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Spacecraft Attitude Control Using Nonlinear Servomechanism TheoryThe recently developed nonlinear servomechanism theory is applied to the attitude control of large maneuvering spacecraft subject to sinusoidal disturbances and parametric uncertainties.
Document ID
20060037958
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
hdl:2014/33207
Authors
Huang, J.
Lin, C.
Hadaegh, F. Y.
Chiang, R. Y.
Date Acquired
August 23, 2013
Publication Date
April 1, 1994
Distribution Limits
Public
Copyright
Other
Keywords
nonlinear servomechanism spacecraft attitude control problem

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