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|a Mendillo, Christopher B.
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|a Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
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|a Cahoy, Kerri
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|a Marinan, Anne D.
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|a Brown, Joshua
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|a Martel, Jason
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|a Howe, Glenn A.
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|a Hewawasam, Kuravi
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|a Finn, Susanna C.
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|a Cook, Timothy A.
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|a Chakrabarti, Supriya
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|a Douglas, Ewan S.
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|a Mawet, Dimitri
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|a Guyon, Olivier
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|a Singh, Garima
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|a Lozi, Julien
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|a Cahoy, Kerri
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|a Marinan, Anne D.
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|a The low-order wavefront sensor for the PICTURE-C mission
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|b SPIE,
|c 2018-05-07T19:11:55Z.
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|z Get fulltext
|u http://hdl.handle.net/1721.1/115250
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|a The PICTURE-C mission will fly a 60 cm off-axis unobscured telescope and two high-contrast coronagraphs in successive high-altitude balloon flights with the goal of directly imaging and spectrally characterizing visible scattered light from exozodiacal dust in the interior 1-10 AU of nearby exoplanetary systems. The first flight in 2017 will use a 10[superscript -4] visible nulling coronagraph (previously flown on the PICTURE sounding rocket) and the second flight in 2019 will use a 10[superscript -7] vector vortex coronagraph. A low-order wavefront corrector (LOWC) will be used in both flights to remove time-varying aberrations from the coronagraph wavefront. The LOWC actuator is a 76-channel high-stroke deformable mirror packaged on top of a tip-tilt stage. This paper will detail the selection of a complementary high-speed, low-order wavefront sensor (LOWFS) for the mission. The relative performance and feasibility of several LOWFS designs will be compared including the Shack-Hartmann, Lyot LOWFS, and the curvature sensor. To test the different sensors, a model of the time-varying wavefront is constructed using measured pointing data and inertial dynamics models to simulate optical alignment perturbations and surface deformation in the balloon environment.
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|a United States. National Aeronautics and Space Administration (Grant NNX15AG23G S01)
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|a Article
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|t Proceedings Volume 9605, Techniques and Instrumentation for Detection of Exoplanets VII
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