NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Attitude control fault protection - The Voyager experienceThe length of the Voyager mission and the communication delay caused by the distances involved made fault protection a necessary part of the Voyager Attitude and Articulation Control Subsystem (AACS) design. An overview of the Voyager attitude control fault protection is given and flight experiences relating to fault protection are provided.
Document ID
19810034959
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Litty, E. C. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1980
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS 80-018
Meeting Information
Meeting: Annual Rocky Mountain Conference
Location: Keystone, CO
Start Date: February 17, 1980
End Date: February 21, 1980
Accession Number
81A19363
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available