HDPWS

Data Access

GALILEO PWS AACS

ResourceID
spase://CNES/NumericalData/CDPP-Archive/Galileo/PWS/AACS/GALILEO_PWS_AACS

Description
This data set contains values of Rotor Attitudes (RA Right Ascension, DEC Declination, Twist) from the Galileo PWS AACS (Attitude and Articulation Control System). The period covered by a data file is 3 or 4 h maximum per day (February 10th, 1990 to December 14th, 1992).

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Details

Version:2.4.0

NumericalData

ResourceID
spase://CNES/NumericalData/CDPP-Archive/Galileo/PWS/AACS/GALILEO_PWS_AACS
ResourceHeader
ResourceName
GALILEO PWS AACS
DOI
https://doi.org/10.24400/802406/mxx7-vqdm
ReleaseDate
2022-03-22 11:28:57Z
Description
This data set contains values of Rotor Attitudes (RA Right Ascension, DEC Declination, Twist) from the Galileo PWS AACS (Attitude and Articulation Control System). The period covered by a data file is 3 or 4 h maximum per day (February 10th, 1990 to December 14th, 1992).
Acknowledgement
Users of these data are encouraged to acknowledge NASA, CNES (Centre National d'Etudes Spatiales) and, CNRS (Centre National de la Recherche Scientifique) for their support to the GALILEO-PWS team, and the CDPP (Centre des Données de la Physique des Plasmas) for the distribution of the GALILEO-PWS data, in all publications. If PI/coI are not part of the publication list, then we suggest to also acknowledge Donald A. Gurnett, the late Alain Roux, Charles Kennel and Scott Bolton for use of GALILEO-PWS data.
Contacts

AccessInformation
RepositoryID
Availability
Online
AccessURL
Name
REGARDS
URL
Description
Access via CNES Data Archive for CDPP
Format
Text.ASCII
InstrumentIDs
MeasurementType
Waves.Passive
MeasurementType
MagneticField
TemporalDescription
TimeSpan
StartDate
1990-02-10 00:00:00Z
StopDate
1992-12-14 00:00:00Z
Parameter #1
Name
GALILEO PWS Rotor Attitude Right Ascension
Description
GALILEO PWS Rotor Attitude Right Ascension in EME50 (Earth Mean Equatorial equinox of 1950)
Caveats
The basic rotor coordinate system has its Z-axis aligned with the spin axis (positive in the opposite direction as the HGA) and its +Y-axis pointing outward from the spacecraft body along the magnetometer boom. X completes the right handed set. This coordinate system spins with the rotor at a period of approximately 19 seconds.
Units
°
UnitsConversion
0.0174532925>rad
Support
SupportQuantity
Other
Parameter #2
Name
GALILEO PWS Rotor Attitude Declination
Description
GALILEO PWS Rotor Attitude Declination in EME50 (Earth Mean Equatorial equinox of 1950)
Units
°
UnitsConversion
0.0174532925>rad
Support
SupportQuantity
Other
Parameter #3
Name
GALILEO PWS Rotor Attitude Twist
Description
GALILEO PWS Rotor Attitude Twist in EME50 (Earth Mean Equatorial equinox of 1950)
Units
°
UnitsConversion
0.0174532925>rad
Support
SupportQuantity
Other