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