DocumentCode
1686098
Title
Active control for large space structure by fuzzy logic controllers
Author
Ofri, Azmon ; Tanchum, Weller ; Guterman, Hugo
Author_Institution
Fac. of Mech. Eng., Technion-Israel Inst. of Technol., Haifa, Israel
fYear
1996
Firstpage
515
Lastpage
518
Abstract
In this study, a `lump-parameter´ model was formulated to represent a large flexible space structure (solar panel) controlled by bonded piezoceramic actuators. A control strategy based on fuzzy logic theory (FLC) was developed for vibration damping. A comparison of the performance of the proposed FLC with that obtained by applying LQR is presented
Keywords
aerospace control; fuzzy control; linear quadratic control; photovoltaic power systems; piezoelectric actuators; solar cell arrays; space vehicle power plants; vibration control; LQR; PZT composite structure; active control; bonded piezoceramic actuators; fuzzy logic control; fuzzy logic controllers; large flexible space structure; large space structure; lump-parameter model; performance; solar panel; vibration damping; Actuators; Bonding; Damping; Flexible structures; Fuzzy control; Fuzzy logic; Motion control; Piezoelectric materials; Space stations; Vibration control;
fLanguage
English
Publisher
ieee
Conference_Titel
Electrical and Electronics Engineers in Israel, 1996., Nineteenth Convention of
Conference_Location
Jerusalem
Print_ISBN
0-7803-3330-6
Type
conf
DOI
10.1109/EEIS.1996.567029
Filename
567029
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