<?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">JAMP</journal-id><journal-title-group><journal-title>Journal of Applied Mathematics and Physics</journal-title></journal-title-group><issn pub-type="epub">2327-4352</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/jamp.2015.32026</article-id><article-id pub-id-type="publisher-id">JAMP-53669</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Radar Cross Section Analysis Using Physical Optics and Its Applications to Marine Targets
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Joon-Tae</surname><given-names>Hwang</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>Suk-Yoon</surname><given-names>Hong</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>Jee-Hun</surname><given-names>Song</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Hyun-Wung</surname><given-names>Kwon</given-names></name><xref ref-type="aff" rid="aff3"><sup>3</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Department of Naval Architecture and Ocean Engineering, Seoul National University, Seoul, Republic of Korea</addr-line></aff><aff id="aff2"><addr-line>Department of Naval Architecture and Ocean Engineering, Chonnam National University, Yeosu, Republic of Korea</addr-line></aff><aff id="aff3"><addr-line>Department of Naval Architecture and Ocean Engineering, Kojecollege, Koje, Republic of Korea</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>jth00@snu.ac.kr(JH)</email>;<email>syh@snu.ac.kr(SH)</email>;<email>jhs@jnu.ac.kr(JS)</email>;<email>khw1@snu.ac.kr(HK)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>30</day><month>01</month><year>2015</year></pub-date><volume>03</volume><issue>02</issue><fpage>166</fpage><lpage>171</lpage><history><date date-type="received"><day>19</day>	<month>November</month>	<year>2014</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>
 
 
   Radar Cross Section (RCS) is one of the most considerable parameters for ship stealth design. As modern ships are larger than their predecessors, RCS must be managed at each design stage for its reduction. For predicting RCS of ship, Radar Cross Section Analysis Program (RACSAN) based on Kirchhoff approximation in high frequency range has been developed. This program can present RCS including multi-bounce effect in exterior and interior structure by combination of geometric optics (GO) and physical optics (PO) methods, coating effect by using Fresnel reflection coefficient, and response time pattern for detected target. In this paper, RCS calculations of ship model with above effects are simulated by using this developed program and RCS results are discussed.  
 
</p></abstract><kwd-group><kwd>Radar Cross Section (RCS)</kwd><kwd> Kirchhoff Approximation</kwd><kwd> Multi-Bounce Effect</kwd><kwd> Response Time Pattern</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The Radar Cross Section (RCS) is concerned with active detection and is an important parameter in stealth design. RCS characteristics are determined by the intrinsic geometric shape. Because modern ships are larger than their predecessors, RCS must be controlled at each design stage for its reduction.</p><p>The RCS of simple shaped objects such as a finite plate, a cylinder, and a sphere etc. is represented analytically in [<xref ref-type="bibr" rid="scirp.53669-ref1">1</xref>]. For more complex shaped targets, numerical calculations were needed. The boundary element method (BEM) [<xref ref-type="bibr" rid="scirp.53669-ref2">2</xref>] and finite element method (FEM) [<xref ref-type="bibr" rid="scirp.53669-ref3">3</xref>] were used at low frequency. These methods give accurate results but require a long computer running time. At high frequency, methods such as physical optics (PO) [<xref ref-type="bibr" rid="scirp.53669-ref4">4</xref>], geometric optics (GO) [<xref ref-type="bibr" rid="scirp.53669-ref5">5</xref>], physical theory of diffraction [<xref ref-type="bibr" rid="scirp.53669-ref6">6</xref>] and geometric theory of diffraction [<xref ref-type="bibr" rid="scirp.53669-ref7">7</xref>] provide relatively quick solutions. At present, most numerical calculations of RCS for a target such as a ship at high frequency are based on Kirchhoff approximation [<xref ref-type="bibr" rid="scirp.53669-ref8">8</xref>]. For prediction for RCS of a ship in high frequency range, Radar Cross Section Analysis Program (RACSAN) based on Kirchhoff approximation in PO has been developed.</p><p>In this paper, RCS for a ship model is numerically simulated by using this program. Various effects, which are multi-bounce effect in exterior and interior structure by combination of GO and PO methods, coating effect by using Fresnel reflection coefficient, and response time pattern for detected target are considered.</p></sec><sec id="s2"><title>2. Theory</title><sec id="s2_1"><title>2.1. Physical Optics</title><p>The high frequency prediction method assumes that each part of the target scatters energy independently from all other parts, the total energy scattered in the far field is obtained by integrating energy scattered by each part. Therefore, the total RCS of a complex target can be composed of a number of segments, and can be obtained by the summation of the RCS of each segment. The root of the total RCS is estimated by the coherent summation of the RCS of each segment to consider phase information as follows:</p><disp-formula id="scirp.53669-formula462"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53669x4.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x5.png" xlink:type="simple"/></inline-formula> is the root of the total RCS, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x6.png" xlink:type="simple"/></inline-formula>is the number of the segment and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x7.png" xlink:type="simple"/></inline-formula> is the root of the RCS</p><p>of each segment. The root of the RCS for a polygonal plate can be expressed by the so-called Kirchhoff approximation as follows [<xref ref-type="bibr" rid="scirp.53669-ref9">9</xref>] [<xref ref-type="bibr" rid="scirp.53669-ref10">10</xref>],</p><disp-formula id="scirp.53669-formula463"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53669x8.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x9.png" xlink:type="simple"/></inline-formula> is the wave number, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x10.png" xlink:type="simple"/></inline-formula>is the polarization vector, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x11.png" xlink:type="simple"/></inline-formula>is the position vector of an origin on or near the plate, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x12.png" xlink:type="simple"/></inline-formula>is<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x13.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x14.png" xlink:type="simple"/></inline-formula>is a unit vector along the incident wave, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x15.png" xlink:type="simple"/></inline-formula>is a unit vector along the reflected wave, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x16.png" xlink:type="simple"/></inline-formula>is a vector describing the length and orientation of the mth edge of the plate, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x17.png" xlink:type="simple"/></inline-formula>is the position vector of the midpoint of the th edge, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x18.png" xlink:type="simple"/></inline-formula>is the length of the projection of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x19.png" xlink:type="simple"/></inline-formula> onto the plane of the plate, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x20.png" xlink:type="simple"/></inline-formula></p><p>is<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x21.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x22.png" xlink:type="simple"/></inline-formula>is the unit normal of the illuminated plate surface, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x23.png" xlink:type="simple"/></inline-formula>is the number of plate edges, and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x24.png" xlink:type="simple"/></inline-formula> is<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x25.png" xlink:type="simple"/></inline-formula>.</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x26.png" xlink:type="simple"/></inline-formula>can be expressed as follows [<xref ref-type="bibr" rid="scirp.53669-ref11">11</xref>]:</p><disp-formula id="scirp.53669-formula464"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53669x27.png"  xlink:type="simple"/></disp-formula></sec><sec id="s2_2"><title>2.2. Effect on the Surface Property</title><p>Referring to <xref ref-type="fig" rid="fig1">Figure 1</xref>. Consider the PO solution for a multilayered facet. The interaction of an incident electromagnetic field with a non-perfectly conducting multilayered facet can be described by Fresnel’s reflection coef-</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Geometry of multilayered facet</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x28.png"/></fig><p>ficients <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x29.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x30.png" xlink:type="simple"/></inline-formula> at the surface of the facet. If the complex material constants of the different layers are known, the reflection coefficient at the surface of the facet is given by [<xref ref-type="bibr" rid="scirp.53669-ref12">12</xref>]</p><disp-formula id="scirp.53669-formula465"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53669x31.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.53669-formula466"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53669x32.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x33.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x34.png" xlink:type="simple"/></inline-formula> satisfy the following recurrence relations</p><disp-formula id="scirp.53669-formula467"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53669x35.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.53669-formula468"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53669x36.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x37.png" xlink:type="simple"/></inline-formula>, and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x37.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x38.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x37.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x38.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x39.png" xlink:type="simple"/></inline-formula> are input impedances of the nth layer for H-polarization and E-pola-</p><p>rization, respectively. The Nth layer is assumed to be semi-infinite long, and the input impedances of the Nth layer is given by</p><disp-formula id="scirp.53669-formula469"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53669x40.png"  xlink:type="simple"/></disp-formula><p>The impedance of the nth layer is</p><disp-formula id="scirp.53669-formula470"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53669x41.png"  xlink:type="simple"/></disp-formula></sec><sec id="s2_3"><title>2.3. Multi-Bounce Effect in Exterior and Interior Structure</title><p>For considering multi-bounce effect in exterior and interior structure, combination of GO and PO methods is used [<xref ref-type="bibr" rid="scirp.53669-ref9">9</xref>]. GO is used for finding reflected or transmitted paths. PO is applied at last bounce time. Effect area is obtained as shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>. A path of transmitted wave into interior structure is calculated by using Snell’s law.</p></sec></sec><sec id="s3"><title>3. Numerical RCS Analysis</title><p>RCS computation is performed for a type of warship. Model which has a curvature is divided into many flat plates. RCS of each flat plate is evaluated using Equation (2).</p>A Type of Warship<p>A warship model for RCS calculation is shown in <xref ref-type="fig" rid="fig3">Figure 3</xref>. The overall length, width and draft of the warship are 000 m, 00 m and 0 m, respectively which are blind in the security classification. The mesh model is composed of 4675 nodes and 4065 elements as shown <xref ref-type="fig" rid="fig3">Figure 3</xref>.</p><fig-group id="fig2"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Concept of multi-bounce: (a) multi-bounce paths and (b) effective area.</title></caption><fig id ="fig2_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x42.png"/></fig><fig id ="fig2_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x43.png"/></fig></fig-group><p>The range of the incident angle is <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x44.png" xlink:type="simple"/></inline-formula> as shown in <xref ref-type="fig" rid="fig3">Figure 3</xref>. When the interval of the incident angle is<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x44.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x45.png" xlink:type="simple"/></inline-formula>. The distance from the center of the model is 20 km for the far field condition. The analysis frequency is 4 Ghz and the wave velocity is<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x44.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x45.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x46.png" xlink:type="simple"/></inline-formula>.</p><p>At first, the RCS results of the contribution of the incident angle are shown in <xref ref-type="fig" rid="fig4">Figure 4</xref>.</p><p>The RCS results of the warship model with the elevation angle are shown in <xref ref-type="fig" rid="fig5">Figure 5</xref>.</p><p>The RCS of the warship model with electronic coating on its surfaces is then analyzed. Electronic coating is applied as shown in <xref ref-type="fig" rid="fig6">Figure 6</xref>.</p><p>The RCS results with electronic coatings are shown in <xref ref-type="fig" rid="fig7">Figure 7</xref>.</p><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Analysis model and range</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x47.png"/></fig><fig-group id="fig4"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> The RCS results of the contribution of the incident angle.</title></caption><fig id ="fig4_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x48.png"/></fig><fig id ="fig4_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x49.png"/></fig></fig-group><fig-group id="fig5"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> RCS results with the elevation angle: (a)<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x56.png" xlink:type="simple"/></inline-formula>: 13.46 dB; (b)<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x56.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x57.png" xlink:type="simple"/></inline-formula>: 15.71 dB; (c)<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x56.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x57.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x58.png" xlink:type="simple"/></inline-formula>: 19.50 dB; (d)<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x56.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x57.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x58.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x59.png" xlink:type="simple"/></inline-formula>: 21.23 dB; (e)<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x56.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x57.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x58.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x59.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x60.png" xlink:type="simple"/></inline-formula>: 34.06 dB; (f)<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x56.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x57.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x58.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x59.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x60.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53669x61.png" xlink:type="simple"/></inline-formula>: 37.37 dB.</title></caption><fig id ="fig5_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x50.png"/></fig><fig id ="fig5_2"><label> (c)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x51.png"/></fig><fig id ="fig5_3"><label>(d)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x52.png"/></fig><fig id ="fig5_4"><label> (e)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x53.png"/></fig><fig id ="fig5_5"><label> (f)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x54.png"/></fig><fig id ="fig5_6"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x55.png"/></fig></fig-group><fig-group id="fig6"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Electronic coating applied on a warship surface: (a) case 1; (b) case 2.</title></caption><fig id ="fig6_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x62.png"/></fig><fig id ="fig6_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x63.png"/></fig></fig-group><fig-group id="fig7"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> RCS results with electronic coating applied: (a) case 1; (b) case 2.</title></caption><fig id ="fig7_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x64.png"/></fig><fig id ="fig7_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53669x65.png"/></fig></fig-group></sec><sec id="s4"><title>4. Conclusion</title><p>To predict RCS of ship at design stage, RACSAN software is developed. This program is based on Kirchhoff approximation in PO as high frequency method. The RCS of ship model is numerically simulated by using this program. Various effects, which are multi-bounce effect in exterior and interior structure by combination of GO and PO methods, electronic coating effect by using reflection coefficient, and response time pattern for detected target are considered. It is expected that RCS of ship can be continuously managed by simulation when ship shape is changed at design stage and controlled by predicting electronic coating effects applied on specific parts by using this program.</p></sec><sec id="s5"><title>Cite this paper</title><p>Joon-Tae Hwang,Suk-Yoon Hong,Jee-Hun Song,Hyun-Wung Kwon, (2015) Radar Cross Section Analysis Using Physical Optics and Its Applications to Marine Targets. Journal of Applied Mathematics and Physics,03,166-171. doi: 10.4236/jamp.2015.32026</p></sec><sec id="s6"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.53669-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Urick, R.J. (1983) Principles of Underwater Sound. 3rd Edition, McGraw-Hill, New York.</mixed-citation></ref><ref id="scirp.53669-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Okumura, T., Masuya, T., Takao, Y. and Sawada, K. (2003) Acoustic Scattering by an Arbitrarily Shaped Body: An Application of the Boundary-Element Method. ICES Journal of Marine Science, 60, 563-570. 
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