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Neptune encounter - Guidance and control's finest hourThe Voyager 2 technology had to be stretched significantly to confront the challenges posed by the environment of Neptune. Little was known about Neptune's characteristics because of its great distance from the sun; and its reduced light levels required longer exposure time. Thus, it was necessary to reduce the spacecraft limit cycle; this was made more difficult by the trajectory selected, which caused high spacecraft-to-target rates (these rates dictated the use of image motion compensation). Another challenge faced by Voyager 2 was the need to perform all the required image motion compensation with a limited quantity of attitude control computer and command computer memory, together with a limited quantity of tape recorder resources. This made necessary a new concept of real-time image motion compensation.
Document ID
19910042205
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Miller, Maurine
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hanover, Gene
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Lin, Ho-Sen
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Patel, Keyur
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wahl, Edward
(JPL Pasadena, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AAS PAPER 90-060
Report Number: AAS PAPER 90-060
Meeting Information
Meeting: Annual Rocky Mountain Guidance and Control Conference
Location: Keystone, CO
Country: United States
Start Date: February 3, 1990
End Date: February 7, 1990
Sponsors: AAS
Accession Number
91A26828
Distribution Limits
Public
Copyright
Other

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