DocumentCode :
2086207
Title :
Robust control for microgravity vibration isolation with parametric uncertainty
Author :
Whorton, Mark S.
Author_Institution :
TD55/Control Syst. Group, NASA Marshall Space Flight Center, Huntsville, AL, USA
Volume :
1
fYear :
2002
fDate :
2002
Firstpage :
256
Abstract :
Many space-science experiments need an active isolation system to provide a sufficiently quiescent microgravity environment. Modern control methods provide the potential for both high-performance and robust stability in the presence of parametric uncertainties that are characteristic of microgravity vibration isolation systems. This paper compares microgravity vibration isolation control system designs using H2 and H methods on the basis of nominal performance and robustness to parametric uncertainties.
Keywords :
H control; aerospace control; feedback; robust control; uncertain systems; vibration isolation; zero gravity experiments; H control; active isolation system; feedback; microgravity vibration isolation systems; parametric uncertainties; robust control; stability; uncertain systems; Acceleration; Attenuation; Control systems; Frequency; Hydrogen; Payloads; Robust control; Space stations; Uncertainty; Vibration control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2002. Proceedings of the 2002
ISSN :
0743-1619
Print_ISBN :
0-7803-7298-0
Type :
conf
DOI :
10.1109/ACC.2002.1024813
Filename :
1024813
Link To Document :
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