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Parametric Robustness Analysis for Cassini Spacecraft Using the LMI Approach without Frequency SweepA generalized Popov multiplier theory enables one to analyze system robustness with mixed real/complex parameters, repeated uncertainties, and multidimensional block uncertainties. Using the Cassini spacecraft thrust vector control (TVC) system as a design case study, modern robust control theory has been applied to the real flight project.
Document ID
20210001242
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
Authors
Chiang, R.
Date Acquired
June 29, 1994
Publication Date
June 29, 1994
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
spacecraft
attitude
control
system
Cassini
robust
control
analysis

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