Systematic design of tape spring hinges for solar array by optimization method considering deployment performances

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This paper reports the systematic development of tape spring hinges for a solar array by an optimization method considering various deployment performances. The nonlinear behavior between the moment and the rotation angle of a tape spring hinge is determined through experimental results rather than through finite element analysis results or theoretical solutions in order to identify the moment-rotation profile accurately. Response surfaces comprising the measured moment-rotation profile and design parameters of a tape spring hinge are generated by a Box-Behnken experimental design. Furthermore, to consider deployment performances such as low latch-up load, latching without overshoot, high deployment stiffness, and high torque margin, the deployment equation is derived by Kane's dynamic equation considering any number of solar panels. The present study proposes a systematic approach for designing tape spring hinges for any number of solar panels; the designed hinges satisfy all design requirements. The approach involves minimizing the cost function including several design requirements and solving the deployment equation containing the response surfaces of the moment-rotation profiles simultaneously. To verify the effectiveness of the proposed approach, several examples are demonstrated.
Publisher
ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER
Issue Date
2015-10
Language
English
Article Type
Article
Keywords

PARTICLE SWARM OPTIMIZER; DYNAMICS; SATELLITE

Citation

AEROSPACE SCIENCE AND TECHNOLOGY, v.46, pp.124 - 136

ISSN
1270-9638
DOI
10.1016/j.ast.2015.06.013
URI
http://hdl.handle.net/10203/205238
Appears in Collection
ME-Journal Papers(저널논문)
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