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Modeling and dynamics of tethered formations for space interferometryWe describe a rather general model used to predict the dynamics and control performance of formations of spacecraft connected by tethers in heliocentric orbit and in low Earth orbit.
Document ID
20060033647
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/16379
Authors
Quadrelli, M.
Date Acquired
August 23, 2013
Publication Date
October 20, 2000
Subject Category
Astrodynamics
Distribution Limits
Public
Copyright
Other
Keywords
space interferometry spacecraft control dynamics reconfiguration

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