The Hinode Mission
DOI: 10.1007/978-0-387-88739-5_10
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Image Stabilization System for Hinode (Solar-B) Solar Optical Telescope

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Cited by 16 publications
(19 citation statements)
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“…The OTA is a diffraction-limited Gregorian telescope with a diameter of 50 cm which is the largest solar optical telescope in space, and the FPP includes the Narrowband Filter Imager (NFI), the Broadband Filter Imager (BFI), and the Spectro-Polarimeter (SP). The SOT provides unprecedented high-resolution photometric and vector magnetic images of the photosphere and chromosphere with a very stable point spread function and is equipped with an image stabilization system (Shimizu et al 2008) with the performance better than 0.01 arcsec rms. The BFI produces photometric images with broad spectral resolution in six bands (CN band, Ca II H line, G band, and three continuum bands) at the highest spatial resolution available from the SOT (0.0541 arcsec pixel −1 sampling) and at a rapid cadence (< 10 s) over a 218 × 109 arcsec FOV.…”
Section: Observation and Data Analysismentioning
confidence: 99%
“…The OTA is a diffraction-limited Gregorian telescope with a diameter of 50 cm which is the largest solar optical telescope in space, and the FPP includes the Narrowband Filter Imager (NFI), the Broadband Filter Imager (BFI), and the Spectro-Polarimeter (SP). The SOT provides unprecedented high-resolution photometric and vector magnetic images of the photosphere and chromosphere with a very stable point spread function and is equipped with an image stabilization system (Shimizu et al 2008) with the performance better than 0.01 arcsec rms. The BFI produces photometric images with broad spectral resolution in six bands (CN band, Ca II H line, G band, and three continuum bands) at the highest spatial resolution available from the SOT (0.0541 arcsec pixel −1 sampling) and at a rapid cadence (< 10 s) over a 218 × 109 arcsec FOV.…”
Section: Observation and Data Analysismentioning
confidence: 99%
“…The research has focused on many aspects related to microvibrations, starting with the sources [7,8], and throughout the years various methodologies have been proposed for their modelling and control [9][10][11][12], e.g., simulating the interface between sources and spacecraft structures and predicting payload pointing errors [13,14]. Among the difficulties related to microvibrations, one of the main ones is their analysis, having to deal with extremely low amplitudes (µg) and a bandwidth that goes up to several hundred Hz.…”
Section: Introductionmentioning
confidence: 99%
“…The microvibrations produced by reaction/momentum wheel assemblies (R/MWA) onboard spacecraft, for example reaction/momentum wheel assemblies (R/MWA), cryo-coolers, thrusters, solar array drive mechanisms, and mobile mirrors, can degrade the performance of instruments with high pointing precision and stability [1][2][3][4]. These disturbances are attracting more and more attentions, because they are significant in the 1k Hz frequency range [5] and excite flexible modes of the spacecraft, which cannot be controlled or reduced by the attitude and orbit control systems.…”
Section: Introductionmentioning
confidence: 99%