PDS_VERSION_ID = PDS3 RECORD_TYPE = VARIABLE_LENGTH RECORD_BYTES = UNK SPACECRAFT_NAME = "CASSINI ORBITER" INSTRUMENT_NAME = "COMPOSITE INFRARED SPECTROMETER" MISSION_PHASE_NAME = "SATURN TOUR" OBJECT = TEXT INTERCHANGE_FORMAT = ASCII PUBLICATION_DATE = 2005-07-01 NOTE = "N/A" END_OBJECT = TEXT END Cassini Composite Infrared Spectrometer Time Sequential Data Record Archive ERRATA.TXT 23 May 2005 C.A. Nixon University of Maryland ============================================================================== INTRODUCTION ============================================================================== This file contains a listing of errors, anomalies, and other notes regarding the data archive from the Cassini orbiter CIRS instrument. Although considerable care has gone into making this volume, errors are both possible and likely. Users of the data are advised to exercise the same caution as they would when dealing with any other unknown data set. Reports of errors or difficulties would be appreciated. Please contact one of the persons listed herein. ============================================================================== ERRORS, ANOMALIES, AND OTHER NOTES ============================================================================== .Although considerable care has gone into making this volume, errors are both possible and likely. Users of the data are advised to exercise the same caution as they would when dealing with any other unknown data set. Reports of errors or difficulties would be appreciated. Please contact one of the persons listed herein. ============================================================================== ERRORS, ANOMALIES, AND OTHER NOTES ============================================================================== CIRS interferogram data suffers from a number of external interferences, especially: - an 8 Hz spike pattern due to the spacecraft clock ticks. - a 1/2 Hz spike pattern due to the Bus Interface Unit, transfer of data. - a sine wave of variable frequency which appears correlated with the electronics board temperature. - scan speed fluctuations which have been traced to two mechanical vibrations on the spacecraft: (a) the MIMI LEMMS actuator (b) the reaction wheels used to turn the spacecraft. These various effects are described in more detail in the cirs_interferences.pdf document found in the DOC directory.