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NumericalData/AMDA/Cluster/Cluster4/Ephemeris/clust4-orb-all.xml 5.4 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://cdpp1.cesr.fr/AMDA-NG/public/schemas/spase-amda-1_2_0.xsd">
    <Version>2.2.6</Version>
    <NumericalData>
        <ResourceID>spase://CDPP/NumericalData/AMDA/Cluster/Cluster4/Ephemeris/clust4-orb-all</ResourceID>
        <ResourceHeader>
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            <ResourceName>orbit</ResourceName>
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            <ReleaseDate>2015-10-16T16:00:00</ReleaseDate>
            <Description>Cluster-2 (FM8/Tango) satellite position and magnetic field model information.</Description>         
            <Contact>
                <PersonID>spase://SMWG/Person/Elena.Budnik</PersonID>
                <Role>TechnicalContact</Role>
            </Contact>
        </ResourceHeader>
        <AccessInformation>
            <RepositoryID>spase://SMWG/Repository/CDPP/AMDA</RepositoryID>
            <Availability>Online</Availability>
            <AccessRights>Open</AccessRights>
            <AccessURL>
                <Name>AMDA at CDPP</Name>
                <URL>amda.cdpp.eu</URL>                
            </AccessURL>
            <Format>NetCDF</Format>
        </AccessInformation>
        <ProviderName>IRAP</ProviderName>
        <InstrumentID>spase://CDPP/Instrument/AMDA/Cluster-Tango/Ephemeris</InstrumentID>
        <MeasurementType>Ephemeris</MeasurementType>
        <TemporalDescription>
            <TimeSpan>
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                <StartDate>2000-08-22T00:00:00Z</StartDate>
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                <StopDate>2015-11-01T23:59:00Z</StopDate>
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            </TimeSpan>
            <Cadence>PT1M</Cadence>
        </TemporalDescription>     
        <Parameter>
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            <Name>xyz_gse</Name>
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            <ParameterKey>c4_xyz_gse</ParameterKey>
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            <Description>Spacecraft position in GSE</Description>
            <Ucd>pos.earth;instr.obsty</Ucd>
            <Units>Re</Units>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>x</Name>
                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
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                    <ParameterKey>c4_xyz_gse(0)</ParameterKey>
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                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>y</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
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                    <ParameterKey>c4_xyz_gse(1)</ParameterKey>
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                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>z</Name>
                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
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                    <ParameterKey>c4_xyz_gse(2)</ParameterKey>
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                    <FillValue>-1.0E31</FillValue>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter> 
        <Parameter>
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            <Name>xyz_gsm</Name>
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            <ParameterKey>c4_xyz_gsm</ParameterKey>
            <Description>Spacecraft position in GSM</Description>
            <Ucd>pos.earth;instr.obsty</Ucd>
            <Units>km</Units>
            <UnitsConversion>1e3&gt;m</UnitsConversion>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSM</CoordinateSystemName>
            </CoordinateSystem>
            <Structure>
                <Size>3</Size>
                <Element>
                    <Name>x</Name>
                    <Qualifier>Component.I</Qualifier>
                    <Index>1</Index>
                    <ParameterKey>c4_xyz_gsm(0)</ParameterKey>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>y</Name>
                    <Qualifier>Component.J</Qualifier>
                    <Index>2</Index>
                    <ParameterKey>c4_xyz_gsm(1)</ParameterKey>
                    <FillValue>-1.0E31</FillValue>
                </Element>
                <Element>
                    <Name>z</Name>
                    <Qualifier>Component.K</Qualifier>
                    <Index>3</Index>
                    <ParameterKey>c4_xyz_gsm(2)</ParameterKey>
                    <FillValue>-1.0E31</FillValue>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>        
        <Parameter>
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            <Name>distance c4-earth</Name>
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            <ParameterKey>c4_r</ParameterKey>
            <Description/>
            <Ucd>pos.earth;instr.obsty</Ucd>
            <Units>Re</Units>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>                            
            </RenderingHints>
            <ValidMin>0.0</ValidMin>
            <FillValue>-1.0E31</FillValue>
            <Support>
                <Qualifier>Magnitude</Qualifier>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter> 
    </NumericalData>
</Spase>