CDPP / CNES

Blame view

NumericalData/AMDA/ISEE/ISEE1/Ephemeris/isee1-orb-all.xml 5.55 KB
Edit Raw Normal View History
1bcff323   Elena.Budnik   NumericalData 
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
 
<?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/ISEE/ISEE1/Ephemeris/isee1-orb-all</ResourceID>
        <ResourceHeader>
            <ResourceName>ISEE 1 Orbit</ResourceName>
            <ReleaseDate>2015-10-16T14:28:00</ReleaseDate>
            <Description/>
            <Contact>
                <PersonID>spase://SMWG/Person/Elena.Budnik</PersonID>
                <Role>TechnicalContact</Role>
            </Contact>
            <InformationURL>
                <Name>UCLA-IGPP ISEE Magnetometer Interactive Data Server</Name>
                <URL>http://www-ssc.igpp.ucla.edu/forms/isee</URL>
                <Description>Data at 60-s and 4-s resolution are available for the entire ISEE mission (October 22, 1977 through  September 25, 1987) and can be displayed either as a plot or an ASCII listing. The ISEE-1 and -2 magnetometer data server is provided by the Institute of Geophysics and Planetary Physics (IGPP) at UCLA, through a grant to Robert J. Strangeway from the NASA Space Physics Data System (SPDS).</Description>
            </InformationURL>
        </ResourceHeader>
        <AccessInformation>
            <RepositoryID>spase://SMWG/Repository/CDPP/AMDA</RepositoryID>
            <AccessRights>Open</AccessRights>
            <AccessURL>
                <Name>AMDA at CDPP</Name>
                <URL>http://amda.cdpp.eu</URL>
            </AccessURL>
            <Format>NetCDF</Format>
        </AccessInformation>
        <ProviderName>NSSDC</ProviderName>
        <ProcessingLevel>Calibrated</ProcessingLevel>
        <InstrumentID>spase://CDPP/Instrument/AMDA/ISEE1/Ephemeris</InstrumentID>
        <MeasurementType>Ephemeris</MeasurementType>
        <TemporalDescription>
            <TimeSpan>
447d3a6e   Elena.Budnik   work 
35
36
 
                <StartDate>1977-10-22T14:49:00Z</StartDate>
                <StopDate>1987-09-26T05:59:00Z</StopDate>
1bcff323   Elena.Budnik   NumericalData 
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
 
            </TimeSpan>
            <Cadence>PT1M</Cadence>
        </TemporalDescription>
        <ObservedRegion>Earth.Magnetosphere</ObservedRegion>
        <ObservedRegion>Earth.Magnetosheath</ObservedRegion>
        <ObservedRegion>Heliosphere.NearEarth</ObservedRegion>
        <Parameter>
            <Name>Spacecraft position vector, GSE</Name>
            <ParameterKey>isee1_xyz</ParameterKey>
            <Description>
                Spacecraft position vector, GSE Cartesian components, in Earth radii
            </Description>
            <Ucd>pos.earth;instr.obsty</Ucd>
            <Cadence>PT1M</Cadence>
            <Units>Re</Units>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSE</CoordinateSystemName>
            </CoordinateSystem>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>
            </RenderingHints>
            <Structure>
                <Size>3</Size>
                <Description>
                    GSE X,Y,Z components of spacecraft position vector
                </Description>
                <Element>
                    <Name>x</Name>
                    <Index>1</Index>
                    <ParameterKey>isee1_xyz(0)</ParameterKey>
                </Element>
                <Element>
                    <Name>y</Name>
                    <Index>2</Index>
                    <ParameterKey>isee1_xyz(1)</ParameterKey>
                </Element>
                <Element>
                    <Name>z</Name>
                    <Index>3</Index>
                    <ParameterKey>isee1_xyz(2)</ParameterKey>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
        <Parameter>
            <Name>Spacecraft position vector, GSM</Name>
            <ParameterKey>isee1_xyz_gsm</ParameterKey>
            <Description>
                Spacecraft position vector, GSM Cartesian components, in Earth radii
            </Description>
            <Ucd>pos.earth;instr.obsty</Ucd>
            <Cadence>PT1M</Cadence>
            <Units>Re</Units>
            <CoordinateSystem>
                <CoordinateRepresentation>Cartesian</CoordinateRepresentation>
                <CoordinateSystemName>GSM</CoordinateSystemName>
            </CoordinateSystem>
            <RenderingHints>
                <DisplayType>TimeSeries</DisplayType>
            </RenderingHints>
            <Structure>
                <Size>3</Size>
                <Description>GSM X,Y,Z components of spacecraft position vector
                </Description>
                <Element>
                    <Name>x gsm</Name>
                    <Index>1</Index>
                    <ParameterKey>isee1_xyz_gsm(0)</ParameterKey>
                </Element>
                <Element>
                    <Name>y gsm</Name>
                    <Index>2</Index>
                    <ParameterKey>isee1_xyz_gsm(1)</ParameterKey>
                </Element>
                <Element>
                    <Name>z gsm</Name>
                    <Index>3</Index>
                    <ParameterKey>isee1_xyz_gsm(2)</ParameterKey>
                </Element>
            </Structure>
            <Support>
                <SupportQuantity>Positional</SupportQuantity>
            </Support>
        </Parameter>
    </NumericalData>
</Spase>