Mirror lightweight for a spaceborne remote sensing instrument
The paper aims at obtaining the optimum lightweight configuration for a primary mirror (M1) with honeycomb patterns for a space satellite. The finite element analysis and Zernike polynomial fitting based on the Taguchi Method are applied to the whole optimization process. Geometrical control factors...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Chinese Geoscience Union
2017-01-01
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| Series: | Terrestrial, Atmospheric and Oceanic Sciences |
| Online Access: |
http://tao.cgu.org.tw/media/k2/attachments/v282p139.pdf
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