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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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Details

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
RolePersonStartDateStopDateNote
1.PrincipalInvestigatorspase://CNES/Person/CDPP-Archive/Stas.Barabash
AccessInformation
RepositoryID
Availability
Online
AccessURL
Name
REGARDS
URL
Description

Access via CNES Data Archive for CDPP

Format
CDF
InstrumentIDs
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