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Robust Constrained Optimization Approach to Control Design for International Space Station Centrifuge Rotor Auto Balancing Control SystemThis thesis discusses application of a robust constrained optimization approach to control design to develop an Auto Balancing Controller (ABC) for a centrifuge rotor to be implemented on the International Space Station. The design goal is to minimize a performance objective of the system, while guaranteeing stability and proper performance for a range of uncertain plants. The Performance objective is to minimize the translational response of the centrifuge rotor due to a fixed worst-case rotor imbalance. The robustness constraints are posed with respect to parametric uncertainty in the plant. The proposed approach to control design allows for both of these objectives to be handled within the framework of constrained optimization. The resulting controller achieves acceptable performance and robustness characteristics.
Document ID
20070010767
Acquisition Source
Johnson Space Center
Document Type
Thesis/Dissertation
Authors
Postma, Barry Dirk
(Draper (Charles Stark) Lab., Inc. Houston, TX, United States)
Date Acquired
August 23, 2013
Publication Date
April 1, 2005
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-9030
Report Number: JSC-CN-9030
Funding Number(s)
CONTRACT_GRANT: NAS9-01069
Distribution Limits
Public
Copyright
Public Use Permitted.
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