NASA NTRS · 19730019090
Fine pointing control, OAO-3
Abstract
The fine error sensor located within the Princeton Experiment Package (PEP) is designed to aquire a star within its field of view to hold the spacecraft within plus or minus one-tenth of an arc second in pitch, and plus or minus three-arc seconds about the yaw axis. Pointing accuracy and stability tests of the fine error sensor exceeded the plus or minus 0.1 arc second requirement.
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Moore, J. V.. 1973-01-01. Fine pointing control, OAO-3. https://ntrs.nasa.gov/citations/19730019090
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