NASA NTRS · 19920020569
Geostationary Operational Environmental Satellite (GOES-N report). Volume 2: Technical appendix
Abstract
The contents include: operation with inclinations up to 3.5 deg to extend life; earth sensor improvements to reduce noise; sensor configurations studied; momentum management system design; reaction wheel induced dynamic interaction; controller design; spacecraft motion compensation; analog filtering; GFRP servo design - modern control approach; feedforward compensation as applied to GOES-1 sounder; discussion of allocation of navigation, inframe registration and image-to-image error budget overview; and spatial response and cloud smearing study.
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1992-02-01. Geostationary Operational Environmental Satellite (GOES-N report). Volume 2: Technical appendix. https://ntrs.nasa.gov/citations/19920020569
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