DocumentCode
1601536
Title
Control of gimbal dynamics via sensitivity models for uncertainty in friction parameters
Author
Schoenwald, D. ; Özgüner, Ü ; Graham, R.
Author_Institution
Dept. of Electr. Eng., Ohio State Univ., Columbus, OH, USA
fYear
1992
Firstpage
52
Abstract
Tracking control of the beta gimbals for the solar array panels on the space station Freedom is investigated. In particular, the issue of control in the presence of uncertainty in motor friction parameters is addressed. The impact of parametric uncertainty on gimbal performance is analyzed by incorporating sensitivity functions in the feedback loop to desensitize the gimbal control law to parameter variations. The simulation results indicate that the inclusion of one particular sensitivity function yields some improvements in closed-loop performance when friction parameters are varied from their nominal values
Keywords
aerospace control; attitude control; feedback; sensitivity; solar cell arrays; space vehicle power plants; tracking systems; beta gimbals; closed-loop performance; feedback loop; friction parameter uncertainty; gimbal dynamics control; motor friction parameters; parametric uncertainty; sensitivity models; solar array panels; space station Freedom; tracking control; Actuators; Angular velocity; Feedback loop; Friction; Motor drives; NASA; Optimal control; Performance analysis; Space stations; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 1992., First IEEE Conference on
Conference_Location
Dayton, OH
Print_ISBN
0-7803-0047-5
Type
conf
DOI
10.1109/CCA.1992.269899
Filename
269899
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