Abstract
The new kinematic scheme for large petal-type space mirror package and deployment is considered. To check the approach the computer and physical models of multibody transformable structure were developed and studied. Results of simulation are presented in the paper.
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References
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© 2015 Springer International Publishing Switzerland
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Bujakas, V.I. (2015). Computer and Physical Simulation of Space Mirror Deployment. In: Flores, P., Viadero, F. (eds) New Trends in Mechanism and Machine Science. Mechanisms and Machine Science, vol 24. Springer, Cham. https://doi.org/10.1007/978-3-319-09411-3_79
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DOI: https://doi.org/10.1007/978-3-319-09411-3_79
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Online ISBN: 978-3-319-09411-3
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