DocumentCode :
2792033
Title :
Application of Shape Memory Alloy Actuators in Active Shape Control of Inflatable Space Structures
Author :
Peng, Fujun ; Jiang, Xin-Xiang ; Hu, Yan-Ru ; Ng, Alfred
Author_Institution :
Directorate of Spacecraft Eng., Canadian Space Agency
fYear :
2005
fDate :
5-12 March 2005
Firstpage :
1
Lastpage :
10
Abstract :
SMA (shape memory alloy) actuators have found a wide range of applications due to their unique properties such as high force, long stroke, small size, light weight, and silent operation, etc. However, their strong nonlinear properties make them a challenge to achieve accurate actuation. This paper presents a simple control strategy based on the idea of adjusting the SMA wire temperature as fast as possible. This strategy is simple, stable, and requires no hysteresis model or thermal model. This strategy is tested with displacement output, and effects of updating rate and input current on control accuracy are also discussed. This control strategy is then used for active shape control of inflatable space structures. Results indicate that under this control strategy, shape memory alloy wire actuators can offer very good accuracy, and for inflatable structure shape control, great improvement can be achieved
Keywords :
alloys; genetic algorithms; microactuators; nonlinear control systems; shape control; shape memory effects; wires; SMA wire temperature; active shape control; control strategy; hysteresis model; inflatable space structures; precision control; shape memory alloy actuators; thermal model; Actuators; Biomembranes; Capacitive sensors; Displacement control; Shape control; Shape memory alloys; Space vehicles; Synthetic aperture radar; Testing; Wire; actuator; inflatable structures; precision control; shape control; shape memory alloy;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2005 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-8870-4
Type :
conf
DOI :
10.1109/AERO.2005.1559577
Filename :
1559577
Link To Document :
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