Abstract
A robustness analysis for the Cassini spacecraft z-axis thrust vector control system is performed using the real/complex Km/μ-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 Km/μ-synthesis is also discussed. © 1998 John Wiley & Sons, Ltd.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callMore From: International Journal of Robust and Nonlinear Control
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
