work

Elena.Budnik
1 parent 9f5f85d6
Showing 6 changed files with 178 additions and 5 deletions Show diff stats
Instrument/AMDA/Rosetta/Ephemeris.xml
NumericalData/AMDA/Rosetta/Ephemeris/ros-orb-comet.xml
NumericalData/AMDA/Rosetta/Ephemeris/ros-orb-cruise.xml
NumericalData/AMDA/Rosetta/Ephemeris/ros-orb-earth1.xml
NumericalData/AMDA/Rosetta/Ephemeris/ros-orb-mars.xml
NumericalData/AMDA/Rosetta/Ephemeris/sun-pol-cgck.xml
@@ -7,7 +7,15 @@
       <ResourceName>Ephemeris</ResourceName>
       <AlternateName> </AlternateName>
       <ReleaseDate>2009-05-20T21:10:13Z</ReleaseDate>
-      <Description>A </Description>
+      <Description>
+    Rosetta Ephemeris data are calculated using SPICE kernels taken from the
+           ftp://ssols01.esac.esa.int/pub/data/SPICE/ROSETTA/kernels/
+            (PSA)
+            
+   Coordinates :
+   
+                
+</Description>
       <Contact>      
         <PersonID></PersonID>
         <Role>MetadataContact</Role>
@@ -6,7 +6,62 @@
     <ResourceHeader>
       <ResourceName>P67 Orbit</ResourceName>
       <ReleaseDate>2015-10-16T16:25:29Z</ReleaseDate>
-      <Description/>
+      <Description>CSO The body-Centered Solar Orbital frames for the Rosetta primary
+   target comet 67P/Churyumov-Gerasimenko, incidental target comet
+   45P/Honda-Mrkos-Pajdusakowa (Rosetta passed through its ion tail in
+   July 2006), and secondary targets asteroids 2867/STEINS and
+   21/LUTETIA are named '67P/C-G_CSO', '45P/H-M-P_CSO',
+   '2867/STEINS_CSO', and '21/LUTETIA_CSO'. 
+   These frames are defined as
+   a two-vector style dynamic frames as follows:
+ 
+      -  The position of the sun relative to the body is the primary
+         vector: the X axis points from the body to the sun.
+
+      -  The inertially referenced velocity of the sun relative to the
+         body is the secondary vector: the Y axis is the component of
+         this velocity vector orthogonal to the X axis.
+
+      -  The Z axis is X cross Y, completing the right-handed reference
+         frame.
+
+      -  All vectors are geometric: no aberration corrections are used.
+ 
+    
+
+   CSEQ  The body-Centered Solar EQuatorial frames for the Rosetta
+   primary target comet 67P/Churyumov-Gerasimenko and secondary target
+   asteroid 21/LUTETIA are named '67P/C-G_CSEQ' and '21/LUTETIA_CSEQ'.
+   These frames are defined as a two-vector style dynamic frames as
+   follows:
+ 
+      -  +X axis is the position of the Sun relative to the body; it's
+         the primary vector and points from the body to the Sun;
+
+      -  +Z axis is the component of the Sun's north pole of date
+         orthogonal to the +X axis;
+
+      -  +Y axis completes the right-handed reference frame;
+
+      -  the origin of this frame is the body's center of mass.
+
+   All the vectors are geometric: no aberration corrections are used.
+
+   C_G-CK  C_G comet fixed frame (CK frame) 
+ 
+     A body-fixed frame is defined using standard
+     body-fixed, CK-based frame formation rules:
+   
+      -  +Z axis is toward the North pole;
+
+      -  +X axis is toward the prime meridian;
+
+      -  +Y axis completes the right hand frame;
+
+      -  the origin of this frame is at the center of the body.
+
+   The orientation of this frame is computed by evaluating
+   corresponding C_G comet attitudes kernels. </Description>
       <Contact>
         <PersonID>spase://SMWG/Person/Elena.Budnik</PersonID>
         <Role>MetadataContact</Role>
@@ -6,7 +6,39 @@
     <ResourceHeader>
       <ResourceName>Full Mission</ResourceName>
       <ReleaseDate>2015-10-16T15:25:29Z</ReleaseDate>
-      <Description/>
+      <Description>HCI: Heliocentric Inertial Frame -
+         All vectors are geometric: no aberration corrections are used.
+         The solar rotation axis is the primary vector: the Z axis points
+         in the solar north direction.
+         The solar ascending node on the ecliptic of J2000 forms the X axis.
+         The Y axis is Z cross X, completing the right-handed reference frame.
+         
+    HEE : Heliocentric Earth Ecliptic Frame -
+
+         All vectors are geometric: no aberration corrections are used.
+
+         The position of the Earth relative to the Sun is the primary vector:
+         the X axis points from the Sun to the Earth.
+
+         The northern surface normal to the mean ecliptic of date is the
+         secondary vector: the Z axis is the component of this vector
+         orthogonal to the X axis.
+
+         The Y axis is Z cross X, completing the right-handed reference frame.
+         
+    HEEQ : Heliocentric Earth Equatorial Frame -
+
+         All vectors are geometric: no aberration corrections are used.
+
+         The solar rotation axis is the primary vector: the Z axis points
+         in the solar north direction.
+
+         The position of the Sun relative to the Earth is the secondary
+         vector: the X axis is the component of this position vector
+         orthogonal to the Z axis.
+
+         The Y axis is Z cross X, completing the right-handed reference frame.
+     </Description>
       <Contact>
         <PersonID>spase://SMWG/Person/Elena.Budnik</PersonID>
         <Role>MetadataContact</Role>
@@ -6,7 +6,17 @@
     <ResourceHeader>
       <ResourceName>Earth Flyby 1 Positions</ResourceName>
       <ReleaseDate>2015-10-16T15:18:29Z</ReleaseDate>
-      <Description/>
+      <Description>
+        GSE : Geocentric Solar Ecliptic -
+         This system has its X axis towards the Sun and its Z axis
+         perpendicular to the plane of the Earth's orbit around the
+         Sun (positive North). Y completes the right-handed system.
+         
+   GSM : Geocentric Solar Magnetospheric -
+         This system has its X axis towards the Sun and its Z axis
+         is the projection of the Earth's magnetic dipole axis
+         (positive North) on to the plane perpendicular to the X
+         axis. Y completes the right-handed system.</Description>
       <Contact>
         <PersonID>spase://SMWG/Person/Elena.Budnik</PersonID>
         <Role>MetadataContact</Role>
@@ -6,7 +6,12 @@
     <ResourceHeader>
       <ResourceName>Mars Flyby Positions</ResourceName>
       <ReleaseDate>2015-10-16T16:25:29Z</ReleaseDate>
-      <Description/>
+      <Description>
+    
+    MSO : Mars-centric Solar Orbital   -  
+        the +X-axis points toward the Sun, 
+        +Z points northward perpendicular to Mars's orbit plane, and 
+        Y completes the right hand system nominally directed opposite Mars's orbital velocity around the Sun. </Description>
       <Contact>
         <PersonID>spase://SMWG/Person/Elena.Budnik</PersonID>
         <Role>MetadataContact</Role>
@@ -0,0 +1,63 @@
+<?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/Rosetta/Ephemeris/sun-pol-cgck</ResourceID>
+    <ResourceHeader>
+      <ResourceName>Sun Posin in C-G_CK frame</ResourceName>
+      <ReleaseDate>2015-10-16T15:25:29Z</ReleaseDate>
+      <Description> 
+     </Description>
+      <Contact>
+        <PersonID>spase://SMWG/Person/Elena.Budnik</PersonID>
+        <Role>MetadataContact</Role>
+      </Contact>
+    </ResourceHeader>
+    <AccessInformation>
+      <RepositoryID>spase://SMWG/Repository/CDPP/AMDA</RepositoryID>
+      <Availability>Online</Availability>
+      <AccessRights>Open</AccessRights>
+      <AccessURL>
+        <URL>http://amda.cdpp.eu</URL>
+      </AccessURL>
+      <Format>NetCDF</Format>
+    </AccessInformation>
+    <ProviderName>PSA</ProviderName>
+    <InstrumentID>spase://CDPP/Instrument/AMDA/Rosetta/Ephemeris</InstrumentID>
+    <MeasurementType>Ephemeris</MeasurementType>
+    <TemporalDescription>
+      <TimeSpan>
+        <StartDate>2004-03-03T00:00:00Z</StartDate>
+        <StopDate>2014-08-04T00:00:00Z</StopDate>
+      </TimeSpan>
+      <Cadence>PT60S</Cadence>
+    </TemporalDescription>   
+    <Parameter>
+      <Name>distance C_G-sun</Name>
+      <ParameterKey>sun_cg_r</ParameterKey>
+      <Ucd/>
+      <Units>AU</Units>
+      <RenderingHints>
+        <DisplayType>TimeSeries</DisplayType>
+      </RenderingHints>     
+    </Parameter>
+    <Parameter>
+      <Name>Sun lat C-G_CK</Name>
+      <ParameterKey>sun_cg_lat</ParameterKey>
+      <Ucd/>
+      <Units>degrees</Units>
+      <RenderingHints>
+        <DisplayType>TimeSeries</DisplayType>
+      </RenderingHints>     
+    </Parameter>   
+    <Parameter>
+      <Name>Sun lon C-G_CK</Name>
+      <ParameterKey>sun_cg_lon</ParameterKey>
+      <Ucd/>
+      <Units>degrees</Units>
+      <RenderingHints>
+        <DisplayType>TimeSeries</DisplayType>
+      </RenderingHints>     
+    </Parameter>
+  </NumericalData>
+</Spase>