interpolated velocity. So, the resulting estimator consists of interpolation (the first term in (2)) and a correction according to the tracer observations (the second term).</p><p>The estimation skill for each time moment we measure by the error ratio</p><p><img src="2-2310080\a1ff1bcb-9851-40d1-a9a1-c2e647a308f3.jpg" /></p><p>where</p><p><img src="2-2310080\eb39d5f2-84f7-473e-b466-085d0ccc26cf.jpg" /></p><p><img src="2-2310080\0163f8f1-cdc4-4202-98cd-353d90729553.jpg" />is the true velocity and the summation is carried out over all the grid points in<img src="2-2310080\00295171-82d2-4c2b-a57f-63208967779f.jpg" />. The relative error <img src="2-2310080\875cc139-702e-47b8-859c-03fbd0174c7b.jpg" /> will be compared to the interpolation error</p><p><img src="2-2310080\f1df6a5d-ce0f-4d23-8adf-154de7d64122.jpg" /></p><p>where</p><p><img src="2-2310080\3f1803cd-5423-4d49-8e89-d68fbd072ec7.jpg" /></p><p>Under some idealistic assumptions it can be shown similarly to [<xref ref-type="bibr" rid="scirp.29371-ref17">17</xref>] that</p><disp-formula id="scirp.29371-formula55067"><label>(4)</label><graphic position="anchor" xlink:href="2-2310080\aa2039f5-d1e0-4f49-8d1b-82fa1ddf5377.jpg"  xlink:type="simple"/></disp-formula><p>i.e. theoretically speaking the method would give about <img src="2-2310080\7cd20aaf-923b-4a15-8ef1-1af44d9bcd0f.jpg" /> improvement comparing to the interpolation. In our numerical experiments with realistic flows shown below this number varies in the range 12% - 32%.</p></sec><sec id="s3"><title>3. Unknown Forcing</title><p>Here we assume that the forcing in (1) is not known, rather some reasonable confidence interval is available. Namely, one believes that</p><p><img src="2-2310080\e44578f7-afe5-495a-a0f0-5b71148c4490.jpg" /></p><p>where <img src="2-2310080\4f4a0795-2f39-4024-a756-f09b1e7d3252.jpg" /> is a given background and <img src="2-2310080\b406e1dc-5f15-4756-b194-e589f452e6df.jpg" /> is a margin depending on the location <img src="2-2310080\46c3ba19-4b39-419e-96ca-c89e4114023c.jpg" /> and moment <img src="2-2310080\ae48d082-5dbb-42ce-b9ad-f40a237ad66f.jpg" /> as well which henceforth are fixed. The tracer gradient on the right hand side is introduced to keep the velocity dimension for<img src="2-2310080\d254e8c1-54ae-4e90-a012-ba72bad06060.jpg" />.</p><p>Let us denote</p><p><img src="2-2310080\5aa754de-7bca-4878-9b32-a1cb85e248ee.jpg" /></p><p>then the last inequality is written as <img src="2-2310080\cf623d71-4ecb-4ad6-bb08-ccb84770426c.jpg" /> where</p><p><img src="2-2310080\4774add1-0005-4fb0-9745-c03260c7f581.jpg" /></p><p>To describe an uncertainty in knowledge of <img src="2-2310080\4b980220-86ac-4586-be76-05b6e116f5fc.jpg" /> we assume that <img src="2-2310080\97ac5755-241a-405e-a927-e8b07bfc3d76.jpg" /> is a fuzzy number with a membership function <img src="2-2310080\a26ad071-3a14-4db4-8b83-a64dd42e5e18.jpg" /> such that <img src="2-2310080\ac289ee8-e2d6-47d6-8987-084fbbb0af26.jpg" /> and <img src="2-2310080\f6e8ac40-9cc2-4d11-9528-1be06a02502f.jpg" /> if <img src="2-2310080\1bda679b-5e47-4e06-abd3-a02ad3bab24a.jpg" /> is outside of the interval <img src="2-2310080\aea1b679-295c-4db3-8aff-be98355d734c.jpg" /> [19,20]. To satisfy Equation (1) in condition of uncertainty about the forcing we formulate the problem of estimating <img src="2-2310080\760a4793-7a60-4685-ae01-67999d658cdd.jpg" /> as the following two-objective optimization problem</p><disp-formula id="scirp.29371-formula55068"><label>(5)</label><graphic position="anchor" xlink:href="2-2310080\d18f10c2-43dc-4eae-ab02-daed646d2d55.jpg"  xlink:type="simple"/></disp-formula><p>which in the traditional approach does not have a solution in contrast to the conditional optimization discussed above for the case of known forcing.</p><p>A key concept in multi-objective optimization is a Pareto optimal solution, e.g. [<xref ref-type="bibr" rid="scirp.29371-ref21">21</xref>]. In plain words it is one in which any improvement of one objective function can be achieved only at the expense of another. For a formal definition see the cited paper.</p><p>To find the set <img src="2-2310080\0e261d23-2d65-4711-9459-fd3eeca976f4.jpg" /> of all Pareto optimal solutions for (5) introduce <img src="2-2310080\18a67361-3645-453e-9442-ac83b477526d.jpg" /> for the interpolated velocity (3) and assume that <img src="2-2310080\157438a1-59e1-4ca7-9a79-004baebb61c7.jpg" /> is even and strictly increasing on<img src="2-2310080\875a5b2b-8951-4bc3-931c-9a18a38350b7.jpg" />, for example <img src="2-2310080\29c4fefb-1f7c-4a43-885f-2ae1f057c191.jpg" /> is a triangle membership function.</p><p>Direct computations lead to the following parametric description of <img src="2-2310080\11741c80-36ec-4e11-b3d9-9fa8c1a96910.jpg" /></p><disp-formula id="scirp.29371-formula55069"><label>(6)</label><graphic position="anchor" xlink:href="2-2310080\95378c37-846e-464e-b267-2131353af2ea.jpg"  xlink:type="simple"/></disp-formula><p>In other words, <img src="2-2310080\bd9d6e0e-7499-414d-ae6e-bbc7c17e62ac.jpg" />is a segment on the straight line in the plane <img src="2-2310080\d8e83f3f-0620-4ef9-85be-f092c7af5e84.jpg" /> passing through <img src="2-2310080\71926132-4b08-4bcb-b9a7-bfb4101e20c9.jpg" /> perpendicular to the line<img src="2-2310080\7f785d97-7b0f-4d85-af6d-3c67000f6122.jpg" />. One of the endpoints of this segment is always coincides with <img src="2-2310080\3009ff26-ad8e-490a-92c6-604813fc0d01.jpg" /> given by (2) while the another one is either <img src="2-2310080\6310764b-0f4d-47d6-ad2e-c59b6f7f736f.jpg" /> or <img src="2-2310080\2ad8cf26-fb1f-420a-820d-41bab158ca61.jpg" /> depending on whether <img src="2-2310080\45a6ae61-b99e-44b3-aeac-cc08129c6c7e.jpg" /> is greater or less than<img src="2-2310080\e97afa8a-5f82-4bc9-9247-14d1dd984e47.jpg" />.</p><p>In principle, any point from <img src="2-2310080\837f1684-412f-410d-9d00-b90da46cf184.jpg" /> could be treated as a sensible estimator of the true velocity. To single out a certain solution one can simply take the middle point of<img src="2-2310080\533e8b7c-df61-4399-bcf9-141bd3f89e8c.jpg" />, however we suggest another way which is more consistent with fuzzy logic ideas and also allows to find out an explicit expression for the estimator. Namely, we change the set up (5) by replacing the quadratic cost function <img src="2-2310080\378b7f22-91bd-49d0-992b-4cb0d4d7a857.jpg" /> by an appropriate membership function <img src="2-2310080\94240e1c-f5f4-42b7-bab8-977c8d23115f.jpg" /> centered at <img src="2-2310080\b232fbe6-28a1-4dcf-ab79-1c569885f769.jpg" /> and then proceed to another fuzzy two-objective optimization problem</p><disp-formula id="scirp.29371-formula55070"><label>(7)</label><graphic position="anchor" xlink:href="2-2310080\2811a6b3-6f9b-4ba8-924a-c093d2e6e9d8.jpg"  xlink:type="simple"/></disp-formula><p>In simple words we try to make the solution as close as possible to the interpolated velocity at the same time maximizing the possibility that just this solution advects the tracer.</p><p>The Pareto optimal set for (7) also can be efficiently described similarly to (6) and then the unique solution can be singled out by taking its center of mass</p><disp-formula id="scirp.29371-formula55071"><label>(8)</label><graphic position="anchor" xlink:href="2-2310080\8fba2f61-46ff-4d3b-93b0-2d11b16a3949.jpg"  xlink:type="simple"/></disp-formula><p>according to fuzzy logic standard rules in aggregating information coming from different sources [19,20].</p><p>Let us parameterize <img src="2-2310080\4a6cde14-dfce-45f8-a984-c36c23a20dc1.jpg" /> as a circular cone inside the circle <img src="2-2310080\72bb0bbd-8f2b-4589-a868-048aadc3ec4b.jpg" /> and zero otherwise where <img src="2-2310080\e24f1828-4227-4ec4-9a41-dc8c40e7d932.jpg" /> is a parameter characterizing uncertainties in the velocity observations. Then take <img src="2-2310080\6f0bfdee-7d6a-46bb-a3b8-573cf676f52f.jpg" /> as a triangle membership function defined by triplet<img src="2-2310080\f029451b-df7f-456b-a716-b7a25b3b69d7.jpg" />. As a result (8) van be readily found in explicit form. Namely, denote</p><p><img src="2-2310080\d32d75b2-1a2a-4c11-9573-8c2dafc92d84.jpg" /></p><p>then (6) is expressible in form</p><disp-formula id="scirp.29371-formula55072"><label>(9)</label><graphic position="anchor" xlink:href="2-2310080\5e4ff092-6da8-47ec-a87c-b956c8fe874b.jpg"  xlink:type="simple"/></disp-formula><p>where for <img src="2-2310080\8732b6d2-86db-4638-a080-2a7f6883ed3d.jpg" /></p><p><img src="2-2310080\a1de63fa-c3cd-42a3-8bec-e21262a1393b.jpg" /></p><p>and for <img src="2-2310080\486ff764-5535-46a3-a896-a894c2f3b767.jpg" /></p><p><img src="2-2310080\a8722409-82cf-4826-aed2-e299f5eba92e.jpg" /></p><p>with</p><p><img src="2-2310080\6f0d41ec-c181-4be1-8e6c-3071c0c595ff.jpg" /></p></sec><sec id="s4"><title>4. Simulations</title><sec id="s4_1"><title>4.1. Gyre Superimposed with Eddy System</title><p>In the first series of experiments the “true” velocity field is given by the following stream function</p><p><img src="2-2310080\f52aab38-9989-4c59-975c-34ce52490ebe.jpg" /></p><p>where</p><p><img src="2-2310080\0228ec7b-523f-417c-9737-fc8620d0b1e7.jpg" /></p><p>is the gyre with space scale <img src="2-2310080\040278b2-1469-4b7d-82f7-ba4525046c18.jpg" /> and the disturbing velocity is expressed by an oscillating regular system of eddies filling up the region</p><p><img src="2-2310080\8f273688-03de-4110-bdf9-5a36fc856608.jpg" /></p><p>where <img src="2-2310080\7c762066-616a-4803-8cdc-b4c0f6500065.jpg" /> is the amplitude and <img src="2-2310080\c2bf7a8c-828e-42a2-83c5-c654422909d6.jpg" /> is the fixed observation time. Finally, suppose that the initial tracer distribution is given by a Gaussian bell</p><p><img src="2-2310080\90a80b1e-8210-446c-ae7c-871429082892.jpg" /></p><p>where R is the patch radius and <img src="2-2310080\3e2ab38c-33d5-4601-bb9d-f8c36c70434b.jpg" /> is its center.</p><p>In all below experiments the region <img src="2-2310080\8eedda2d-bdd7-41a8-be66-0a411bdbf74e.jpg" /> remains the same with<img src="2-2310080\c11ac3a1-48d6-45ef-b608-23ca69b4997c.jpg" />. The fine grid <img src="2-2310080\1fdcce7e-cb11-4892-a8c8-1b62ff1575ee.jpg" /> defined as the set of all integer pairs <img src="2-2310080\7ffddc23-c2a9-433d-b6ad-b6ea5084ee07.jpg" /> is also kept constant (thus<img src="2-2310080\9d04d753-92b9-41a4-8181-6217216e4faf.jpg" />), while the step of the coarse grid is defined by <img src="2-2310080\fe1dcc34-12b3-47b6-aa03-9623361c3920.jpg" /> where <img src="2-2310080\c83851fb-bb4e-43e5-b634-9db35a781ef1.jpg" /> is the coarseness parameter which assumes three possible values<img src="2-2310080\94f63166-0529-411f-a20a-268ea1cf53f3.jpg" />.</p><sec id="s4_1_1"><title>4.1.1. Known Forcing</title><p>In the first experiment we assumed zero forcing for the tracer,<img src="2-2310080\6bc52363-b4c0-446d-9686-5d27e4600fd4.jpg" />. The estimates (2) were computed for each time moment <img src="2-2310080\94fc4589-8c43-4fd3-905f-5eeebc603008.jpg" /> with <img src="2-2310080\154d3dd3-cb2d-41eb-be3f-641ac6349d09.jpg" /> and then compared to the pure interpolation.</p><p>Weights <img src="2-2310080\a84e3354-07f2-4641-a50f-71600869bdae.jpg" /> in the interpolation objective function were chosen to be inversely proportional to the squared distances <img src="2-2310080\9d6607de-9968-4511-8128-225873e6f503.jpg" /> where x is the point in which the velocity is estimated and <img src="2-2310080\aa7973ae-3cf5-4b7c-8c97-dac7f068ea5b.jpg" /> are vertices of the square in <img src="2-2310080\06e3d8a7-bcde-47f1-b6b5-5629cf6495ae.jpg" /> where <img src="2-2310080\ed3529db-2290-4929-a8fc-9082383b5ef5.jpg" /> lies.</p><p>An example is shown in <xref ref-type="fig" rid="fig1">Figure 1</xref> for the terminal time moment <img src="2-2310080\b4f6cdde-e768-4f1a-8d2e-5548859a4a47.jpg" /> under the following values of other parameters R = 10, R<sub>b</sub> = 10, x<sub>0</sub> = 3, y<sub>0</sub> = 3, a = 5, k = 3, c = 8. As one can see, the estimated velocity field (first panel at the bottom) fairly captures principal features of the real velocity even for extremely high coarseness. In terms of numbers the relative estimation error <img src="2-2310080\0bcfc71a-d13c-499c-b64b-d8555ed2991e.jpg" /> is significantly less than the interpolation error <img src="2-2310080\97a2f97e-5e44-441a-94f7-660b995788bc.jpg" /> such that <img src="2-2310080\00741088-5b3d-4234-8cee-d06ee60d19da.jpg" /> which is well agreed with the theoretical bound (4).</p><p>We also show the gyre itself (last panel at the bottom) to illustrate that the interpolation itself captures well the large scale part of the circulation.</p><p>Results for other experiments are summarized in the following table.</p><p>From <xref ref-type="table" rid="table1">Table 1</xref> the following conclusions can be drawn</p><p>-&#160;&#160;&#160;&#160;&#160;&#160; In all the instances the estimation error is less than the interpolation error.</p><p>-&#160;&#160;&#160;&#160;&#160;&#160; The estimation error is most sensitive to the coarseness parameter <img src="2-2310080\12d55b88-d8a6-4aa0-9b93-ee1404d4c7ac.jpg" /> characterizing sparseness of the velocity observations.</p><p>-&#160;&#160;&#160;&#160;&#160;&#160; The least influential parameter is the patch radius.</p><p>-&#160;&#160;&#160;&#160;&#160;&#160; The estimation error decreases as eddy density <img src="2-2310080\2c54d814-8759-4d99-ad07-583518c21870.jpg" /> decreases.</p><p>-&#160;&#160;&#160;&#160;&#160;&#160; As amplitude <img src="2-2310080\f80b19bc-f858-4629-a641-6dea61868c6e.jpg" /> kept constant, the range of improvement <img src="2-2310080\ae06b08c-f356-4783-be0f-4845b1aaec4e.jpg" /> is <img src="2-2310080\e865fb7d-65c4-4077-8da4-042465d17f3a.jpg" /> with the minimum value at <img src="2-2310080\dc6c4b9c-1a72-4561-a819-413f3d39040c.jpg" /> and maximum value at<img src="2-2310080\130abf4c-e850-41e0-bbfb-b01b5b4762fd.jpg" />.</p><p>The goal of next two experiments whose results are presented in Tables 2 and 3 was to examine high and low amplitudes<img src="2-2310080\9bff9a8a-7fb1-40f4-ba4f-f5933f3d8804.jpg" />.</p><p>As one can see from <xref ref-type="table" rid="table2">Table 2</xref> a sharp rise in the eddy amplitudes (ten times) modestly increases the estimation error, while when we go back to very small amplitude <img src="2-2310080\e5919cde-c4c3-4871-96a2-37809b4999b3.jpg" /> the error decays by 2 - 3 times depending on the coarseness (<xref ref-type="table" rid="table3">Table 3</xref>).</p></sec><sec id="s4_1_2"><title>4.1.2. Unknown Forcing</title><p>In the second series of experiments we tested the same model and “real” velocities with the “unknown” tracer forcing</p><disp-formula id="scirp.29371-formula55073"><label>(10)</label><graphic position="anchor" xlink:href="2-2310080\ef31e839-535e-402b-9ec7-15c6e55d625b.jpg"  xlink:type="simple"/></disp-formula><p>Real velocity fieid, k = 3, a = 5, c = 8&#160;&#160;&#160;&#160;&#160;&#160; Observed veiocity field, k = 3, a = 5, c = 8&#160;&#160; &#160;Tracer distribution under real velocity in 3 days</p><p><img src="2-2310080\11f2b1a2-bd2e-4998-bece-1cd67a439ee6.jpg" /></p><p>Esimated velocity field, k = 3, a = 5, c = 8&#160;&#160; &#160;&#160;&#160;&#160;&#160;Optimal Interpolation, k = 3, a = 5, c = 8&#160; &#160;&#160;Large scale velocity field, k = 3, a = 5, c = 8</p><p><xref ref-type="table" rid="table1">Table 1</xref>. Dependence of the estimation and interpolation error on the eddy density (k), observation coarseness (c) and the patch radius (R) for the fixed amplitude a = 5.</p><p><img src="2-2310080\5c038dd6-b890-4c8f-a016-044903b27c13.jpg" /></p><p><xref ref-type="table" rid="table2">Table 2</xref>. Dependence of the estimation and interpolation error on the observation coarseness (c) and the patch radius (R) for the fixed amplitude a = 50 and eddy density k = 3.</p><p><img src="2-2310080\be433e5f-e873-4693-a923-ba51e1ca8bc4.jpg" /></p><p><xref ref-type="table" rid="table3">Table 3</xref>. Dependence of the estimation and interpolation error on the observation coarseness (c) and the patch radius (R) for the fixed amplitude a = 1 and eddy density k = 3.</p><p><img src="2-2310080\f09a6334-d797-4fba-8192-0b0c9a0bc525.jpg" /></p><p>where <img src="2-2310080\bf63100d-8579-406d-bb2d-f5a69c2ed6db.jpg" /> is a given amplitude. The experiment conditions were the same as in the previous subsection except that the transport Equation (1) was integrated to generate tracer observations with the forcing given in (10) and the velocity estimates were obtained from the more general Equation (9) instead of (2). We underscore that in estimating the velocity field by (9) expression (10) for the forcing was not used at all. The only information on the forcing used for estimating was <img src="2-2310080\5007af3a-b223-4c6b-8bfa-b44bd55f6c4a.jpg" /> and<img src="2-2310080\d0da1e8b-51a9-4078-8c66-c6be5647b201.jpg" />.</p><p>The goal of experiments with fuzzy estimator (9) was to compare it with the estimator (2) which simply ignores the forcing uncertainty. We carried out such a comparison for two values of the parameter <img src="2-2310080\17383086-7757-424b-a29f-dc5964ba4e0d.jpg" /> characterizing the forcing intensity. The results are summed up in Tables 4 and 5. The relative error of the fuzzy estimator <img src="2-2310080\63313c19-3bdb-4ec7-9f7c-15d01de3b548.jpg" /> is defined similarly to<img src="2-2310080\2b1377e6-0918-4279-aab2-d6b0c362699e.jpg" />.</p><p>The main conclusions concerning an unknown forcing are as follows:</p><p>-&#160;&#160;&#160;&#160;&#160;&#160; In most of scenarios the fuzzy estimator overperforms the non-fuzzy one.</p><p>-&#160;&#160;&#160;&#160;&#160;&#160; Under high amplitude of an unknown forcing and low coarseness the simple interpolation can perform better than either of the estimators.</p></sec></sec><sec id="s4_2"><title>4.2. Coastal Flow</title><p>The goal of the last experiment Which is prensented in <xref ref-type="fig" rid="fig2">Figure 2</xref> was to examine the method performance in detecting a single vortex (eddy) surrounded by a steady coastal current. The “true” velocity field is shown in the first panel at the upper row. On the next panel sparse direct velocity measurements are presented, which certainly do not allow to capture the eddy because of too low resolution. Finally, in the third panel we give tracer observations which exposing the eddy, but not sufficient to recover the whole flow.</p><p>The estimate according to the developed fuzzy algorithm is shown in the first panel of the lower row. One can see that the procedure was able to efficiently combine both kinds of the observations thereby adequately to retrieve both the eddy and background current. We compare the result with a pure interpolation (second panel) where the eddy turned out to be almost invisible. The only positive outcome of the interpolation is a fair estimate of the background flow (last panel).</p><p>In terms of numbers the improvement of the fuzzy estimate comparing to interpolation is only about<img src="2-2310080\e87d4ecc-826b-49af-bf17-0774278dbe7f.jpg" />, but in fact qualitatively the results are quite different.</p></sec></sec><sec id="s5"><title>5. Conclusions</title><p>A method is developed for estimating surface velocities on a fine grid by combining two kinds of observations:</p><p>True&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160; Observed velocity field&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160; Tracer</p><p><img src="2-2310080\06582062-939a-4994-adc2-993065453f0d.jpg" /></p><p>Estimated velocity field&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160; Optimal Interpolation&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160; Background</p><p><xref ref-type="table" rid="table4">Table 4</xref>. Comparison between the fuzzy estimator (δ<sub>f</sub>), non-fuzzy (δ<sub>e</sub>, Section 2), and interpolation (δ<sub>i</sub>) for h = 5.</p><p><img src="2-2310080\d5518383-173d-4a17-8918-20e4f6959564.jpg" /></p><p><xref ref-type="table" rid="table5">Table 5</xref>. Comparison between the fuzzy estimator (δ<sub>f</sub>), non-fuzzy (δ<sub>e</sub>, Section 2), and interpolation (δ<sub>i</sub>) for h = 10.</p><p><img src="2-2310080\6ce83438-cef9-417c-8206-2a04aaa698c2.jpg" /></p><p>velocity itself on a coarse grid and tracer on a fine grid.</p><p>The first version of the method is aimed at the known forcing in the transport equation. The corresponding estimator is nothing more but the solution of a classical conditional optimization problem with a traditional quadratic cost function. Numerical experiments were conducted with a gyre superimposed by a vortex system to investigate the method performance depending on the coarseness of velocity measurements, the number of eddies, and the gyre radius. Improvement in the estimate comparing to the pure interpolation was around 25% - 40% depending on the above parameters.</p><p>In the second version of the method designed for a poorly known forcing we model uncertainties in the forcing and velocity measurements using a fuzzy set approach. Arising a simple two-objective fuzzy optimization problem allows an explicit solution. With poorly known forcing an improvement in estimation comparing to interpolation is more modest. Moreover, for low coarseness interpolation can work even slightly better under large unknown forcing. As for comparing the fuzzy and non-fuzzy algorithm (which does not account for uncertainties in the forcing at all) the former is better in all the scenarii, even though the difference in estimation error is not much significant.</p><p>On the qualitative level the method overperforms interpolation as well for a typical coastal flow with an isolated eddy.</p></sec><sec id="s6"><title>6. Acknowledgements</title><p>The support of the Office of Naval Research under grant N00014-11-1-0369 and NSF under grant CMG-0530893 is greatly appreciated.</p></sec><sec id="s7"><title>REFERENCES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.29371-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">C. Wunsch, “The North Atlantic General Circulation West of 50W Determined by Inverse Methods,” Reviews of Geophysics, Vol. 16, No. 4, 1978, pp. 583-620.  
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