Abstract
The law of universal gravitation, proposed by Newton, provides the theoretical basis for the development of artificial satellites, which consist of the proprietary system and support system. The deployable antenna is an important part of the proprietary system.
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References
Li TJ (2012) Deployment analysis and control of deployable antenna. Aerosp Sci Technol 18(1):42–47
Kashni K (1988) Representation of cables in space subjected to uniformly distributed loads. Int J Space Struct 3(4):221–230
Zhang YQ, Yang DW, Li SL (2016) An integrated control and structural design approach for mesh reflector deployable space antennas. Mechatronics 35:71–81
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Duan, B., Zhang, Y., Du, J. (2020). Analysis and Control of Flexible Multibody Deployment. In: Large Deployable Satellite Antennas. Springer Tracts in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-15-6033-0_4
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DOI: https://doi.org/10.1007/978-981-15-6033-0_4
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Online ISBN: 978-981-15-6033-0
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