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  <titleInfo>
    <title>FPGA based adaptive PD fuzzy controller for flying robot</title>
  </titleInfo>
  <name type="personal">
    <namePart>Chaiyong Lamprom</namePart>
    <role>
      <roleTerm authority="marcrelator" type="text">creator</roleTerm>
    </role>
  </name>
  <name type="personal">
    <namePart>Lertsak Lekawat</namePart>
    <role>
      <roleTerm type="text">Chairperson</roleTerm>
    </role>
  </name>
  <name type="personal">
    <namePart>Manukid Parnichkun</namePart>
    <role>
      <roleTerm type="text">Examination Committee</roleTerm>
    </role>
  </name>
  <name type="personal">
    <namePart>Chumnarn Punyasai</namePart>
    <role>
      <roleTerm type="text">Examination committee</roleTerm>
    </role>
  </name>
  <name type="corporate">
    <namePart>Thailand Graduate of Science and Technology(TGIST)</namePart>
    <role>
      <roleTerm type="text">Scholarship Donor</roleTerm>
    </role>
  </name>
  <name type="corporate">
    <namePart>National Science and Technology; Development Agency (NSTDA)</namePart>
    <role>
      <roleTerm type="text">Scholarship Donor</roleTerm>
    </role>
  </name>
  <typeOfResource>text</typeOfResource>
  <genre authority="marc">series</genre>
  <genre authority="marc">technical report</genre>
  <originInfo>
    <place>
      <placeTerm type="code" authority="marccountry">th</placeTerm>
    </place>
    <place>
      <placeTerm type="text">Bangkok</placeTerm>
    </place>
    <publisher>Asian Institute of Technology</publisher>
    <dateIssued>2002</dateIssued>
    <issuance>continuing</issuance>
  </originInfo>
  <language>
    <languageTerm authority="iso639-2b" type="code">eng</languageTerm>
  </language>
  <physicalDescription>
    <extent>115 p.</extent>
  </physicalDescription>
  <abstract>The paper illustrated Field Programmable Gate Arrays ( FPGA) based adaptive proportional Derivative controller for a flying robot. The Kalt 30 Baron nonlinear Helicopter model is used as a mobile platform in which Xilinx xc4062xla will be used as a controller system. A digital compass tcm2-50 was used to measure the heading direction. This thesis study presents the adaptive fuzzy TSK controller by control output error method ( COEM ) and its implementation to hardware controller. The system is partially autonomous because only a heading direction is designed . The lateral and floating height of the flying robot is manually by cyclic controlled by a human pilot . However it is only an approach of control scheme that it needs to be redesign for pitch, roll and floating height.</abstract>
  <note>thesis submitted in partial fulfillment of the requirements for the degree of Master of Engineering, School of Advanced Technologies</note>
  <note>Thesis (M.Eng.) - Asian Institute of Technology, 2002</note>
  <subject authority="lcsh">
    <topic>Field programmable gate arrays</topic>
  </subject>
  <subject authority="lcsh">
    <topic>Robots</topic>
    <topic>Control systems</topic>
  </subject>
  <subject authority="lcsh">
    <topic>Fuzzy systems</topic>
  </subject>
  <relatedItem type="series">
    <titleInfo>
      <title>Thesis ; no. ME-02-05</title>
    </titleInfo>
    <name type="corporate">
      <namePart>Asian Institute of Technology.</namePart>
      <namePart/>
    </name>
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  <identifier type="uri">http://203.159.5.9/ait-thesis/detail.php?q=B07339</identifier>
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    <url displayLabel="Full-Text">http://203.159.5.9/ait-thesis/detail.php?q=B07339</url>
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    <recordCreationDate encoding="marc">030829</recordCreationDate>
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