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The Voyager 2 scan platform anomalyThe two Voyager spacecraft were launched in the summer of 1977, flew past Jupiter in 1979, and reached Saturn in 1980 and 1981. The Voyager Attitude and Articulation Control Subsystem (AACS) controls the positioning of a scan platform on which scientific instruments are mounted. On August 26, 1981, it was discovered that the azimuth axis of the scan platform of Voyager 2 had not completed the commanded slew. The profile of the failed slew command resembled a similar scan failure on Voyager 1 on February 23, 1979. In that case, contamination of the output gear mesh in the azimuth actuator was identified as the most probable cause of the failure. The problem was solved by cycling the azimuth actuator until the contaminant broke down and smooth operation was restored. A similar treatment applied to the Voyager 2 problem failed. Details of the Voyager 2 anomaly investigation are discussed.
Document ID
19830062955
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Marchetto, C. A.
(California Institute of Technology, Jet Propulsion Laboratory, Guidance and Control Section, Pasadena CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS PAPER 83-046
Report Number: AAS PAPER 83-046
Meeting Information
Meeting: Guidance and control 1983
Location: Keystone, CO
Start Date: February 5, 1983
End Date: February 9, 1983
Accession Number
83A44173
Distribution Limits
Public
Copyright
Other

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