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タイトルPinhole/coronograph pointing control system integration and noise reduction analysis
本文(外部サイト)http://hdl.handle.net/2060/19840025702
著者(英)Greene, M.
著者所属(英)Alabama Univ.
発行日1981-09-01
言語eng
内容記述The Pinhole Occulter Facility (P/OF) is a Space Shuttle based experiment for the production of solar coronographics and hard X-ray images. The system is basically pinhole camera utilizing a deployable 50-m flexible boom for separating the pinholes and coronograph shields from the recording devices located in the Shuttle bay. At the distal end of the boom from the Shuttle is a 25 kg mask containing pinholes and coronograph shields. At the proximal end the detectors are located and mounted, along with the deployable boom, to the ASPS gimbal pointing system (AGS). The mask must be pointed at the Sun with a high degree of pointing stability and accuracy to align the axes of the detectors with the pinholes and shields. Failure to do so will result in a blurring of the images on the detectors and a loss of resolution. Being a Shuttle based experiment, the system will be subjected to the disturbances of the Shuttle. The worst of these is thruster firing for orbit correction; the Shuttle uses a bang-bang thruster control system to maintain orbit to within preset limits. Other disturbances include man motion, motion induced by other systems, and gravity gradient torques.
NASA分類INSTRUMENTATION AND PHOTOGRAPHY
レポートNO84N33773
BER-274-100
NASA-CR-171152
NAS 1.26:171152
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/158321


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