Payload characterization for CubeSat demonstration of MEMS deformable mirrors
Coronagraphic space telescopes require wavefront control systems for high-contrast imaging applications such as exoplanet direct imaging. High-actuator-count MEMS deformable mirrors (DM) are a key element of these wavefront control systems yet have not been flown in space long enough to characterize...
| Main Authors: | , , , , |
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| Other Authors: | |
| Format: | Article |
| Language: | en_US |
| Published: |
SPIE
2015
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| Online Access: | http://hdl.handle.net/1721.1/96919 https://orcid.org/0000-0001-5391-9844 https://orcid.org/0000-0002-7791-5124 https://orcid.org/0000-0001-9005-2493 |