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Command and control of the Voyager spacecraftThe Voyager Mission was designed to be conducted using reprogrammable onboard computers. This decision was based on the need for highly reliable semi-autonomous operations of the spacecraft and the lengthy two-way communication times envisioned during the mission. Command and control of the spacecraft is effected by the process through which the programs for these computers are developed. While this results in a relatively passive real-time command and control function, provisions exist for intervention to occur in order to modify or augment the programs or respond to spacecraft anomalies.
Document ID
19870037700
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Adamski, Terrence P.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 87-0501
Accession Number
87A24974
Distribution Limits
Public
Copyright
Other

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