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VENUS EXPRESS: ASPERA-4 IMA Ancillary Geometry Parameters (CDF)

ResourceID
spase://CNES/NumericalData/CDPP-Archive/VEX/ASPERA4/VEX_ASPERA4_ORB

Description
This data set contains the VEX spacecraft position and attitude in both EMEJ2000 and VSO coordinates system.

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Version:2.4.0

NumericalData

ResourceID
spase://CNES/NumericalData/CDPP-Archive/VEX/ASPERA4/VEX_ASPERA4_ORB
ResourceHeader
ResourceName
VENUS EXPRESS: ASPERA-4 IMA Ancillary Geometry Parameters (CDF)
DOI
https://doi.org/10.24400/802406/y8dv-3654
ReleaseDate
2022-06-06 17:35:00Z
Description
This data set contains the VEX spacecraft position and attitude in both EMEJ2000 and VSO coordinates system.
Acknowledgement
Please acknowledge the Principal Investigator(s) as well as the ESA Planetary Science Archive and the CDPP (Centre des Données de la Physique des Plasmas) when making a publication using the data you are going to download. Principal Investigator(s): S. Barabash (IRF, Kiruna, Sweden)
Contacts
Role Person StartDate StopDate Note
1. PrincipalInvestigator spase://CNES/Person/CDPP-Archive/Stas.Barabash
AccessInformation
RepositoryID
spase://CNES/Repository/CDPP-Archive/REGARDS-CDPP
Availability
Online
AccessURL
Name
REGARDS
URL
https://regards.cnes.fr/user/cdpp/modules/1777?sp=DatasetName;q=DatasetName:VEX_ASPERA4_ORB
Description
Access via CNES Data Archive for CDPP
Format
CDF
InstrumentIDs
spase://CNES/Instrument/CDPP-Archive/VEX/ASPERA4/IMA
MeasurementType
Ephemeris
TemporalDescription
TimeSpan
StartDate
2005-12-09 00:00:00Z
StopDate
2014-11-27 00:00:00Z
ObservedRegion
Venus.Magnetosphere
Parameter #1
Name
Position X EMEJ2000
Description
x-coordinate position of the satellite defined in the centered EMEJ2000 reference frame.
Units
km
UnitsConversion
1e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
J2000
Support
Qualifier
Component.I
SupportQuantity
Positional
Parameter #2
Name
Position Y EMEJ2000
Description
y-coordinate position of the satellite defined in the centered EMEJ2000 reference frame.
Units
km
UnitsConversion
1e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
J2000
Support
Qualifier
Component.J
SupportQuantity
Positional
Parameter #3
Name
Position Z EMEJ2000
Description
z-coordinate position of the satellite defined in the centered EMEJ2000 reference frame.
Units
km
UnitsConversion
1e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
J2000
Support
Qualifier
Component.K
SupportQuantity
Positional
Parameter #4
Name
Attitude 1 EMEJ2000
Description
1st attitude parameter of the satellite defined in the centered EMEJ2000 reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
J2000
Support
SupportQuantity
Orientation
Parameter #5
Name
Attitude 2 EMEJ2000
Description
2nd attitude parameter of the satellite defined in the centered EMEJ2000 reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
J2000
Support
SupportQuantity
Orientation
Parameter #6
Name
Attitude 3 EMEJ2000
Description
3rd attitude parameter of the satellite defined in the centered EMEJ2000 reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
J2000
Support
SupportQuantity
Orientation
Parameter #7
Name
Attitude 4 EMEJ2000
Description
4th attitude parameter of the satellite defined in the centered EMEJ2000 reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
J2000
Support
SupportQuantity
Orientation
Parameter #8
Name
Attitude 5 EMEJ2000
Description
5th attitude parameter of the satellite defined in the centered EMEJ2000 reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
J2000
Support
SupportQuantity
Orientation
Parameter #9
Name
Attitude 6 EMEJ2000
Description
6th attitude parameter of the satellite defined in the centered EMEJ2000 reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
J2000
Support
SupportQuantity
Orientation
Parameter #10
Name
Attitude 7 EMEJ2000
Description
7th attitude parameter of the satellite defined in the centered EMEJ2000 reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
J2000
Support
SupportQuantity
Orientation
Parameter #11
Name
Attitude 8 EMEJ2000
Description
8th attitude parameter of the satellite defined in the centered EMEJ2000 reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
J2000
Support
SupportQuantity
Orientation
Parameter #12
Name
Attitude 9 EMEJ2000
Description
9th attitude parameter of the satellite defined in the centered EMEJ2000 reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
J2000
Support
SupportQuantity
Orientation
Parameter #13
Name
Position X VSO
Description
x-coordinate position of the satellite defined in the VSO reference frame.
Units
km
UnitsConversion
1e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
VSO
Support
Qualifier
Component.I
SupportQuantity
Positional
Parameter #14
Name
Position Y VSO
Description
y-coordinate position of the satellite defined in the VSO reference frame.
Units
km
UnitsConversion
1e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
VSO
Support
Qualifier
Component.J
SupportQuantity
Positional
Parameter #15
Name
Position Z VSO
Description
z-coordinate position of the satellite defined in the VSO reference frame.
Units
km
UnitsConversion
1e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
VSO
Support
Qualifier
Component.K
SupportQuantity
Positional
Parameter #16
Name
Attitude 1 VSO
Description
1st attitude parameter of the satellite defined in the VSO reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
VSO
Support
SupportQuantity
Orientation
Parameter #17
Name
Attitude 2 VSO
Description
2nd attitude parameter of the satellite defined in the VSO reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
VSO
Support
SupportQuantity
Orientation
Parameter #18
Name
Attitude 3 VSO
Description
3rd attitude parameter of the satellite defined in the VSO reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
VSO
Support
SupportQuantity
Orientation
Parameter #19
Name
Attitude 4 VSO
Description
4th attitude parameter of the satellite defined in the VSO reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
VSO
Support
SupportQuantity
Orientation
Parameter #20
Name
Attitude 5 VSO
Description
5th attitude parameter of the satellite defined in the VSO reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
VSO
Support
SupportQuantity
Orientation
Parameter #21
Name
Attitude 6 VSO
Description
6th attitude parameter of the satellite defined in the VSO reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
VSO
Support
SupportQuantity
Orientation
Parameter #22
Name
Attitude 7 VSO
Description
7th attitude parameter of the satellite defined in the VSO reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
VSO
Support
SupportQuantity
Orientation
Parameter #23
Name
Attitude 8 VSO
Description
8th attitude parameter of the satellite defined in the VSO reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
VSO
Support
SupportQuantity
Orientation
Parameter #24
Name
Attitude 9 VSO
Description
9th attitude parameter of the satellite defined in the VSO reference frame.
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
VSO
Support
SupportQuantity
Orientation
Parameter #25
Name
Mission phase
Description
The CRUISE sub-phase corresponds to data collected before the VOI (VENUS Orbit Injection), including the Near Earth Verification (NEV) and Interplanetary Cruise (IC) sub-phases. After the VOI, the nominal mission is divided into different VENUS mission sub-phases defined by the VENUS EXPRESS mission planning.
Support
SupportQuantity
Other
Parameter #26
Name
Orbit number
Description
Orbit number
Support
SupportQuantity
Other