<?xml version="1.0" encoding="ISO-8859-1"?><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance">
<front>
<journal-meta>
<journal-id>2007-9753</journal-id>
<journal-title><![CDATA[RIIIT. Revista internacional de investigación e innovación tecnológica]]></journal-title>
<abbrev-journal-title><![CDATA[RIIIT. Rev. int. investig. innov. tecnol.]]></abbrev-journal-title>
<issn>2007-9753</issn>
<publisher>
<publisher-name><![CDATA[Universidad Autónoma de Coahuila]]></publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id>S2007-97532025000200001</article-id>
<title-group>
<article-title xml:lang="es"><![CDATA[Plataforma de emulación de nanosatélites basada en un cojinete neumático]]></article-title>
<article-title xml:lang="en"><![CDATA[Nanosatellite emulation platform based on an air bearing]]></article-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Tabares-Hernández]]></surname>
<given-names><![CDATA[J.F.]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[García-Mejía]]></surname>
<given-names><![CDATA[J.F.]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Granda-Gutiérrez]]></surname>
<given-names><![CDATA[E.E.]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Reyes-Morales]]></surname>
<given-names><![CDATA[R.]]></given-names>
</name>
<xref ref-type="aff" rid="Aff"/>
</contrib>
</contrib-group>
<aff id="Af1">
<institution><![CDATA[,Universidad Autónoma del Estado de México Centro Universitario ]]></institution>
<addr-line><![CDATA[ ]]></addr-line>
<country>Mexico</country>
</aff>
<aff id="Af2">
<institution><![CDATA[,Centro Regional de Desarrollo Espacial Atlacomulco  ]]></institution>
<addr-line><![CDATA[Atlacomulco Estado de México]]></addr-line>
</aff>
<pub-date pub-type="pub">
<day>00</day>
<month>04</month>
<year>2025</year>
</pub-date>
<pub-date pub-type="epub">
<day>00</day>
<month>04</month>
<year>2025</year>
</pub-date>
<volume>13</volume>
<numero>73</numero>
<fpage>1</fpage>
<lpage>14</lpage>
<copyright-statement/>
<copyright-year/>
<self-uri xlink:href="http://www.scielo.org.mx/scielo.php?script=sci_arttext&amp;pid=S2007-97532025000200001&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://www.scielo.org.mx/scielo.php?script=sci_abstract&amp;pid=S2007-97532025000200001&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://www.scielo.org.mx/scielo.php?script=sci_pdf&amp;pid=S2007-97532025000200001&amp;lng=en&amp;nrm=iso"></self-uri><abstract abstract-type="short" xml:lang="es"><p><![CDATA[Resumen Los satélites de tamaño reducido requieren de una buena regulación de orientación que les permita contrarrestar perturbaciones una vez desplegados, sin embargo, realizar pruebas en operación es complicado, por ello se requieren herramientas que representen el comportamiento de un satélite para evaluar la viabilidad de reguladores. Este trabajo aborda la construcción de un dispositivo a partir de un cojinete neumático y motores con ruedas de reacción, capaz de representar el movimiento rotacional de un satélite en órbita, describiendo el proceso de construcción, dispositivos utilizados, y la configuración de los sensores; de igual manera se realizan pruebas de funcionamiento en la medición de la orientación y la atenuación de interferencia provocado por el flujo de aire del dispositivo neumático y el movimiento de los motores.]]></p></abstract>
<abstract abstract-type="short" xml:lang="en"><p><![CDATA[Abstract Small satellites require a good orientation regulation that allows them to counteract disturbances once in orbit, however, testing in operation is complicated, so tools that represent the behavior of a satellite are required to assess the feasibility of regulators. This work deals with the construction of a device based on a pneumatic bearing and reaction wheels motors, capable of representing the rotational movement of a satellite in orbit describing the construction process; the devices used, and the configuration of the sensors; likewise, operational tests are carried out on the measurement of the orientation and attenuation of interference caused by the air flow of the pneumatic device and the vibrations generated by the movement of the motors.]]></p></abstract>
<kwd-group>
<kwd lng="es"><![CDATA[Cojinete neumático]]></kwd>
<kwd lng="es"><![CDATA[Ruedas de reacción]]></kwd>
<kwd lng="es"><![CDATA[Satélites]]></kwd>
<kwd lng="es"><![CDATA[Regulador de orientación]]></kwd>
<kwd lng="es"><![CDATA[Unidad de medición inercial]]></kwd>
<kwd lng="en"><![CDATA[Air bearing]]></kwd>
<kwd lng="en"><![CDATA[Reaction wheels]]></kwd>
<kwd lng="en"><![CDATA[Satellites]]></kwd>
<kwd lng="en"><![CDATA[Orientation regulator]]></kwd>
<kwd lng="en"><![CDATA[Inertial measurement unit]]></kwd>
</kwd-group>
</article-meta>
</front><back>
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