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NumericalData/CDPP-AMDA/UKS/ORBIT/uks-orb-all.xml 9.83 KB
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<?xml version="1.0" encoding="UTF-8"?>
<Spase xmlns="http://www.spase-group.org/data/schema" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.spase-group.org/data/schema http://www.spase-group.org/data/schema/spase-2_3_0.xsd">
   <Version>2.3.0</Version>
   <NumericalData>
      <ResourceID>spase://CNES/NumericalData/CDPP-AMDA/UKS/ORBIT/uks-orb-all</ResourceID>
      <ResourceHeader>
          <ResourceName>orbit</ResourceName>
          <AlternateName>ephemeris</AlternateName>      
          <ReleaseDate>2019-05-05T12:34:56Z</ReleaseDate>
         <Description>           
         </Description>
          <Acknowledgement>User will acknowledge the AMPTE/UKS team in any publication resulting from the use of these data.
         </Acknowledgement>
         <Contact>
           <PersonID>spase://SMWG/Person/David.J.Southwood</PersonID>
           <Role>PrincipalInvestigator</Role>
         </Contact>
          <Contact>
              <PersonID>spase://SMWG/Person/Malcolm.W.Dunlop</PersonID>
              <Role>DataProducer</Role>
          </Contact>
         <InformationURL>
           <Name>NSSDC Master Catalog</Name>
             <URL>https://nssdc.gsfc.nasa.gov/nmc/experiment/display.action?id=1984-088C-04</URL>
           <Description>
           </Description>
         </InformationURL>
      </ResourceHeader>
      <AccessInformation>
         <RepositoryID>spase://SMWG/Repository/CNES/CDPP-AMDA</RepositoryID>
         <Availability>Online</Availability>
         <AccessRights>Open</AccessRights>
         <AccessURL>
            <Name>AMDA at CDPP</Name>
            <URL>
                http://amda.cdpp.eu
            </URL>
         </AccessURL>
         <Format>Text</Format>
         <Acknowledgement>
                AMDA is a science analysis system provided by the Centre de Donnees de la 
                Physique des Plasmas (CDPP) supported by CNRS, CNES, Observatoire de Paris and 
                Universite Paul Sabatier, Toulouse
         </Acknowledgement>
      </AccessInformation>
      <ProviderName></ProviderName> 
       <ProviderResourceName></ProviderResourceName>
      <ProviderAcknowlegment> </ProviderAcknowlegment>
      <InstrumentID>spase://CNES/Instrument/CDPP-AMDA/UKS/Ephemeris</InstrumentID>
      <MeasurementType>Ephemeris</MeasurementType>
      <TemporalDescription>
         <TimeSpan>
             <StartDate>1984-08-25T07:31:00</StartDate>
             <StopDate>1985-06-15T23:59:59</StopDate>
         </TimeSpan>
          <Cadence>PT300S</Cadence>
      </TemporalDescription>
       <ObservedRegion>Earth.Magnetosheath</ObservedRegion>
       <ObservedRegion>Earth.Magnetosphere</ObservedRegion>
       <ObservedRegion>Earth.Magnetosphere.Magnetotail</ObservedRegion>   
       <ObservedRegion>Heliosphere.NearEarth</ObservedRegion>
      <Parameter>
         <Name>xyz_gse</Name>
         <ParameterKey>uks_orb_xyz</ParameterKey>
         <Description>
             Spacecraft position in GSE Cartesian coordinates
         </Description>
         <Units>Re</Units>
         <UnitsConversion>6.378e6;km</UnitsConversion>
         <CoordinateSystem>
            <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
            <CoordinateSystemName>GSE</CoordinateSystemName>
         </CoordinateSystem>
         <RenderingHints>
              <DisplayType>TimeSeries</DisplayType>
         </RenderingHints>
         <Structure>
            <Size>3</Size>
            <Element>
                <Name>x</Name>
                <Qualifier>Component.I</Qualifier>
                <Index>1</Index>
                <ParameterKey>uks_orb_xyz(0)</ParameterKey>                           
            </Element>
            <Element>
                <Name>y</Name>
                <Qualifier>Component.J</Qualifier>
                <Index>2</Index>
                <ParameterKey>uks_orb_xyz(1)</ParameterKey>      
            </Element>
            <Element>
                <Name>z</Name>
                <Qualifier>Component.K</Qualifier>
                <Index>3</Index>
                <ParameterKey>uks_orb_xyz(2)</ParameterKey> 
            </Element>
         </Structure>
      </Parameter>
       <Parameter>
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           <Name>xyz_gsm</Name>
           <ParameterKey>uks_orb_gsm</ParameterKey>
           <Description>
               Spacecraft position in GSM Cartesian coordinates
           </Description>
           <Units>Re</Units>
           <UnitsConversion>6.378e6;km</UnitsConversion>
           <CoordinateSystem>
               <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
               <CoordinateSystemName>GSM</CoordinateSystemName>
           </CoordinateSystem>
           <RenderingHints>
               <DisplayType>TimeSeries</DisplayType>
           </RenderingHints>
           <Structure>
               <Size>3</Size>
               <Element>
                   <Name>x</Name>
                   <Qualifier>Component.I</Qualifier>
                   <Index>1</Index>
                   <ParameterKey>uks_orb_gsm(0)</ParameterKey>                           
               </Element>
               <Element>
                   <Name>y</Name>
                   <Qualifier>Component.J</Qualifier>
                   <Index>2</Index>
                   <ParameterKey>uks_orb_gsm(1)</ParameterKey>      
               </Element>
               <Element>
                   <Name>z</Name>
                   <Qualifier>Component.K</Qualifier>
                   <Index>3</Index>
                   <ParameterKey>uks_orb_gsm(2)</ParameterKey> 
               </Element>
           </Structure>
       </Parameter>
       <Parameter>
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           <Name>IRM_to_UKS_gse</Name>
           <ParameterKey>uks_orb_scdist</ParameterKey>
           <Description>
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               UKS Spacecraft position relative to IRM in GSE Cartesian coordinates
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           </Description>
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           <Units>km</Units>
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           <CoordinateSystem>
               <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
               <CoordinateSystemName>GSE</CoordinateSystemName>
           </CoordinateSystem>
           <RenderingHints>
               <DisplayType>TimeSeries</DisplayType>
           </RenderingHints>
           <Structure>
               <Size>3</Size>
               <Element>
                   <Name>x</Name>
                   <Qualifier>Component.I</Qualifier>
                   <Index>1</Index>
                   <ParameterKey>uks_orb_scdist(0)</ParameterKey>                           
               </Element>
               <Element>
                   <Name>y</Name>
                   <Qualifier>Component.J</Qualifier>
                   <Index>2</Index>
                   <ParameterKey>uks_orb_scdist(1)</ParameterKey>      
               </Element>
               <Element>
                   <Name>z</Name>
                   <Qualifier>Component.K</Qualifier>
                   <Index>3</Index>
                   <ParameterKey>uks_orb_scdist(2)</ParameterKey> 
               </Element>
           </Structure>
       </Parameter>
       <Parameter>
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           <Name>vel_gse</Name>
           <ParameterKey>uks_orb_v</ParameterKey>
           <Description>
               Spacecraft velocity in GSE Cartesian coordinates
           </Description>
           <Units>km/s</Units>
           <UnitsConversion></UnitsConversion>
           <CoordinateSystem>
               <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
               <CoordinateSystemName>GSE</CoordinateSystemName>
           </CoordinateSystem>
           <RenderingHints>
               <DisplayType>TimeSeries</DisplayType>
           </RenderingHints>
           <Structure>
               <Size>3</Size>
               <Element>
                   <Name>vx</Name>
                   <Qualifier>Component.I</Qualifier>
                   <Index>1</Index>
                   <ParameterKey>uks_orb_v(0)</ParameterKey>                           
               </Element>
               <Element>
                   <Name>vy</Name>
                   <Qualifier>Component.J</Qualifier>
                   <Index>2</Index>
                   <ParameterKey>uks_orb_v(1)</ParameterKey>      
               </Element>
               <Element>
                   <Name>vz</Name>
                   <Qualifier>Component.K</Qualifier>
                   <Index>3</Index>
                   <ParameterKey>uks_orb_v(2)</ParameterKey> 
               </Element>
           </Structure>
       </Parameter>
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       <Parameter>
           <Name>vel_gsm</Name>
           <ParameterKey>uks_orb_vgsm</ParameterKey>
           <Description>
               Spacecraft velocity in GSM Cartesian coordinates
           </Description>
           <Units>km/s</Units>
           <UnitsConversion></UnitsConversion>
           <CoordinateSystem>
               <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
               <CoordinateSystemName>GSM</CoordinateSystemName>
           </CoordinateSystem>
           <RenderingHints>
               <DisplayType>TimeSeries</DisplayType>
           </RenderingHints>
           <Structure>
               <Size>3</Size>
               <Element>
                   <Name>vx</Name>
                   <Qualifier>Component.I</Qualifier>
                   <Index>1</Index>
                   <ParameterKey>uks_orb_vgsm(0)</ParameterKey>                           
               </Element>
               <Element>
                   <Name>vy</Name>
                   <Qualifier>Component.J</Qualifier>
                   <Index>2</Index>
                   <ParameterKey>uks_orb_vgsm(1)</ParameterKey>      
               </Element>
               <Element>
                   <Name>vz</Name>
                   <Qualifier>Component.K</Qualifier>
                   <Index>3</Index>
                   <ParameterKey>uks_orb_vgsm(2)</ParameterKey> 
               </Element>
           </Structure>
       </Parameter>
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</NumericalData>
</Spase>