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Dynamic isolation of a spacecraft science platform via momentum compensationThe dynamic isolation of a two degree of freedom inertially stabilized science platform from the spacecrft basebody is examined. The important implications of a momentum compensated platform for pointing performance and cost are discussed, and the concept of a new system called the Integrated Platform Pointing and Attitude Control Subsystem utilizing the above property is presented. The results established in this paper are demonstrated by a computer simulation.
Document ID
19850028931
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Boussalis, D.
(California Institute of Technology, Jet Propulsion Laboratory, Guidance and Control Section, Pasadena CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1983
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
85A11082
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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