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LMI multiplier Km/μ-analysis of the Cassini spacecraft

✍ Scribed by J. H. Ly; R. Y. Chiang; K. C. Goh; M. G. Safonov


Publisher
John Wiley and Sons
Year
1998
Tongue
English
Weight
369 KB
Volume
8
Category
Article
ISSN
1049-8923

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✦ Synopsis


A robustness analysis for the Cassini spacecraft z-axis thrust vector control system is performed using the real/complex K K / -analysis theory. The analysis is done using the linear matrix inequality (LMI) technique for finding optimal fixed-order multipliers. The utilization of the LMI fixed-order multiplier optimization theory for K K / -synthesis is also discussed.