<?xml version="1.0" encoding="UTF-8"?>
<!DOCTYPE article
  PUBLIC "-//NLM//DTD Journal Publishing DTD v2.0 20040830//EN" "http://dtd.nlm.nih.gov/publishing/2.0/journalpublishing.dtd">
<article xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:mml="http://www.w3.org/1998/Math/MathML" article-type="research-article" dtd-version="2.0" xml:lang="EN">

  <front>

    <journal-meta>

      <journal-title>Information Technology Journal</journal-title>

      <issn pub-type="ppub">1812-5638</issn>

      <issn pub-type="epub">1812-5646</issn>

      <publisher>

        <publisher-name>Asian Network for Scientific Information</publisher-name>

      </publisher>

    </journal-meta>


    <article-meta>

      <article-id pub-id-type="doi">10.3923/itj.2012.563.565</article-id>


      <title-group>

        <article-title><![CDATA[The Design for Airborne Electronic Equipment Fault Diagnostic System Base on IPC]]></article-title>

      </title-group>


      <contrib-group>

        <contrib contrib-type="author" xlink:type="simple">


          <name name-style="western">

            <surname>Weng</surname>

            <given-names>Cheng</given-names>

          </name>


        </contrib>

      </contrib-group>


      <pub-date pub-type="collection">


        <month>4</month>




        <year>2012</year>

      </pub-date>


      <volume>11</volume>

      <issue>4</issue>


      <abstract><![CDATA[<p>With the rapid development of science and technology, modern aviation equipment increases its functionality, while, its structure becomes more and more complex, the speed and reliability requirements are increasing also. The study introduces the design for airborne electronic equipment fault diagnostic system based on IPC, containing the design about the hardware and software, as well as function and task.</p>]]></abstract>


    </article-meta>

  </front>


  <ref-list>




      <ref id="854904">

        <label>1</label>

        <citation citation-type="journal" xlink:type="simple">

          <person-group person-group-type="author">

            <name name-style="western">

              <surname>Lord, D.H. and D. Gleason,</surname>

              <given-names></given-names>

            </name>

          </person-group>

          <year>1981</year>

          <article-title><![CDATA[Design and evaluation methodology for built-in test.]]></article-title>

          <source>IEEE Trans. Reliab.,</source>

          <volume>30</volume>

          <fpage>222</fpage>

          <lpage>226</lpage>

        </citation>

      </ref>


















      <ref id="854910">

        <label>2</label>

        <citation citation-type="journal" xlink:type="simple">

          <person-group person-group-type="author">

            <name name-style="western">

              <surname>Shao, J.J. and L.R. Lamberson,</surname>

              <given-names></given-names>

            </name>

          </person-group>

          <year>1988</year>

          <article-title><![CDATA[Impact of BIT design parameterson systems RAM.]]></article-title>

          <source>Reliab. Eng. Syst. Saf.,</source>

          <volume>23</volume>

          <fpage>219</fpage>

          <lpage>246</lpage>

        </citation>

      </ref>


















      <ref id="854917">

        <label>3</label>

        <citation citation-type="journal" xlink:type="simple">

          <person-group person-group-type="author">

            <name name-style="western">

              <surname>Chen, P. and H.C. Xu,</surname>

              <given-names></given-names>

            </name>

          </person-group>

          <year>2002</year>

          <article-title><![CDATA[Avionics BIT review.]]></article-title>

          <source>China Shipping,</source>

          <volume>6</volume>

          <fpage>108</fpage>

          <lpage>110</lpage>

        </citation>

      </ref>
















  </ref-list>

</article>

