DocumentCode
2492231
Title
Integrated identification and control of magneto-rheological dampers for manned space missions
Author
Kaya, Mustafa Aytug ; Bayrakceken, Mehmet Kemal ; Celik, Eyyup
Author_Institution
Air War Coll., Turkish Air Force, Istanbul, Turkey
fYear
2011
fDate
9-11 June 2011
Firstpage
89
Lastpage
94
Abstract
Prolonged stay in space provokes physiological changes in astronauts. Hurdling negative effects of zero-g environment requires routine exercise. A lightweight, reliable treadmill platform utilizing a magnetorheological damper was modeled to suppress the vibration of the platform for this purpose, since a magnetorheological damper is a semi-active device that is maintenance free and requires low power. Immediate servicing would not be available in space applications; therefore, an adaptive inverse control algorithm was utilized so that the system would not be affected by the uncertainties and parameter changes that might happen within the system. The system is controlled via LQR and S/KS mixed sensitivity H∞ methods which produce the desired control force required from the damper. Adaptive inverse algorithm is the inverse function of the damper model, which uses the desired force as input and produces the control voltage that will be applied to the damper.
Keywords
H∞ control; adaptive control; aerospace control; damping; magnetorheology; vibration control; S/KS mixed sensitivity H∞ methods; adaptive inverse control algorithm; damper model; integrated identification; inverse function; magnetorheological damper; manned space missions; semiactive device; space applications; Damping; Fluids; Force; Friction; Mathematical model; Shock absorbers; Voltage control; ISS; MR damper; magnetorheological damper; magnetorheological fluids; satellite;
fLanguage
English
Publisher
ieee
Conference_Titel
Recent Advances in Space Technologies (RAST), 2011 5th International Conference on
Conference_Location
Istanbul
Print_ISBN
978-1-4244-9617-4
Type
conf
DOI
10.1109/RAST.2011.5966971
Filename
5966971
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