NASA NTRS · 19660059571
A split-damper inertially coupled passive gravity-gradient attitude control system.
Abstract
Attitude errors of inertially coupled gravity gradient satellite with solar radiation pressure as dominant disturbance, noting slot problems in stabilized package accommodating damper motion
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Merrick, V. K., Tinling, B. E., Watson, D. M.. 1966-01-01. A split-damper inertially coupled passive gravity-gradient attitude control system.. https://ntrs.nasa.gov/citations/19660059571
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