HPDE.io

cruise

ResourceID
spase://CNES/NumericalData/CDPP-AMDA/Rosetta/Ephemeris/ros-orb-cruise

Description

Coordinate systems used for cruise phase:
* 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 vectororthogonal to the Z axis. The Y axis is Z cross X, completing the right-handed reference frame.

View XML | View JSON | Edit

Details

Version:2.4.1

NumericalData

ResourceID
spase://CNES/NumericalData/CDPP-AMDA/Rosetta/Ephemeris/ros-orb-cruise
ResourceHeader
ResourceName
cruise
ReleaseDate
2014-08-26 10:45:57Z
Description

Coordinate systems used for cruise phase:
* 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 vectororthogonal to the Z axis. The Y axis is Z cross X, completing the right-handed reference frame.

Contacts
RolePersonStartDateStopDateNote
1.TechnicalContactspase://SMWG/Person/Elena.Budnik
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
CDPP/AMDA HAPI Server
URL
Style
HAPI
Description

Web Service to this product using the HAPI interface.

Format
CSV
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 http://amda.cdpp.eu/help/policy.html. Please acknowledge the Data Providers.
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
CDPP/AMDA Web application
URL
Description

Access to Data via CDPP/AMDA Web application.

Format
CSV
Format
VOTable
Format
CDF
Format
PNG
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 http://amda.cdpp.eu/help/policy.html. Please acknowledge the Data Providers.
ProviderName
PSA
InstrumentIDs
MeasurementType
Ephemeris
TemporalDescription
TimeSpan
StartDate
2004-03-03 00:00:00Z
StopDate
2014-08-04 00:00:00Z
Cadence
PT1H
Parameter #1
Name
xyz_hee
ParameterKey
ros_xyz_hee
Units
AU
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
HEE
Structure
Size
3
Element
Name
x
Index
1
ParameterKey
ros_xyz_hee(0)
Element
Name
y
Index
2
ParameterKey
ros_xyz_hee(1)
Element
Name
z
Index
3
ParameterKey
ros_xyz_hee(2)
Support
SupportQuantity
Positional
Parameter #2
Name
xyz_heeq
ParameterKey
ros_xyz_heeq
UCD
pos.bodyrc;instr.obsty
Units
AU
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
HEEQ
RenderingHints
DisplayType
TimeSeries
Structure
Size
3
Element
Name
x
Index
1
ParameterKey
ros_xyz_heeq(0)
Element
Name
y
Index
2
ParameterKey
ros_xyz_heeq(1)
Element
Name
z
Index
3
ParameterKey
ros_xyz_heeq(2)
Support
SupportQuantity
Positional
Parameter #3
Name
xyz_hci
ParameterKey
ros_xyz_hci
UCD
pos.bodyrc;instr.obsty
Units
AU
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
HCI
RenderingHints
DisplayType
TimeSeries
Structure
Size
3
Element
Name
x
Index
1
ParameterKey
ros_xyz_hci(0)
Element
Name
y
Index
2
ParameterKey
ros_xyz_hci(1)
Element
Name
z
Index
3
ParameterKey
ros_xyz_hci(2)
Support
SupportQuantity
Positional
Parameter #4
Name
distance ros-sun
ParameterKey
r_sun_ros
Units
AU
RenderingHints
DisplayType
TimeSeries
Support
SupportQuantity
Positional