uks-orb-all.xml 10.3 KB
<?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-2.4.1.xsd">
  <Version>2.4.1</Version>
  <NumericalData>
    <ResourceID>spase://CNES/NumericalData/CDPP-AMDA/UKS/ORBIT/uks-orb-all</ResourceID>
    <ResourceHeader>
      <ResourceName>orbit</ResourceName>
      <AlternateName>ephemeris</AlternateName>
      <ReleaseDate>2020-02-04T16:16:40Z</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/CDPP/AMDA</RepositoryID>
      <Availability>Online</Availability>
      <AccessRights>Open</AccessRights>
      <AccessURL>
        <Name>CDPP/AMDA HAPI Server</Name>
        <URL>https://amda.irap.omp.eu/service/hapi</URL>
        <Style>HAPI</Style>
        <ProductKey>uks-orb-all</ProductKey>
        <Description>Web Service to this product using the HAPI interface.</Description>
      </AccessURL>
      <Format>CSV</Format>
      <Acknowledgement>Thank you for acknowledging the use of AMDA in publications with wording like "Data analysis was performed with the AMDA science analysis system provided by the Centre de Données de la Physique des Plasmas (CDPP) supported by CNRS, CNES, Observatoire de Paris and Université Paul Sabatier, Toulouse". See the Rules of the road at https://amda.cdpp.eu/help/policy.html . Please acknowledge the Data Providers.</Acknowledgement>
    </AccessInformation>
    <AccessInformation>
      <RepositoryID>spase://SMWG/Repository/CDPP/AMDA</RepositoryID>
      <Availability>Online</Availability>
      <AccessRights>Open</AccessRights>
      <AccessURL>
        <Name>CDPP/AMDA Web application</Name>
        <URL>https://amda.cdpp.eu</URL>
        <Description>Access to Data via CDPP/AMDA Web application.</Description>
      </AccessURL>
      <Format>CSV</Format>
      <Format>VOTable</Format>
      <Format>CDF</Format>
      <Format>PNG</Format>
      <Acknowledgement>Thank you for acknowledging the use of AMDA in publications with wording like "Data analysis was performed with the AMDA science analysis system provided by the Centre de Données de la Physique des Plasmas (CDPP) supported by CNRS, CNES, Observatoire de Paris and Université Paul Sabatier, Toulouse". See the Rules of the road at https://amda.cdpp.eu/help/policy.html . Please acknowledge the Data Providers.</Acknowledgement>
    </AccessInformation>
    <InstrumentID>spase://CNES/Instrument/CDPP-AMDA/UKS/Ephemeris</InstrumentID>
    <MeasurementType>Ephemeris</MeasurementType>
    <TemporalDescription>
      <TimeSpan>
        <StartDate>1984-08-18T23:55:00Z</StartDate>
        <StopDate>1985-01-15T08:00:00Z</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>
      <Support>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <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>
      <Support>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>IRM_to_UKS_gse</Name>
      <ParameterKey>uks_orb_scdist</ParameterKey>
      <Description>
               UKS Spacecraft position relative to IRM in GSE Cartesian coordinates
           </Description>
      <Units>km</Units>
      <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>
      <Support>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>vel_gse</Name>
      <ParameterKey>uks_orb_v</ParameterKey>
      <Description>
               Spacecraft velocity in GSE Cartesian coordinates
           </Description>
      <Units>km/s</Units>
      <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>
      <Support>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>vel_gsm</Name>
      <ParameterKey>uks_orb_vgsm</ParameterKey>
      <Description>
               Spacecraft velocity in GSM Cartesian coordinates
           </Description>
      <Units>km/s</Units>
      <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>
      <Support>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
    <Parameter>
      <Name>distance uks-earth</Name>
      <ParameterKey>uks_orb_mag</ParameterKey>
      <Description>
               Spacecraft distance to earth center
           </Description>
      <Units>Re</Units>
      <RenderingHints>
        <DisplayType>TimeSeries</DisplayType>
      </RenderingHints>
      <Support>
        <SupportQuantity>Positional</SupportQuantity>
      </Support>
    </Parameter>
  </NumericalData>
</Spase>