2.4.0 spase://CNES/NumericalData/CDPP-Archive/Galileo/PWS/AACS/GALILEO_PWS_AACS GALILEO PWS AACS https://doi.org/10.24400/802406/mxx7-vqdm 2022-03-22T11:28:57Z 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). 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. spase://CNES/Person/CDPP-Archive/Donald.A.Gurnett PrincipalInvestigator spase://CNES/Person/CDPP-Archive/Philippe.Louarn CoInvestigator spase://CNES/Person/CDPP-Archive/William.S.Kurth CoInvestigator spase://CNES/Person/CDPP-Archive/CDPP.general.contact GeneralContact spase://CNES/Repository/CDPP-Archive/REGARDS-CDPP Online REGARDS https://regards.cnes.fr/user/cdpp/modules/1777?sp=DatasetName;q=DatasetName:GALILEO_PWS_AACS Access via CNES Data Archive for CDPP Text.ASCII spase://CNES/Instrument/CDPP-Archive/Galileo/PWS Waves.Passive MagneticField 1990-02-10T00:00:00Z 1992-12-14T00:00:00Z GALILEO PWS Rotor Attitude Right Ascension GALILEO PWS Rotor Attitude Right Ascension in EME50 (Earth Mean Equatorial equinox of 1950) 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. ° 0.0174532925>rad Other GALILEO PWS Rotor Attitude Declination GALILEO PWS Rotor Attitude Declination in EME50 (Earth Mean Equatorial equinox of 1950) ° 0.0174532925>rad Other GALILEO PWS Rotor Attitude Twist GALILEO PWS Rotor Attitude Twist in EME50 (Earth Mean Equatorial equinox of 1950) ° 0.0174532925>rad Other